JP2015112929A - Manufacturing method and components of flying body for individual's aerial work - Google Patents

Abstract

PROBLEM TO BE SOLVED: To provide a flying body that enables an individual's short time and easy high place work to be carried out safely, reliably, and at low price.SOLUTION: A flying body for aerial work composes an upper flying body 101 of a plurality of electric motors 205, a plurality of propellers 204, carbon fiber-reinforced resin, glass fiber-reinforced resin, a carbon fiber tape, a carbon fiber wire, an aluminum pipe, foamed resins, a rope, a stainless annealing wire, a wire, and a honeycomb sandwich panel, and performs free aerial movement by the movement of the center of gravity of a lower hanging body 102 composed of a human 104, an electric current control device, a shock absorber 207, and a battery 208.

Description

Aircraft, mechanical engineering, electrical engineering, helicopter.

A personal helicopter with a counter-rotating rotor is not suitable for a personal aerial work flying object because the noise and air pollution of the internal combustion engine is severe and the exposed rotor is large and the aerial work is difficult and expensive.

Patent Publication 2013-107528 Patent Publication 2012-218735

Illustrated helicopter mechanism and control (Bluebacks) Hideo Suzuki (2001/10/19) New Adamski Complete Works 3 Science of Life in the 21st Century (Central Art Publishing) Translated by Hachiro Kubota by Georgia Adamski (2013/4/15)

The desire for individuals to fly freely is intense. The wish could not be fulfilled in terms of safety and price. At a position higher than the ladder in building work and painting work, it was necessary to assemble a scaffold that would be troublesome, time consuming and expensive even for high altitude work. There was a risk of falling when working at heights. Personal helicopters are expensive and unsuitable for high altitude work.

The present invention is the realization of Leonardo da Vinci's dream. I gained knowledge of personal flying objects through impression wave communication with the Tenshin Seishin Goddess Otsutsu Himegami. The consciousness of the fetus where Amateru's wife, Atsuru Seori, and Amaterasu intermingled became various ideas such as a number of children or sea urchin spines. It was transmitted for 24 hours from early morning to noon, evening or midnight by wave, and as a result, it was delivered as a manufacturing method and constituent material for personal aerial work flying objects. A couple who has one child and a husband who has one child becomes one of the family, and one more is the application of the cosmic principle that gives birth to multiple families and thrives. The universe principle is the law of cause and effect. You can see the cause and effect by looking at the results. If you ask for a cause, the cause will be the result. For this reason, he strongly desires to fly in the sky, and unites his consciousness with the precious aspiration that is the root of cosmic consciousness. The invention is the result. This is the history of the present invention. There is a mission to make the earth a peaceful and clean space for the sake of mankind so that the universe does not develop and become emptiness of the throat. This is an invention that advances the current technology only one step. I want you to recall an aerial work flying light truck. An aerial work flying object is an aerial work flying light truck that can move freely in the air within the safe range without the need of advanced flight technology in the air like a light truck for leisure or work on the earth Make space available. The policy of description description is aimed at precise and easy-to-understand accuracy, intelligibility, clear technology and technical progress. This invention could not have been achieved without the strong cooperation of the God God God God. I would like to thank the spirit of Karakuri Giemon Shigenohaka Tanaka. This invention largely depends on the space philosophy translated by Hachiro Kubota by Georgia Damsky. Thanks to this book, it has become possible to receive impression waves from space consciousness. Here are the signposts and footprints of the invention. Thank you to all of you. Everything is connected. I strongly encourage you to live with the universe, leaving everything to the Creator. Everything is the gift of the Creator, the Creator. We see a macro world that is visible, but there is a macro world invisible behind it. The world can be seen with the eyes of the heart. Humans were born in this world to do filial piety. Parents are heavenly parents and earth parents. Life is a place to learn patience. There are many repetitions due to many combinations of accuracy and combination. Please forgive me. This is to prevent abuse of rights. If an individual wants to fly freely, that's a strong human race. We assumed a combination of various methods. This is because the description is specific and detailed. The manufacturing method and materials of personal aerial work flying objects are the realization of human dreams. In order to achieve light weight, robustness, practical application, and safe and reliable flight, there can be no invention without a composite material that combines various technologies of humanity. The invention of a composite material and a powerful and lightweight motor was necessary. In order to realize a power hybrid hybrid device to realize a flying object for personal aerial work, it was necessary to invent a device in which energy different from the conventional one was integrated and computer-controlled. Anti-bird strike fiber reinforced resin metal composite turbine laminated electric motor forced air cooling overall heat radiating fiber reinforced resin metal composite internal combustion engine angular momentum adjustment spring wheel torque converter clutch computer management generator motor output power transmission integrated hybrid device, forced air cooling overall radiating fiber Reinforced resin metal composite rotor magnet stator Electric coil disk laminated electric motor, bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor, forced air cooling overall heat radiating fiber reinforced resin metal composite internal combustion engine, etc. were required . Personal air work flying object simulates dandelion seeds flying in the sky, multiple electric motors, multiple internal combustion engines, composite devices, multiple propellers, hot air balloons, gas balloons, carbon fiber reinforced resin, glass fiber reinforced resin, Carbon fiber tape, carbon fiber wire, aluminum pipe, foamed resin, rope, stainless steel wire, wire assemble the saddle-shaped assembly, laminated honeycomb sandwich panel, horizontal member and vertical member into the upper flying body, human, current control device In addition, the shock absorber and battery are used as the lower suspension, and the flying object can be moved freely by moving the center of gravity, enabling safe, reliable, inexpensive, and easy personal work in a short time. For the elderly who lost their teeth, we invented a silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer mesh part metal ceramic composite laminated denture manufacturing method. This is an application of a composite layering technology for flying objects in the individual aerial work. May God's love come. Thank you for all the mourning gods.

It has made it possible to enjoy leisure and sports such as the quietness of the clear air, the safety of large passenger planes, high-speed work in a short period of time, and relatively easy floating. Laminated composite materials are technologies that can be applied to aircraft, airships, and spacecraft.

It is the whole block diagram of the personal air work flying object which simulated the seed of the dandelion. It is the whole block diagram of the personal aerial work flying object of the hot air balloon and gas balloon which simulated the shape of the ice cream cone, or the hot air balloon and gas balloon combined type or helium mixed propane gas combustion hot gas balloon. Hot air balloon and gas balloon simulating the shape of an ice cream cone or a combination of hot air balloon and gas balloon or helium mixed propane gas combustion hot gas balloon FIG. 4 is a diagram showing that the position of the flying object for personal aerial work can be freely changed by freely changing the inclination of the electric motor. It is a figure which shows the upper flying body which assembled the square pipe in the cross-beam shape, and although it is the method of a two-layer horizontal member in the figure, it is usually about three to nine layers. It is the figure which looked down at FIG. 4 from the celestial direction. Turbine blade stacking rotor permanent magnet stator Electric coil Electric motor is the simplest method applied to an aerial work flying object. In the figure, the upper turbine blade blade has a permanent magnet at the center and an electric coil at the bottom. It is the figure which installed in the blade | wing blade radially along the concentric circle, and showed that the whole rotation was prevented by reversely rotating the blade | wing of an upper and lower turbine. It is the figure which looked down at FIG. 6 from the top toward the bottom. It is sectional drawing of a forced air cooling whole heat radiation metal fiber reinforced resin compound internal combustion engine, and a cylinder and a cylinder head are color-coded into black and white so that a structure can be understood well with a left and right cylinder. It is a figure of a forced air cooling whole heat radiation permanent magnet rotor electric coil stator disk lamination | stacking type | mold fiber reinforced resin metal composite electric motor. The air opened for forced air cooling becomes a kind of air blower by rotating a hole that is inclined at an angle of 19.5 to 33 degrees with respect to the rotation surface with respect to the rotation direction of the disk. It is a figure of the disk-shaped rotor fixed to the axis | shaft arrange | positioned radially along the concentric circle | round | yen with the permanent magnet opened with inclination so that it may send to [FIG. The rotor was rotated at an angle of 19.5 to 33 degrees with respect to the disk surface, and the rotor was rotated at an angle so that the forced air-cooled air that would be a kind of blower was sent backward through a hole that was opened diagonally. An electric coil that allows air to pass through the hole is arranged and fixed radially along the concentric circles of the stator disk, and fixed to a casing with a hole through which the shaft of the electric motor passes through the center of the stator. It is a figure of a child. It is sectional drawing of a bird strike prevention device fiber reinforced resin metal composite turbine lamination type electric motor. Bird Strike Prevention Device Fiber Reinforced Resin Metal Composite Turbine of a blade type rotor with a blade fixed to the shaft of an electric motor fixed with a permanent magnet embedded in the blade along a concentric circle with respect to the shaft of the laminated motor FIG. Bird Strike Prevention Device Fiber Reinforced Resin Metal Metal Composite Turbine Stacked Electric Motor Concentric with the shaft of the electric coil embedded in the blade and fixed at the center of the blade with a hole through which the electric motor shaft passes. It is a figure of the blade type stator fixed to the casing of the motor. The upper flying object of the personal aerial work flying object is a sphere. The upper flying body of the personal aerial work flying object is a figure of a rectangular parallelepiped. The upper flying body of the personal aerial work flying object is a rectangular parallelepiped cross-sectional view, and the horizontal member for rigid connection rigidly connected to the vertical center member is inserted through the horizontal member for fixation and fixed with a fixture, and then attached or detached. It is the figure which installed the electric motor and the propeller, or the fan in the both ends of the horizontal member for use. The above figure is a figure where the horizontal member for attachment / detachment penetrates into the center of the vertical member in the horizontal member for rigid connection, and is fixed with the fixture. A horizontal member is inserted and two removable horizontal members are abutted in the center and then fixed with a fixture.The figure below shows a single horizontal member inserted into a rigid horizontal member on one side. It is the figure fixed with the fixing tool. The upper flying body of the personal aerial work flying object is a cylindrical figure. The upper flying body of the personal aerial work flying object is a figure like a bunch of kites. It is a figure of the top flying body of a personal aerial work flying object having a conical shape with the bottom of the cone on top and the apex on the bottom. It is the figure where the upper flying body of the personal aerial work flying object is a horizontal disk, and a plurality of propellers or fans are installed inside the disk. It is the figure which the upper flying body of the personal aerial work flying object connected the some cylindrical shape horizontally. FIG. 5 is a diagram in which a plurality of horizontal disks are installed inside a sphere in which the upper flying object of the personal aerial work flying object is framed by the meridian and latitude lines of the globe, and a plurality of propellers or fans are installed in the disk. FIG. 5 is a diagram in which a plurality of horizontal disks are installed in a frame along a rotation quadratic curve, and a plurality of propellers or fans are installed in the disk. FIG. 6 is a diagram in which a plurality of propellers or fans are installed along a semicircular inside of a hemispherical net of an upper flying object of a personal aerial work flying object. It is the figure which the upper flying body of the personal aerial work flying object connected the spheroid vertically. It is the figure which the upper flying body of the personal aerial work flying object made the shape of a spheroid. It is a figure of the shape which connected the conical bottom face to the upper and lower surfaces of the cylinder shape where the upper flying body of the personal aerial work flying object suddenly sharpened both ends of a short pencil. It is the figure which the part of the cylinder shortened in the shape which connected the bottom of the cone shape to the upper and lower surfaces of the cylinder shape where the upper flying body of the personal aerial work flying object suddenly sharpened both ends of a short pencil. It is the figure which combined the cone and the cylinder that the upper flying body of the personal aerial work flying object suddenly turned the short pencil lead upward. A hemispherical shape like a monkey in the kitchen with a belt-shaped member knitted like a hemispherical bamboo basket and shaped like a crest of Shimadzu crest in a circle in the middle The figure shows an electric motor and a pre-peller or fan installed at the center of the cross beam of a figure like a crest of Shimadzu in a circle with a top and bottom. It is the figure which showed that the mark-shaped member of the center Maruta was fixed with a fixing tool, and assembly and disassembly were made easy. Braided electric motor or blade outer peripheral permanent magnet fixed outer circumferential ring electric coil with hemispherical bamboo rods like hemispherical bamboo braids knitted with belt-shaped members like a colander in the kitchen It is the figure which showed that the assembly and decomposition | disassembly of the spherical cage | basket shape fixed with the fixing tool on both sides of the fixed electric motor could be performed easily. It is the figure which laminated | stacked the honeycomb sandwich structure board | plate as an upper flying body. It is the figure which looked down at FIG. 34 from the celestial direction. The large round part has a hole in the honeycomb sandwich structure plate, and a propeller or fan and an electric motor are installed inside. There is a method in which the electric motor is a blade-laminated electric motor. A small circle is a vertical member for stacking honeycomb sandwich structure plates. It is a figure of the upper flying object which connected the abacus ball vertically. Hot air balloon, gas balloon, hot gas combined use balloon, hot gas balloon, external suspension cable back fan blow type personal aerial work flying object overall configuration that envelope (ball skin) can be automatically taken out and stored by envelope winder FIG. Hot air balloon, gas balloon, hot gas combined use balloon, hot gas balloon, external suspension cable back fan blower type personal aerial work flying object seen from the left side of the passenger who can automatically carry out and store the envelope (ball skin) with the envelope winder FIG. Hot air balloons, gas balloons, hot gas combined use balloons, hot gas balloons, and external suspension cables that can automatically carry out and store envelopes It is the figure accommodated in the envelope winder. It is a partial block diagram seen from the back of a hot air balloon, a gas balloon, a hot gas combined use balloon, a hot gas balloon, an external suspension cable back fan blower type personal aerial work flying object in which an envelope (ball skin) can be automatically carried out and stored. It is the partial block diagram seen from the right surface of the hot air balloon in which an envelope (ball skin) can be carried out and stored automatically, a gas balloon, a hot gas combined balloon, a hot gas balloon, and an external suspension cable back fan blowing type personal aerial work flying object. It is a partial block diagram seen from the left side of a hot air balloon, a gas balloon, a hot gas combined use balloon, a hot gas balloon, and an external suspension cable back fan blower type personal aerial work flying object in which an envelope (ball skin) can be automatically carried out and stored. It is sectional drawing of an envelope winder, a torch, and a burner. The figure on the left shows the tip cylindrical root spherical kerosene lamp squirt type envelope combustion prevention net lowered to the bottom when the envelope is stored. It is a figure. It is the elements on larger scale which looked at the backpack and the backpack peripheral device from the passenger | crew's left side. It is the elements on larger scale which looked at the state which the envelope winder rolled the envelope halfway from the passenger's left side. A view from the top of the truncated cone to the bottom to describe how to knit a bowl with a cone shaped side of the truncated cone that houses the ice cream cone shaped envelope is there. It is the figure seen from the side surface upper part of the truncated cone in order to describe the knitting method of the kite shape which accommodated the cone-shaped envelope of ice cream, and the side surface of the truncated cone used as the structure of an upper flying body became a bowl shape. Envelope (ball skin) is housed in ice cream cone-shaped jar. Suspension cable is inside the envelope. Hot air balloon, gas balloon, hot gas combined balloon, hot gas balloon, below ice cream cone-shaped jar It is the whole block diagram which looked at the personal aerial work flying object which can be moved up and down, front and back, and left and right with a propeller or fan which can project the beam in four directions and change the direction of the electric motor with a spherical hinge at the beam tip. Envelope (ball skin) is housed in ice cream cone-shaped jar. Suspension cable is inside the envelope. Hot air balloon, gas balloon, hot gas combined balloon, hot gas balloon, below ice cream cone-shaped jar It is the partial block diagram which looked at the personal aerial work flying object which can move the propeller or the fan which can project the beam in four directions and change the direction of the electric motor with a spherical hinge at the beam tip, and which can move up and down, front and back and right and left. Envelope (ball skin) is housed in ice cream cone-shaped jar. Suspension cable is inside the envelope. Hot air balloon, gas balloon, hot gas combined balloon, hot gas balloon, below ice cream cone-shaped jar A propeller or fan with a beam projecting in all directions and a spherical hinge at the beam tip that can change the direction of the electric motor. It is a figure which shows the place accommodated in the cone-shaped bowl of. Envelope (ball skin) is housed in ice cream cone-shaped jar. Suspension cable is inside the envelope. Hot air balloon, gas balloon, hot gas combined balloon, hot gas balloon, below ice cream cone-shaped jar It is the partial block diagram which looked at the personal aerial work flying object which can move the propeller or the fan which can project the beam in four directions and can change the direction of the electric motor with a spherical hinge at the beam tip, and which can move up and down, front and back and right and left. Envelope (ball skin) is housed in ice cream cone-shaped jar. Suspension cable is inside the envelope. Hot air balloon, gas balloon, hot gas combined balloon, hot gas balloon, below ice cream cone-shaped jar Cross section of the envelope of a personal aerial work flying object that can move up and down, front and back, left and right, with a propeller or fan that can project the beam in all directions and the direction of the electric motor with a spherical hinge at the beam tip It is a figure which shows that a suspension cable is wound up with the suspension cable winder under the cone-shaped bowl of ice cream. It is sectional drawing which shows a honeycomb structure, OX structure, a flex structure, a bisecting structure, and a feather structure. It is the figure of the cross section which made the shape like a sea urchin spine by the laser processing on the surface of resin or fiber reinforced resin, and vacuum-deposited the weather-resistant substance on it as needed. The part that is pulled by the material equivalent to the bamboo material of the bamboo basket that knits the cocoon member is the one that the steel wire is bundled into a bundle or the part that receives the compressive force knitted like a hand-knitted sweater is rigid with a honeycomb structure By arranging a flexible honeycomb structure around the honeycomb structure, members like this belt can bend flexibly and the middle of the honeycomb structure is fixed with fiber reinforced resin and epoxy resin as the base material of the belt The steel wire rods are those in which a rheological body that suppresses fatigue fracture is encased in a resin jacket or contained in a fiber reinforced resin. FIG. 2 is a cross-sectional view of an aircraft fuselage and exoskeletons of both wings in a skeleton like a kite woven with bamboo members using a belt member. You can see the floor and the wall that supports the floor under the ceiling and the wall that supports the ceiling. In order to conserve fuel, both wings are divided into a three-section wall-like skeleton, and the joints between the wings are reinforced with belt material. Reinforcement by aircraft fuselage and wings and fuselage and both wing belt members, and reinforcement by fuselage, tail wing, fuselage and tail wing belt members in a skeleton like a braid woven with bamboo members using belt members Can be seen. 1 is a cross-sectional view of an exoskeleton of an aircraft fuselage. The exoskeleton is wrapped like a bamboo basket with a belt member. The belt member is a bundle of wires bundled in parallel with each other, and has a honeycomb structure for receiving a compressive load. A buffer is visible on the inside and outside of the belt member. On the outside of the cushioning member, a fiber reinforced resin skin is visible and a piano wire or prestressed concrete steel wire net is visible in the skin. The inner surface of the fiber reinforced resin can be seen inside the buffer member. It is sectional drawing of the belt member which knits a fence like the bamboo of a bamboo basket. The tension portion is enclosed in the mantle with a rheological body that is bundled by assembling steel wires. The compression part has a honeycomb structure, and a flexible honeycomb structure such as a resin surrounds a rigid section such as a metal. In the middle you can see the substrate of fiber reinforced resin. A steel wire and a honeycomb structure are attached to the base material with an epoxy resin or the like. The belt member is strong and can knit the structure like a fold. From the analogy of H-shaped steel, it was found that sandwiching a honeycomb structure with a steel wire like a sandwich is more advantageous for deformation. This is called a sandwich belt member. This is a cross-sectional view of the outer wall of the aircraft, formed by knitting the shape of the aircraft with a belt member like a bamboo fence, and wrapping the skeleton like a fence with a belt member from inside and outside with shock absorbers on the outside A piano wire or prestressed concrete steel wire is embedded in the outermost skin where the fiber reinforced resin is bonded to the inside with an epoxy resin or the like to prevent the member from being shredded when the aircraft crashes into the ground. This piano wire or prestressed concrete steel wire counteracts the force of the aircraft expanding above. This metal net prevents lightning strikes. It is a figure which shows the relationship between an internal frame | skeleton, a propeller or a fan, and an electric motor in case the upper flying body of a personal aerial work flying object is a square pole. It is a figure which shows the internal skeleton in case the upper flying body of a personal aerial work flying object is a cylinder. It is sectional drawing of a horizontal member at the time of assembling the upper flying body of a personal aerial work flying object in a well beam. It is the figure which showed a mode that a hopper processed a weather resistance in all directions like a sucker of an octopus with a movable type vacuum hopper vapor deposition laser sintering lamination spray apparatus. It is sectional drawing which showed the mode of the inside of a movable-type vacuum hopper vapor deposition laser sintering lamination | stacking spraying apparatus. A cross-sectional view in which a resin is pressed into a wood conduit or a teacher's tube and cured to process the wood, then a number of holes are drilled like a honeycomb structure to reduce the weight, and then the periphery is covered with a fiber reinforced resin for reinforcement. It is. Plywood or laminated timber or the above-mentioned solid wood was reinforced with resin and innumerable holes were drilled and compressed into 1 to 3 atmospheres in an adhesive between wood and wood like a honeycomb structure Resin spheres such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 mm to 33 mm and a thickness of 0.195 mm to 3.3 mm encapsulated with air or gas are the shape of a small crushed egg grain The outer surface of the object cured by inserting and reducing the weight of the object by mixing and adhering the object is 3.3 mm to 195 mm in thickness with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin. It is sectional drawing of the thing hardened | cured by covering reinforcement. A sheet of paper such as corrugated cardboard, laminated with air and hardened with an adhesive, has a structure like a honeycomb structure, that is, a hexagonal or round hole like a hexagonal hole in the honeycomb structure. In order to reduce the weight by making a plurality of small holes such as hexagons or circles with a side of a hexagon or a diameter of about 1.95 mm to 33 mm in order to make a plurality of holes spaced at intervals of 33 mm to 33 mm A material whose surface is reinforced with foaming resin such as urethane foam or a paper-like small hole having a plurality of small holes of 19.5 mm to 33 mm in space, that is, a hexagonal hole in the honeycomb structure. Carbon fiber reinforced resin or glass is used after the outer surface of the foamed resin is reinforced with a metal or paper honeycomb structure. It is a cross-sectional view of what hardened coated reinforced at 195 millimeters thick 3.3 mm in fiber reinforced resin such as fiber reinforced resin. Shredded paper with a thickness of about 0.195mm to 3.3mm with a square or rectangular side cut into a corn flake shape with a size of about 1.95mm to 33mm or a shredder used in office work Add the air to the agitated paper and stir it to make the paper crumpled or wrap around the curled air, making it half soft and fluffy. The object with the paper fibers loosened is mixed with air together with an adhesive such as epoxy resin, stirred, compressed appropriately and solidified, and molded into a member with the required strength, and it has a cavity inside By adjusting the amount of adhesive, the required strength can be obtained, and the paper that has been cut into this cone flake shape and mixed with air is mixed with the adhesive. In order to reduce the weight after forming the compressed member in a mold, a small hole having a side of about 1.95 mm to 33 mm such as a circle diameter or a hexagon is spaced from 19.5 mm to 33 mm. In this case, a honeycomb structure similar to the honeycomb structure, that is, a hexagonal hole in the honeycomb structure is replaced with a circular hole, the outer surface is covered with foamed resin, and the outer surface is resin, fiber reinforced resin, paper or metal honeycomb. FIG. 3 is a cross-sectional view of a structure in which a structure is attached and wrapped and then the surface is covered and reinforced with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin at a thickness of 3.3 to 195 mm. 1 between the tape that is wound around and the tape that is wound from now on, with paper or fiber-containing tape or fiber reinforced resin or other film material tape wrapped around the material like a laver roll sushi in a cylindrical shape Pressure gas made of resin such as spherical or polyhedral polyethylene terephthalate having a diameter of 1.95 mm to 33 mm and a thickness of 0.195 mm to 330 mm enclosed with compressed air or gas of 3 to 1 atm. The object is like a small crushed egg particle shape with a number of children, or a sphere with a size of tennis ball to volleyball, or a polyhedron and fiber shape with a diameter of 0.195 microns to 3.3 mm A cotton-like product made of strong chemical fiber or natural fiber At the same time, an appropriate amount of adhesive such as epoxy resin is mixed, mixed with air, stirred, and the gap between the products filled with resin pressure gas is suitable for cotton-like fibers and adhesive such as resin. A layer of honeycomb structure made of paper, resin, or metal on the outer surface of a fiber reinforced membrane material tape or a commercially available tape and tape packed between air and filled with air. It is formed by bonding with an adhesive such as epoxy resin, and the outer surface of the honeycomb structure is 3.3 mm to 195 mm thick and coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin. It is sectional drawing. Spherical or polyhedral polyethylene terephthalate such as polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and encapsulated with compressed air or gas of 1 to 3 atmospheres is a numerator. A small crushed egg-like product such as the above and a fiber-like diameter of 0.195 microns to 3.3 millimeters of chemical fiber or natural fiber in the form of cotton are suitable. Mix the amount of adhesive such as epoxy resin and stir while containing air, and fill the gap between the objects filled with pressure gas made of resin with cotton-like fibers and resin or other adhesive containing moderately air The object was formed into the shape of a member, and it was wrapped with a white thin film that was an aggregate of eggs of a number of children as a result of hardening with moderate air containing adhesive. Before the adhesive is cured, an object that looks like an elongated lump of a number of children is put into a mold to form the required member shape, and the outer surface of the object that has been hardened with air is formed. FIG. 2 is a cross-sectional view of a product having a surface of 3.3 mm to 195 mm coated with a fiber reinforced resin such as a carbon fiber reinforced resin or a glass fiber reinforced resin after being wrapped in a honeycomb structure. It is made of foamed resin such as polystyrene foam or urethane foam, and is formed by adhering a honeycomb structure layer made of paper, resin or metal around the foamed resin with an adhesive such as epoxy resin. It is sectional drawing of the thing which carried out the coating reinforcement | strengthening with fiber reinforced resins, such as carbon fiber reinforced resin or glass fiber reinforced resin, from 3.3 millimeters to 195 millimeters. There is a method that uses a three-dimensional honeycomb structure such as a weir-ferran structure with a metal such as steel using a molten metal laminate forging fixation technique in a three-dimensional three-dimensional lamination technique. Electricity that can extrude the net-shaped laminated metal that can be poured into the molten metal to be laminated in a mesh shape of about 0.195mm to 33mm in height using a ceramic mold as in the case of printer lamination technology The lower surface of the ceramic mold that can maintain a high temperature below the melting point is a nozzle-shaped mold with a mesh-shaped cross section obtained by horizontally cutting the honeycomb structure to be molded, and the upper surface of the ceramic mold is a hopper-shaped ceramic mold The ceramic mold is horizontally lowered onto the production base using a small amount of molten steel or other metal, and a small amount of metal such as molten steel is poured from the top to the bottom with an inert gas. It is a cross-sectional view of a ceramic mold frame metal such quick withdrawal molten steel subjected to press-injection form the shape of a mesh of masses ceramic molding frame cold I. The method of exchanging multiple ceramic molds according to the type of each layer in the three-dimensional honeycomb structure is the same as the number of cut surfaces that are cut horizontally by the number of layers for repeating one unit of the basic structure of the honeycomb structure. A plurality of ceramic molds are continuously connected horizontally to form a strip, and the ceramic molds move up, down, front, back, left, and right while shifting the position of the ceramic molds up, down, front, back, left, and right. After casting the molten metal mold to be laminated, the ceramic mold is lifted, the ceramic mold is cleaned by vibration of the ceramic mold, the laminated metal surface is forged, and the laser cutting spine is processed. It is a figure which shows that the process of a series of flow work is automatable by shifting to the up and down, front and back, and right and left. Steel sheet laminating laser melt forging laminating technology is a method of forging formation after laminating metal sheets such as mesh shapes such as steel and laminating part of the laminating surface with laser technology like a 3D printer. A three-dimensional honeycomb structure that is virtually formed on the substrate is virtually placed, and the virtual three-dimensional honeycomb structure is cut by a horizontal plane in the first stage and punched to form a cross-sectional shape. A virtual three-dimensional honeycomb in a horizontal plane on the second stage on the first stage where a sheet of metal such as steel having a thickness of about 1.95 microns to 33 mm is placed on the production base. A sheet of metal such as steel having a thickness of about 1.95 microns to 33 millimeters in the shape of a cross section obtained by horizontally cutting the structure is punched. -A metal sheet such as steel that has been punched and sheared and placed in a second stage, and the second stage sheet is made into a second stage. The center of the mesh is melted by laser technology along the shape of the second stage sheet, and the upper and lower stages. This second stage of forging while keeping the solid shape by hitting the mesh of a metal sheet such as steel that has been melted and fixed to a suitable temperature after being melted and fixed with a mechanically driven computer controlled hammer On the top, a virtual three-dimensional honeycomb structure on the third horizontal plane is cut horizontally, and a sheet of steel with a thickness of about 1.95 microns to 33 mm thick is punched and sheared with a punching shear. Lay the center of the mesh with the laser technology along the shape of the mesh of this third stage sheet with a sheet of metal such as a steel sheet placed in the third stage, and the upper and lower sheets After fusing and fixing, the metal sheet of steel or other metal sheet such as steel that has cooled down to an appropriate temperature is hit by a mechanically driven computer controlled hammer with an appropriate hitting condition, and the forging is repeated by repeating this operation while maintaining the solid shape It is the figure which showed the steel sheet lamination | stacking laser fusion forging lamination | stacking technique more than the series of the flow work process which can be replaced by the layer of a metal sheet | seat while forging a typical three-dimensional structure. The vacuum deposition technique is to draw a figure using thin metal wires in the shape you want to deposit, and charge the thin metal wires as electrodes, and spread the vacuum deposited material on the opposite pole to the entire pole. The crucible lid in the shape of a crane neck flask is placed in close contact with a normal crucible that is prevented to melt and evaporate in the crucible that prevents the entire evaporation material from diffusing, and the tip of the crane neck is passed through a conduit having the opposite potential of the evaporation material There is a method of drifting the nozzle from the movable conduit by the diffusive power to evaporate the vapor deposition material led to the nozzle having the reverse potential of the vapor deposition material and reaching the target electrode from the nozzle. Also, move the crucible flask shaped crucible like a 3D printer Like a crane-necked flask-shaped 3D printer, it is selectively and intensively lowered from the nozzle-shaped vapor deposition material outlet at the tip of the crane neck directly above the target thin line and does not scatter to other parts. Vapor deposition controlled by a device such as a camera shutter with a small amount is deposited and deposited according to the shape of the electrode of the thin wire to be charged by concentrating and depositing the vapor deposition material on the target thin wire at the top with electrostatic force and laminating the thin wires. The method of forming a three-dimensional solid shape by a vacuum vapor deposition material or using conductive ink instead of a target thin line is to draw a vapor deposition target figure like a three-dimensional printer and charge the figure to the figure. By vacuum-depositing in a manner and drawing a figure to be laminated like a three-dimensional printer on the target figure so as to laminate further, charging the figure and intensively vacuum-depositing from the top on the top figure to repeat this process It is the figure which showed that the laminated three-dimensional structure by a vacuum evaporation material can be formed. The method of applying silver clay technology to three-dimensional lamination is to use ink containing a fine powder of metal to be laminated with oily or water-soluble air contact hardener on paper or resin fiber nonwoven paper. Draw a figure you want to laminate on paper or resin fiber nonwoven paper placed on the manufacturing base like a 3D printer, and add another sheet of paper on the figure you want to laminate like a 3D printer Adjust the amount of ink so that the curable ink containing fine metal powder penetrates between the fibers of the paper and the ink of the upper paper and the lower paper fits in, and shapes it with a printer like a three-dimensional printer Draw a figure with a curable ink containing fine metal powder that you want to laminate and laminate the paper on this paper. This is repeated to obtain a product in which paper or resin fiber nonwoven paper is laminated and cured. With paper or tree The purpose of using paper or resin fiber non-woven paper to obtain a three-dimensional structure by burning fiber non-woven paper to sinter-bond the metal is to reduce the lamination time, ensure the width of the ink, and smooth the surface of the method of three-dimensional lamination For this reason, by printing a plurality of spot-like dots at fixed positions around the figure to be laminated, when the bundle of paper is cured, the point group is laminated and cured into a columnar shape to form a laminated bundle of paper. The above is a cross-sectional view showing a new three-dimensional lamination technique, in which the shape is protected until it is sintered and the cured paper bundle can be easily transported. Denture manufacturing method applying beam theory on elastic floor is silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part metal ceramic composite laminated denture manufacturing method description, silicon rubber sucker layer shock absorbing layer honeycomb Structure layer Fiber resin layer Interlocking part Metal ceramic composite laminated denture manufacturing method is to place the gypsum gums on the gypsum male mold manufacturing base around the gums and the base of the gums in the human oral cavity The method of laminating from a soft resin to a hard resin on which the release material layer is sprayed on the male mold is a method of laminating the beam on the elastic floor so that when the force is applied by engaging the denture, the force is applied to the entire gum. The first layer in which the denture contacts the gums is a medically safe silicone rubber sucker layer on top of which foam urethane is applied. A relatively thin fiber having a thickness of about 1.95 millimeters to 3.3 millimeters made of a fiber reinforced resin on a honeycomb structure provided with a honeycomb structure layer as an intermediate layer on a stress buffer layer as a simple stress buffer layer Denture surface layer made of reinforced resin, and fiber reinforced resin is a fiber reinforced resin, and only the meshing portion of the top end of the tooth is a metal having a thickness of about 0.195 mm to 3.3 mm or Sintered metal, metal ceramic, porcelain, ceramic, or a composite of these metals and ceramics. The dentures as a whole are 0 except for the part that is engaged when pinched with a finger like a mouthpiece made of resin, metal, and ceramic. .Since it is soft enough to move from 195mm to 0.33mm, the joint part is hard and resin part at the same time It has a stress buffer layer with a shock absorber that can transmit force to the fiber reinforced resin through the honeycomb structure when the force is applied to the denture with dentures that can be peeled off. The surface of the denture inside the dentures of medical foamed resin is made of medical silicone rubber and has good adhesion, and the gums eliminate the air inside the dentures, making it a structure that sucks into the gums just like a sucker. It is a structure that does not hurt due to the fragments of teeth entering between the gums and dentures, and only the meshing part becomes a metal or ceramic or metal-ceramic composite that forms a complete meshing tooth shape by laser cutting technology Then, the resin of the meshed portion is processed like sea urchin spine as described in the claims, and the necessary amount of titanium is deposited or bitten. This is a plugging device in which adhesive is applied to the surface and titanium powder is applied to the surface and the surface of the denture is sintered by laser technology, or only the meshing part is made of titanium in a thin horseshoe shape and fiber reinforced resin is returned to the center of the teeth. It is possible to fix using an adhesive. Shock absorbers are placed on the back of the shape memory alloy that is covered with resin so that the upper and lower dentures can move softly at the end of the dentition and memorized at the spring or body temperature along the temporomandibular joint. A metal material covered with resin or shock absorbing material made of steel or a spring material or a shape memory alloy whose shape is memorized at body temperature is embedded in the denture and the denture is made into the palate with saliva viscosity Functionality that gently softens the adhesive force with the restoring force of the metal, stabilizes the denture in the palate, and infiltrates the denture resin with a medical effect or refreshing substance Dentures are included in this method, and strong, light and tough hard objects that do not hurt even when chewed can be manufactured. Structure layer Fiber resin layer Metallic ceramic layer Metal and resin that stabilize dentures on the top and bottom, shock absorber and silicon rubber sucker layer are manufactured separately and assembled using a medical adhesive such as epoxy resin. The above is a laminated cross-sectional view showing a method for manufacturing a metal-ceramic composite laminated denture of a silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing portion, which is to be included in the claims. Silicone rubber sucker layer Shock absorption layer Honeycomb structure layer Fiber resin layer Intersection metal ceramic composite Laminate metal that gently stabilizes dentures on the upper and lower sides of the denture. It is the figure which showed that. It is a figure which shows the layer only of the meshing part made from the metal, porcelain, or ceramic safe for medical use. It is a cross-sectional view showing that there is a method in which the internal space, which is a cross-sectional view of a sandwich belt member-extraskeletal spherical flying object, is used for multiple purposes and is used in multiple stages on a honeycomb structured floor. The exoskeleton sphere shaped flying object for sandwich belt member application has a configuration in which the head, both wings and tail are attached to the spherical passenger part, and it is about the size of a jumbo jet (registered trademark) and the wide space inside the sphere is This method, which is used for multiple purposes and can support multiple honeycomb floors with a cocoon-shaped wall and floor, can be used for multiple purposes because the interior of the wing can take a large space. It is an external view of the exoskeleton formed in the shape. As an application of a sandwich belt member, a thick flying fish model gains overall lift.The flying object simulates a thick flying fish with a skeleton-like exoskeleton, and the flying object has a rounded trunk like a goldfish and both thick wings are Bernoulli theorem 1 is a cross-sectional view of the fuselage body of this flying object that produces a lift by generating a pressure difference between the upper and lower parts of the entire flying object. As an application of a sandwich belt member, a thick flying fish model gains overall lift.The flying object simulates a thick flying fish with a skeleton-like exoskeleton, and the flying object has a rounded trunk like a goldfish and both thick wings are Bernoulli theorem The entire flying object has a structure like a cross section of a wing, and the fuselage of this flying object that obtains lift by generating a pressure difference between the upper and lower parts is cut in the direction in which the flying object travels. As an application of a sandwich belt member, a thick flying fish model gains overall lift.The flying object simulates a thick flying fish with a skeleton-like exoskeleton, and the flying object has a rounded trunk like a goldfish and both thick wings are Bernoulli theorem The entire flying object has a structure like a cross section of the wing, and the flying object that produces lift by generating a difference in pressure between the upper and lower parts is knitted into a saddle shape using a sandwich belt member. FIG. As an application of a sandwich belt member, a thick flying fish model gains overall lift.The flying object simulates a thick flying fish with a skeleton-like exoskeleton, and the flying object has a rounded trunk like a goldfish and both thick wings are Bernoulli theorem The entire flying object has a structure like a cross section of a wing, and the fuselage of this flying object that obtains lift by generating a pressure difference between the upper and lower parts is cut in the direction in which the flying object travels. At the tail of this flying object, a forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine is used to obtain rotational force, and a forced air-cooling whole heat-dissipating fiber-reinforced resin metal composite rotor permanent magnet stator electric coil disk stacked electric motor as a generator A flying object that simulates a thick flying fish can move forward by sending wind backward with a bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor using that power after obtaining power with the method used It is the figure which showed that. It is the figure which attached the bird strike prevention device fiber reinforced resin metal composite turbine lamination type electric motor to the tip of both wings of the flying object which acquired thick flying fish simulation whole lift. It is the figure which attached the bird strike prevention device fiber reinforced resin metal compound turbine lamination type electric motor to the body tail of the thick flying fish simulated whole lift acquisition flight object and the horizontal tail tip. It is the figure which attached the bird strike prevention device fiber reinforced resin metal compound turbine lamination type electric motor to the both wing tip of the thick flying fish simulation whole lift acquisition flight object, the fuselage tail, and the horizontal tail tip. Sphere center disc outer periphery plural duct fan disc outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast suspended fallable flying object is a cross-sectional view cut by a plane orthogonal to the traveling direction of the flying object. FIG. 3 is a cross-sectional view of a wing-shaped portion of a disk around a sphere of a flying object that can be dropped by hanging a fuel generator ballast suspended by a parachute installed fuel generator ballast, a wing-shaped part of the outer periphery of a sphere center disk, a plurality of duct fans, and a disk. FIG. 5 is a cross-sectional view of a flying object that can be suspended from a fuel generator ballast suspended horizontally at the center of the disk. Sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging dropable flying object The parachute is opened at the time of falling, and the opening of the upper part of the parachute is opened with a wire at the time of falling to induce the fall of the spherical disk, so that it falls down like a fluttering leaf and a leaf flies and relaxes the collision with the ground. is there. This contains a float that spreads like an air bag when it touches the sea. Sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging dropable flying object The parachute is opened at the time of the fall, and the mouth of the upper part of the parachute is opened with a wire at the time of the fall. It is a figure of a spherical disk dancing in the air as a leaf of the tree dances in the air. The bottom of the sphere has a structure that allows heavy loads such as generator fuel to be hung at the bottom like a ballast tank, and when the airflow is bad, the heavy parts such as the ballast generator and fuel are suspended below This ballast part that lowers the center of gravity and prevents the entire disk from rotating to the top and bottom has a structure that can be dropped separately from the spherical disk body in a safe position to reduce the weight when falling. It is the figure which showed the thing which relieve | moderates the impact at the time of the fall by providing the impact-absorbing layer in the part of the ball | bowl from which the lowermost periphery of this ball | bowl which can be suspended was cut off. Sphere center disc outer periphery Multiple duct fan disc outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging dropable flight object spherical disc outer left and right sides are processed into wing shape and both left and right wings are elongated longer FIG. FIG. 4 is a cross-sectional view of a wing of a disk portion of a flying object that can be dropped by hanging a fuel generator ballast suspended by a parachute installed fuel generator ballast, a part of the outer periphery of a sphere center disk, and a plurality of duct fans. The duct engine has a structure in which a plurality of duct engines are blown and floated on the outer periphery of the disc part, and a cross-shaped beam is provided in the middle of the cylindrical height, and two rotary engines are arranged above and below the center of the cross. Forced air-cooling of engine or twin-type horizontal piston General heat-dissipating fiber reinforced resin-metal composite internal combustion engine is fixed, and the upper and lower fans are duct fans that rotate inside a cylindrical shape. It is sectional drawing of the duct fan which obtains floating force with a fan. The duct engine has a structure in which a plurality of duct engines are blown and floated on the outer periphery of the disc part, and a cross-shaped beam is provided in the middle of the cylindrical height, and two rotary engines are arranged above and below the center of the cross. Forced air-cooling of engine or twin-type horizontal piston General heat-dissipating fiber reinforced resin-metal composite internal combustion engine is fixed, and the upper and lower fans are duct fans that rotate inside a cylindrical shape. It is the figure which looked at the duct fan which obtains floating force with a fan from the upper part. In the enlarged view of the sectional view of the sandwich belt member, a honeycomb structure in which wires such as front and back steel wires are bundled in parallel is a belt member for knitting a ridge structure fixed with an epoxy resin or the like. It is sectional drawing of the fuselage | body of the flying object which has the exoskeleton which knitted the sandwich belt member like the bamboo basket. The waterproof and airtight zipper is waterproof and airtight and has a thickness of about 0.195mm to 3.3mm thicker than the two underlying fabrics in order to prevent the fabric from getting into the zipper. Resin fins with a width of about the size of the seam and a length of about the length of the zipper are two on the back, the front, and a total of four zipper seams. When the zipper is sewn one by one and the zipper is pulled up, the fabric prevents the cloth from biting into the zipper, and the part where the fins that cover the zipper from the zipper seam on both sides of the zipper overlap the fin The back and front of the zipper are tightly sealed with resin or rubber-based resin, so that the fabric is zippered even if the zipper is pulled up rapidly Kamikomu it is airtight waterproof internal simultaneously zipper can be pulled pulling the lightly zipper no, or a cross-sectional view of a zipper not catch waterproof and airtight. It is a front view of the sandwich belt member kite exoskeleton of a ray simulated flying object. It is a side view of the sandwich belt member kite exoskeleton of a ray simulated flying object. It is a top view of the sandwich belt member 籠 knitting exoskeleton of a ray simulated flying object. It is an upper external view of the ray simulated flying object. It is a lower whole external view of a ray simulated flying object. It is the whole front external view of a ray simulated flying object. It is the whole back external view of a ray simulation flying object.

The personal airborne flying object has an aircraft weight of 19.5 kg to 33 kg, a loaded human 19.5 kg to 66 kg, a flight altitude of 19.5 m to 33 m, a flight time of 19.5 minutes to 33 minutes, and a cost of 19. It is about 50,000 to 330,000 yen. Flight technology can also be applied to large passenger aircraft. Invented the safety of the sky and the silence of the sky. Here, in order to clarify the invention, one or two of the items of the claims which record the claims, the personal aerial work flying object has a structure simulating the seeds of dandelions flying in the sky, From here, it is a description of the light and strong material of the personal aerial work flying object, the material form of the material of the personal aerial work flying object is equivalent to an amino acid, which has a structure simulating a chemical structural bond model of protein Primary, secondary, tertiary, and quaternary binding side of proteins in which basic structures such as metal, resin, and fiber reinforced resin form a three-dimensional structure by binding with multiple branches such as peptide bonds Chain conformation domain (conformation) motif (super-secondary structure) computerized dynamics to form various forms of folds (folding) like fold proteins In this patent claim, there is a method using a cutting three-dimensional modeling technique or a three-dimensional three-dimensional lamination technique to determine and manufacture a three-dimensional structure in consideration of a tension member and a compression member so as to satisfy mechanical requirements by mechanical mechanics analysis. The term “honeycomb” used means a broadly defined honeycomb structure such as a weir-ferran structure, and is a fiber reinforced object that includes a hexagonal honeycomb structure, an OX structure, a flex structure, a bisecto structure or a feather structure. The term “resin” is defined as a term that refers to carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin, etc.In this claim, a honeycomb structure and fiber reinforced resin are used extensively to realize a flying object for personal aerial work. Used in the scope of the present invention in which the invention of a laminated composite material of light weight and toughness was invented The term flying object is defined as an object flying in the air, and the techniques and materials of personal aerial work flying objects are applied in various fighters, passenger planes, helicopters, airships, spacecrafts, satellites, space stations, etc. A simple method for weathering a personal aerial work flying object according to the present invention may be applied to a steel surface according to the present invention. A plurality of sea urchin spines at intervals of about 3.3 nanometers to about 1.95 millimeters in diameter and about 3.3 nanometers to about 1.95 millimeters in height and about 3.3 nanometers to about 1.95 millimeters by the method described above. Weather-resistant resin, which is a method of vacuum-depositing titanium, aluminum, or glass on this surface, uses laser technology on the surface of epoxy resin, etc. Use multiple lasers with multiple thicknesses and depths from 3.3 nanometers to 1.95 millimeters, and use a square surface with square sides from 3.3 nanometers to 1.95 millimeters as seen on the grid. A plurality of sea urchins are cut at intervals of 3.3 nanometers to 1.95 millimeters and 3.3 nanometers to 1.95 millimeters in height and 3.3 nanometers to 1.95 millimeters. Lasers are formed by laminating layers of metal or glass such as titanium or aluminum alternately on the surface of an object processed like an elongated barb or by laminating a single material to form a film and vacuum-deposited film The weather-resisting tree is made by increasing the weather resistance of the resin by filling the part cut out by the technology to the extent necessary for weather resistance to create a layered film that is anti-oxidation and UV protection in an amorphous state. This method can be used for weathering surface treatment of civil engineering structures such as steel, tools, machines, automobiles, reinforced concrete, etc. There is a movable vacuum hopper vapor deposition sintered laminating spray device that can be used for surface processing of flying objects instead of painting. The problem of peeling between layers in the layered method, in which the electrostatic coating is applied in combination with the laser technique, replacing the baked part of the electrostatic coating, is eliminated by cutting technology like sea urchin spines. Using a device that has a larger octopus suction cup, the weather-resistant substance is made into fine powder and mixed with the adhesive solvent liquid to the processed surface. There is a method of fixing from the slip to the spray processing surface and baking by the method described in the scope of claims of the present invention, or a crucible of a normal vacuum vapor deposition device with a gimbal structure and a vacuum vapor deposition direction of 360 degrees is possible. Possible vacuum hopper atom atom implantation spray deposition powder electrostatic transport laser welding sintering laser cutting spine laminating method surface weathering processing method creates a vacuum in the hopper and has a movable base of 195mm to 3300mm without bottom Using a square or conical funnel-shaped hopper, the bottom of the hopper is made of silicon-based resin or rubber-based resin along the bottom of the hopper so that it can be kept airtight. Attach the bottom of the square or cone of the hopper to the surface you want to weatherproof so From the top of the square or cone to the bottom processing surface after emptying, using laser technology like a CRT electron gun, spraying weather resistant fine particles from the nozzle at high pressure for surface processing Electrostatically transport the charged atoms, molecules, or fine particles necessary for weather resistance and transport them to the processing surface where you want to ensure the weather resistance, or electrically move the atoms, molecules, or fine particles as if they were an electron gun. The particles are charged and accelerated using an electric field, and laser processing is performed like a scanning line electron on the scanning surface of a cathode ray tube of an electron gun to weld and fix a weather-resistant substance on the processing surface. Alternatively, the electrostatically transported material is welded or sintered on the surface that needs to be processed, such as the movement of electrons in the scanning line, using laser technology, or a weather-resistant material with a gimbal crucible There is also a powder electrostatic transport laser welding sintering method in which the weathering substance is fixed and fixed on the work surface by evaporating and electrostatically transporting the material. There is also a vacuum deposition method as a method of bonding to the weather-resistant processed surface for performing the process, and a fine powder ultrasonic wave in which the size of the resin or metal charged on the surface to be weather-resistant processed is about 3.3 nanometers to 0.195 millimeters. The size of the resin layer or metal layer is formed by the method of electrostatically transporting to the processing surface while diffusing by vibration, melting the surface of the resin layer or metal layer with laser technology, and welding and fixing or sintering. 3.3 Nano to 0.195 millimeters of charged fine fiber fragments are electrostatically transported to the processing surface to form a fiber layer, on which a resin layer or Using a laser technique on the surface of the resin or metal layered by forming a metal layer, a plurality of grooves with thicknesses and depths of about 3.3 nanometers to about 0.195 millimeters are cut, and each side of the square seen by the grid is 3 A square surface of about 3 to 1.95 millimeters is cut by laser technology and cut to a diameter of about 3.3 to 1.95 millimeters and a height of about 3.3 to 1.95 millimeters. An object like an elongated sea urchin of a sea urchin is processed into a plurality of square surfaces at intervals of about 3.3 nanometers to 1.95 millimeters, and the amount of titanium or aluminum metal necessary for weather resistance is formed on the plurality of spines. A glass crucible is melted in a crucible with a gimbal structure. The crucible is heated in an electric furnace to evaporate the weathering material and vacuum-deposit the processed surface to charge the vapor of the weathering material to create a vacuum space. The laser-barbed processing is performed directly on the base of the structure, which is a method of vacuum-depositing the weather-resistant processed surface inside the removable hopper and performing weather-resistant processing on the surface of resin, fiber reinforced resin or metal. This method, including the method of vapor-depositing active substances, can be applied not only to flying objects but also to existing structures. The above series of processes can be automated robot construction. The application of the laminated honeycomb structure fiber reinforced resin composite technology of the personal aerial work flying object described in this claim, which is a description of the light and tough material, can be applied to the denture manufacturing method applying the beam theory on the elastic floor From here, the silicon rubber suction layer, the shock absorbing layer, the honeycomb structure layer, the fiber resin layer, the meshed part, the description of the metal ceramic composite laminated denture manufacturing method, Layer impact absorption layer honeycomb structure layer fiber resin layer mesh part metal ceramic composite laminated denture manufacturing method is placed on the gypsum male mold manufacturing base around the gums and gum roots in the human oral cavity Spraying a layer of medically safe release material onto the gypsum gum mold from the top to the layering method of laminating from a medically safe soft resin to a hard resin is when the denture is subjected to force by meshing The first layer where the dentures contact the gums is a medically safe silicone rubber sucker layer on top of it that uses the theory of beams on the elastic floor to make the force spread over the gums. A relatively thin layer of 1.95 mm to 3 made of a fiber reinforced resin is provided on the honeycomb structure by providing a honeycomb structure layer as an intermediate layer on a stress buffer layer such as urethane foam. Denture surface layer made of fiber-reinforced resin that is safe for medical use with a thickness of about 3 millimeters. The fiber-reinforced resin is made of fiber-reinforced resin and only the meshed portion at the top end of the tooth is 0. Medical-safe metal, sintered metal, metal ceramic, porcelain, ceramic, or a composite of these metals and ceramics with a thickness of about 195 mm to 3.3 mm, and the dentures as a whole are resin, metal, and ceramic This is a denture that is soft enough to move about 0.195mm to 0.33mm when the fingers are pinched with a finger like a mouthpiece made of When a force is applied to the denture, the shock absorber passes through the honeycomb structure and transmits the force to the fiber reinforced resin. A denture with a stress buffer layer made of shock absorbing material that can distribute force to the body, and the inner surface of the denture of the medical foamed resin has good adhesion with medical silicone rubber, and the gums eliminate the air inside the denture and sucker The metal that forms a complete meshing part tooth shape with laser cutting technology that has a structure that sticks snugly to the gums and has a structure that does not hurt, such as a piece of rice cracker entering between the gums and dentures Alternatively, the ceramic or metal-ceramic composite is formed only by the engagement portion, and the resin of the engagement portion is processed on the resin that is safe for medical use by processing the sea urchin spine described in the claims. Deposit the necessary amount of safe titanium for medical use or apply an adhesive to the joint and apply titanium powder to sinter the denture surface with laser technology. It is possible to use only a thin horseshoe shape made of titanium and a fiber reinforced resin with a fiber reinforced resin with a return at the center of the teeth to fix it using an adhesive so that the upper and lower dentures can move softly to the end of the dentition Steel or spring material or shape memory alloy in which shape is memorized at body temperature, which is covered with resin and has a shock absorbing material attached to the back of a shape memory alloy memorized at temperature or body temperature that is safe for medical use A metal material covered with resin or shock absorbing material of wire rod or plate material is embedded in the denture and the force to attach the denture to the palate with the viscosity of saliva is gently supplemented by the restoring force of the metal, and the denture is stabilized in the palate Penetration of a medically safe substance for medical use, such as a diabetic drug that must be taken regularly under the guidance of a doctor, or a substance that refreshes the mood This functional rubber denture is included in this method, and it is possible to produce a comfortable functional denture that is comfortable, strong, light and tough and hard to bite. Shock absorption layer Honeycomb structure layer Fiber resin layer Interlocking metal Ceramic layer Manufacturing of metal, resin, shock absorber and silicon rubber sucker layer that stabilize dentures on the top and bottom, and assemble with medical adhesives such as epoxy resin The method is also included in the scope of the present patent claims, and the above is a description of the silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part metal ceramic composite laminated denture manufacturing method, from here on wood and paper The surface of the honeycomb structure made of resin, foam resin, etc.










Reinforced with fiber reinforced resin


As a flying structure, solid wood conduits and mentor pipes are filled with curable resin to strengthen the wood, and then a hexagonal side of the honeycomb structure is 1.95. Hexagons of millimeters to about 33 millimeters or circles having a diameter of about 1.95 millimeters to 33 millimeters and a plurality of small holes at intervals of about 1.95 millimeters to 33 millimeters. Products whose pores are filled with foaming resin such as urethane foam and reinforced with a thickness of about 1.95 to 33 mm, or whose outer surface is reinforced with fibers such as carbon fiber reinforced resin or glass fiber reinforced resin instead of urethane foamed resin. Products hardened by resin reinforcement with a thickness of 1.95mm to 33mm, plywood or collection 19 is a hexagonal shape with a side of about 1.95 millimeters to 33 millimeters or a circle with a diameter of about 1.95 millimeters to 33 millimeters by reinforcing a solid wood or solid wood described in the claims with resin. Compressed air or gas of 1 to 3 atm was enclosed in an adhesive between wood and wood in a wood structure with a plurality of holes spaced at intervals of 5 to 33 millimeters Resin spheres such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 3.3 millimeters can be mixed with a small number of small crushed egg grains. The outer surface of an object that has been cured by adding air to the object that has been reduced in weight by bonding with resin. Bonded with fiber reinforced resin, such as carbon fiber reinforced resin or glass fiber reinforced resin, with a thickness of 3.3 mm to 195 mm coated and reinforced, or paper such as corrugated cardboard laminated and bonded with air In order to make a structure hardened with an agent into a structure like a honeycomb structure, that is, a hexagonal hole or a round hole like a hexagonal hole in a honeycomb structure in a corrugated cardboard at a distance of 19.5 mm to 33 mm. One of the sides of a square or a circle with a diameter of about 1.95 to 33 millimeters, such as hexagons or circles, with a plurality of small holes to reduce the weight, and the surface of the object reinforced with foaming resin such as urethane foam or paper A honeycomb structure such as a honeycomb structure in which a plurality of small holes are provided with a plurality of holes spaced from 19.5 mm to 33 mm. Thicken fiber-reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin after the outer surface of foamed resin reinforced by replacing hexagonal hole of structure with circular hole is wrapped with metal or paper honeycomb structure 3.3mm to 195mm coated and reinforced, or paper with a thickness of about 0.195mm to 3.3mm, square or rectangular sides of 1.95mm to about 33mm A piece of food that is cut into a corn flake shape or shredded with paper shredded for use in offices is mixed with air and stirred to make the paper crumpled or wrap up with curled air. After half of the fluffy paper fibers are loosened, this half is soft and fluffy. The molded object is lightly mixed with an epoxy resin or other adhesive, mixed with air, and then compressed and solidified to form the required strength. There is a cavity inside and the amount of adhesive is adjusted. The diameter of the circle to reduce the weight after forming the compressed material by mixing the paper and the agglomerated into the cone flakes, mixed with agitated paper and adhesive, which has the required strength Alternatively, a hexagonal hole having a side similar to a honeycomb structure by opening a plurality of small holes each having a side of about 1.95 mm to 33 mm at intervals of 19.5 mm to 33 mm, that is, a hexagonal hole in the honeycomb structure is a circular hole. After the outer surface is covered with foamed resin, the resin or fiber reinforced resin or paper or metal honeycomb structure is attached to the outer surface and wrapped. There is a method of using a material obtained by covering and reinforcing the surface of the material with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin at a thickness of 3.3 to 195 mm as a member of the flying object, or paper or A tape of fiber material or fiber reinforced resin or other membrane material is rolled into a cylindrical shape with nori sushi rolled, with the material sandwiched between the tape and the tape to be wound from 1 atm. A product in which pressure gas made of resin such as spherical or polyhedral polyethylene terephthalate having a diameter of 1.95 to 33 mm and a thickness of 0.195 to 330 mm in which compressed air or gas of 3 atm is enclosed is enclosed. Something like a small crushed egg grain shape or about a tennis ball A ball or polyhedron with a size of from about volleyball to a polyhedron and a cotton or other chemical fiber or natural fiber with a pulling force of about 0.195 microns to 3.3 millimeters in diameter. Mix an appropriate amount of an adhesive such as epoxy resin, mix it with air, and stir it. The gap between the resin-filled pressure gas will be filled with cotton-like fibers and an adhesive such as resin containing appropriate air. A honeycomb-structured layer made of paper, resin or metal on the outer surface of a fiber-reinforced membrane material tape or a commercial tape and a tape that is packed with air and solidified with air. The outer surface of the honeycomb structure is 3.3 mm to 195 mm and covered with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin. Use a cover reinforced material, or the structure of the flying body is made of paper, incombustible paper, aramid paper, resin or metal honeycomb structure, and the outer surface of the honeycomb structure is carbon fiber reinforced resin or glass fiber reinforced resin, etc. There is a method of using as a member a material which is reinforced by coating and reinforcing with a fiber reinforced resin of 3.3 to 195 mm, or a diameter 1 in which compressed air or gas of 1 to 3 atm is enclosed Resin spheres such as .95 mm to 33 mm thick 0.195 mm to 3.3 mm spherical or polyhedral polyethylene terephthalate have a small crushed egg grain shape and a fiber diameter of 0. A tensile force of 195 microns to 3.3 millimeters Mix together materials made of cotton or natural fiber together with an appropriate amount of an adhesive such as epoxy resin and mix with air to stir the gap between the materials filled with resin pressure gas. An article filled with cotton-like fibers and an adhesive such as a resin that contains moderately air is formed into a shape of the member, and the air is moderately contained with an adhesive and hardened as a result. Before the adhesive is cured, an object that looks like an elongated lump of a small number of children wrapped in a thin film is put into a mold to form the necessary members, and air is formed. The outer surface of the object that has been cured is wrapped with a honeycomb structure, and the surface is coated with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin with a thickness of 3.3 to 195 mm as a member. There is a method to use, there is Is formed by forming the center member of the flying body with foamed resin such as polystyrene foam or urethane foam, and bonding the honeycomb structure layer made of paper, resin or metal around the foamed resin with an adhesive such as epoxy resin. The outer surface of the honeycomb structure is 3.3 mm to 195 mm in thickness and coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin, or compressed air of 1 to 3 atm or Gas encapsulated resin spheres such as polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 330 millimeters, such as polyethylene terephthalate, are small crushed egg grains or tennis balls A sphere with a size from about 1 to about volleyball Or the polyhedron and the fiber diameter of 0.195 micron to 3.3 millimeter size chemical fiber or natural fiber like cotton and mixed with an appropriate amount of adhesive and mixed with air. In the space around the sphere or polyhedron with agitated material, chemical fiber cotton and adhesive material is filled with air and stirred and filled with air and hardened with paper, resin or metal around this outer surface The resulting honeycomb structure layer is formed by bonding with an adhesive such as an epoxy resin, and the outer surface of the honeycomb structure is 3.3 mm to 195 mm in thickness and is reinforced with a fiber such as carbon fiber reinforced resin or glass fiber reinforced resin. There is a method of using a resin-coated or reinforced material or a honeycomb structure made of paper, resin, or metal alone as a member of a flying body. The above is wood, paper, resin, foamed resin, etc. This is a description of the material of the resulting honeycomb structure reinforced with fiber reinforced resin, and the above is a description of a light and tough composite material. From here, it is a description of the safety and structural reinforcement of the flying object or aircraft, There is a method in which the above composite materials are combined and used as a member of an air vehicle. For the reinforcement of the surface of these air vehicle members or for lightning protection measures, a piano wire having a diameter of 1.95 mm to 33 mm or a steel wire for prestressed concrete is used. After embedding a net and applying tensile force (pre-tension) in advance, the fiber resin is cured, and then the stress is controlled with a computer using a strain gauge or the like on a steel wire for piano wire or prestressed concrete. And bulge force and ano wire or steel for prestressed concrete This method of suppressing the expansion of the aircraft in the sky by antagonizing the pretension expansion force, which is the pre-tensioning force of the wire rod, is a way to prevent the aircraft or aircraft from colliding with the ground Piano wire or prestressed concrete steel wire mesh prevents tearing apart and ensures passengers' living space in the event of a crash. The flight structure is iron, steel, aluminum, stainless steel, titanium, or ultra-lightweight There is a method of using a member made by rolling forging or extruding metal such as general-purpose magnesium alloy or using a member manufactured by molten metal lamination forging fixation technology. Weirs made of metals such as steel using molten metal lamination forging fixation technology There is a method of using a framework structure of a three-dimensional honeycomb structure such as a gellan structure, and the molten metal lamination forging and fixing technique uses a ceramic mold as in the lamination technique of a three-dimensional printer, and the height per layer is 0.195. The bottom surface of the ceramic mold that can keep the high temperature below the melting point with the electricity that the molten metal that the molten metal you want to stack in the mesh shape of millimeters to about 33 millimeters can flow in can be extruded horizontally. A ceramic mold with a mesh-shaped nozzle mold with a cut cross section and an upper surface of the ceramic mold with a hopper-shaped mold is horizontally lowered onto the production base, and one layer above it. With a device that lowers the molten metal drop and comes into close contact with the ceramic mold, increasing the pressure of the inert gas and performing one more injection A small amount of metal such as molten steel is poured in, and injection injection is performed from the top to the bottom with an inert gas. The metal is rapidly drawn up and the molten steel is cooled and solidified, and is drawn on the production base according to the shape of the ceramic mold form. The mesh shape to be laminated with a machine-driven computer-controlled hammer that has been adjusted to the extent that the mesh shape is slightly thickened with a metal such as steel with a mesh shape that is laminated is forged while retaining the three-dimensional shape. The thickness and depth of the grooves are adjusted to be slightly thicker on the premise of forging, and the thickness and depth of the plurality of grooves on the upper surface of the forged metal are changed from 3.3 nano to 0.3 by using laser technology. Cutting a 195mm groove into multiple squares with a square side of 3.3nm to 1.95mm on one side of the grid. Long spines have a diameter of about 3.3 nanometers to 1.95 millimeters and a height of about 3.3 nanometers to about 1.95 millimeters and are cut like multiple spines at intervals of about 3.3 nanometers to about 1.95 millimeters. Ceramic molds that have been laser processed and pulled up give high frequency vibration and extra gold













After cleaning the remaining genus of the genus, the ceramic mold is lowered onto the forged mesh-shaped metal layer, a small amount of molten metal is poured into it, and press-injection with an inert gas is performed. After that, the tip of a plurality of elongate barbs laser-processed to the above dimensions is poured into the metal in the shape of the grid, and then the spines are melted by the heat of the molten metal and some of the barbs melt into the next layer. By adhering to each other, the previous layer and the next layer are fixed, and the fixed upper layer is forged with a machine-driven computer-controlled hammer that adjusts the striking condition, and the surface is forged by laser technology on the surface. Repeating this series of operations to change the ceramic formwork by repeating this series of operations that cuts the grid by size and forms multiple elongated barbs in the grid and improves the bite with the next molten metal It is possible to obtain a three-dimensional honeycomb structure made of forged steel such as weir ferran structure made of metal such as forged steel, etc. With conventional lamination technology, the laminated part is peeled like bamboo fiber The method of exchanging multiple ceramic molds according to the type of each layer of the three-dimensional honeycomb structure, which eliminates the problem of damage caused by biting, sticking and forging by the sea urchin spines on the laminated surface Is a ceramic molding mold as a band by continuously connecting a plurality of ceramic molding molds horizontally by the number of cut surfaces horizontally cut by the number of repeating one unit of the basic configuration shape of the honeycomb structure The ceramic mold was moved up, down, front, back, left, and right while shifting the position of the top, bottom, front, back, left, and right. In addition, by cleaning the ceramic mold by vibration of the ceramic mold, forging the laminated metal surface, and laser cutting barbs, the mold can be shifted up, down, front, back, left and right to automate a series of flow operations. Or steel sheet laminating laser melt forging laminating technology, like a three-dimensional printer, laminating a sheet of metal such as a mesh shape such as steel, and partially forging the laminating surface by laser technology A 3D honeycomb structure to be virtually formed on the manufacturing base is virtually placed on the manufacturing base, and the virtual 3D honeycomb structure is cut into a cross-sectional shape cut by the first horizontal plane and punched and sheared. Place a sheet of metal, such as steel with a thickness of about 1.95 microns to 33 millimeters, on a manufacturing base. A sheet of metal such as steel having a thickness of about 1.95 microns to 33 millimeters in the shape of a cross section obtained by horizontally cutting a virtual three-dimensional honeycomb structure on the horizontal surface of the second step is formed on the first step. A metal sheet such as steel that has been punched and sheared with a punching shear is placed on the second stage, and the center of the mesh is melted by laser technology along the shape of the second stage sheet. Laminated sheets that are forged while holding the three-dimensional shape by hitting the mesh of a metal sheet such as steel that has been melted and fixed in the lower sheet and then cooled to an appropriate temperature with a machine-driven computer-controlled hammer with an appropriate hitting condition A cross section of a virtual three-dimensional honeycomb structure on the horizontal plane of the third stage on the second stage, which has been corrected to be thick on the assumption that This third stage is a third stage in which a sheet of metal such as steel is formed by punching and shearing a metal sheet such as steel having a thickness of about 1.95 microns to a thickness of 33 mm with a punching shear. According to the shape of the mesh of the sheet, the center of the mesh is melted by laser technology and the upper and lower sheets are melted and fixed, and then cooled to an appropriate temperature. By repeating this operation of forging while holding a solid shape by hitting it with a machine-driven computer controlled hammer, a series of flow work steps can be performed by replacing a virtual three-dimensional structure with a metal sheet layer while forging 3D honeycomb structure such as Weir Ferran structure forged metal such as laminated forged steel is a framework of flying object or large passenger aircraft This is a description of aircraft design methods and aircraft technology. From the aircraft design philosophy, the inner skeleton of a passenger aircraft has a hollow inside like a bird skeleton. The outer shell of the passenger plane that must be strong and contain a certain amount of light weight must be strong. When the passenger plane crashes with the ground, it is a three-dimensional structure such as a wire-ferran structure in which a metal such as laminated forged steel is forged. Three-dimensional honeycomb structure skeleton such as Weir Ferran structure that absorbs and relieves impact energy to some extent by deforming the honeycomb structure skeleton is processed into a sandwich belt member and outside the skeleton like an aircraft kite and inside the skeleton Belts and belts that weave skeletons that form the outer wall of an aircraft while laminating heat insulating materials and fiber reinforced resins The crossing point of the belt member that is cured and fixed using epoxy resin etc. when the aircraft's kite is completed is the first time that the belt member knitting this kite is knitted into the shape of an aircraft, and when it is completed, On the outside of the skeleton of the belt member having such a shape, 1 to 3 atm is compressed with an industrial gel material, Hanenite (registered trademark), foamed urethane, or a resin ball that can withstand changes in atmospheric pressure above and above the ground. Air or gas encapsulated with a pressure gas made of resin such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 to 33 mm and a thickness of 0.195 to 330 mm is a small collapse of a few children Things like the shape of an egg or a sphere with a size of about a tennis ball to a volleyball Or a polyhedron and an adhesive such as an epoxy resin with an appropriate amount of a combination of a chemical fiber or a natural fiber like cotton having a pulling force of about 0.195 microns to 3.3 millimeters in diameter. A mixture of air filled with air and mixed with a pressure gas made of resin filled with an adhesive such as cotton fibers and resin as a shock absorber. When the resin ball to be used crashes with the ground and crashes, a shock absorber that is more than absorbing energy is attached, and the outer surface of the shock absorber is the outer wall of the fiber resin and the inside of the skeleton The inner wall of the fiber-reinforced resin inner skin is placed between the shock absorbers to protect the safety of the passengers. This skeleton belt has a piano wire or prestressed control like a muscle fiber on the outside. There is a method of gathering steel wires manufactured by a method in which metal steel wires such as REIT steel wires are bundled in parallel or a method of knitting like a hand-knitted sweater with wires, and the inside that is used properly according to the application is metal The honeycomb structure of the fiber and the fiber reinforced resin honeycomb structure are arranged on the tension part of the belt, which is a bamboo-like skeleton that weaves a bamboo belt of a strong belt member arranged in a balanced manner like the hard part and the soft part of the turtle shell There is a method in which the wire is bundled in parallel like a belt like a muscle fiber, and the wire is knitted like a hand-knitted sweater. There is a method in which a rheology body is filled between the wires and the wire is wrapped so that the rheology body does not leak with a resin outer membrane. -The body can be replaced with fiber reinforced resin, that is, it is subjected to the pulling force of the belt, which is a method in which wires such as steel bundled in parallel or bundled or wire knitted like a hand-knitted sweater is housed in fiber reinforced resin The honeycomb structure in which the honeycomb material is used for the inner part of the belt that receives compressive force with the wire bundled in a bundle in parallel with the belt shape or the wire rod knitted like a hand knitted sweater The resin honeycomb structure surrounds the metal honeycomb structure from the surroundings, and I want you to see the turtle shell here. The soft hexagonal shell is formed around the turtle-shaped hard hexagon shell. The combination of this rigid and soft honeycomb structure that surrounds the compartments makes the belt member bend slightly but flexibly In addition, like the H-shaped steel, the rheological body and the steel wire in the mantle and then the fiber reinforced resin substrate and then the rigid and flexible material so that the member can withstand alternating stresses of compression and tension The belt member is made more dynamic by the honeycomb structure, then the fiber reinforced resin base material, then the steel wire and rheology body are wrapped in a mantle, that is, the honeycomb structure is sandwiched between both sides by a wire such as steel. In this patent claim, which is an advantageous and easy-to-use material, this member is called a sandwich belt member. The rheological body of the sandwich belt member has a method of replacing it with a fiber reinforced resin. When we do, we will mainly refer to the sandwich belt member, and the belt member will make an aircraft skeleton made of bamboo bamboo. The inside is a wide cavity, as if the fuselage, both wings, and the tail are all mechanical structures, like an aircraft made by weaving bamboo baskets. This is designed to balance the entire aircraft, which is a masterpiece of bamboo bamboo weaving so that it can withstand fatigue of repeated loads and stress is distributed as you see The method is like a float of a Nebuta Festival. Fiber-reinforced resin such as paper is placed on a skeleton like bamboo basket, and piano wire or prestressed steel wire is pretensioned inside the fiber-reinforced resin of the outermost skin ( A technology that hardens the fiber reinforced resin after applying tension to the steel wire in advance and is embedded in the fiber reinforced resin layer in the form of a mesh. In other words, the outermost skin is a piano wire or a prestressed steel wire. As the fiber reinforced resin with the mesh of the center in the center, it will not break into fine dust at the end of the crash, and the outer skin is made of fiber reinforced resin with shock absorbers sandwiched around the kite skeleton as described for the safety of the flying object Because of the sandwich structure, the impact energy is reduced in the order of fiber reinforced resin outer wall shock absorber 籠 shape skeletal impact absorber fiber reinforced resin inner wall wall to absorb and relieve the impact energy. However, the method of the present invention is a design method that goes from the center to the outside where the skeleton is rigid and the outer skin is fragile. The design method must be revised with respect to human life rather than economy, sandwich belt member 籠 exoskeleton shape flight as application of sandwich belt member The body is composed of a spherical passenger part with a head, both wings, and a tail, and is about the size of a jumbo jet (registered trademark). This method, which can support multiple floors with a honeycomb structure, can take a large space inside the wings. The flying object simulates a thick flying fish with a saddle-shaped exoskeleton The flying object is a stubby body that is round like a goldfish and the thick wings are structured like a cross section of the wing according to Bernoulli's theorem Forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine to obtain rotational force at the tail part of this squadron that produces a difference in pressure between the upper and lower parts and obtains lift Forced air-cooled whole heat-dissipating fiber Reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor as a generator Forced air cooling whole heat dissipation fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type generator after getting power Bird Strike Prevention Device Fiber Reinforced Resin Metal Composite Turbine Stacked Electric Motor Using Its Power Sends Wind Backward to Fly Flying Objects Simulating Thick Flyfish Propulsion Device Forced Air Cooling Whole Radiation Fiber Reinforced resin metal composite internal combustion engine Angular momentum adjustable spring wheel torque converter clutch forced air cooling whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk generator generator output power transmission transmission integrated hybrid device A wide internal space that can be comprehensively managed by computer It can be used for multi-purpose partitioning with cocoon-shaped walls, floors, and honeycomb structures knitted with Chibelt members. Bird strike prevention device fiber reinforced resin metal composite turbine laminate type electric













The motor-attached method is a sandwich belt member that can obtain a strong driving force. The center of the sphere-shaped exoskeleton is a sphere and the outer periphery of the sphere is a disk shape. Peripheral part Wing shape Relief of falling fallen parachute installation Fuel generator Ballast hanging Droppable flying object has several ducts on the outer periphery of the disc part where the exoskeleton of the flying object is knitted with sandwich belt members In order to obtain buoyancy that is blown down by the engine and floats up, the disk part is expanded to the left and right, and multiple ducts and engines can be arranged radially on the concentric circles of the disk The part where the wind hits the direction of travel of the disk The duct engine that processes into a wing shape has a cross-shaped beam in the middle of the cylindrical height, and two rotary engines above and below the center of the cross. Or two zero-type fighter aircraft Sakae engine twin engine horizontal piston simulated forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine fixed up and down at the center of the cross beam fixed to the shaft of each internal combustion engine The upper and lower propellers or fans are a duct fan that rotates inside a cylindrical shape. Engine exhaust is taken into a silencer in the disk and purified through a ceramic filter and exhausted from the lower surface of the disk. There is a method of obtaining electric power at the same time as buoyancy by installing a forced air-cooling whole heat-dissipating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacked generator between the internal combustion engines of this type Because there is a levitation force by the ventilation of a certain vertical duct, it does not require a long runway, and it is fixed on the boundary between the spherical surface and the disk with respect to the traveling direction of the sphere. Basic Bird Strike Prevention Device Fiber Reinforced Resin Metal Composite Turbine Stacked Electric Motor Sends Wind Backward and Advances to Control the Right and Left and Up and Down Attitude Controls by the Difference in Four Outputs of Four Motors in the Direction of Travel The right and left of the outer circumference of the spherical disk controlled by the difference in the output of the duct engine is processed into a wing shape, and there is also a method of extending both wings to the left and right, and it is possible to attach an aileron to the wing and control the pitch. Four bird strike prevention devices that obtain buoyancy with the duct engine described in the claims that seem to be flying in the air Fiber reinforced resin metal composite Turbine laminated electric motor with forced air cooling Whole heat radiating fiber reinforced resin metal composite Internal combustion engine angular momentum adjustable spring wheel torque converter clutch forced air cooling whole heat dissipation fiber reinforced resin metal composite rotor A permanent magnet stator electric coil disk laminated generator motor output power transmission transmission integrated hybrid device combined with a hybrid device that obtains propulsive force A ray simulation model that simulates the shape of a ray that deforms a spherical central circumferential disk The flight speed is stabilized by sending the wind backwards using four laminated electric motors with fiber reinforced resin and metal composite turbines that stabilize the flight by extending the tail sharply from the disk like the ray to be included in the scope of the term The vertical duct of the disk is configured to reduce the burden on the duct fan by obtaining the buoyancy of the wings according to obtaining the forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable flywheel torque converter clutch Forced air cooling Whole heat radiating fiber reinforced resin Metal composite rotor Permanent magnet stator Electric coil disk laminated generator Motor output power transmission It is possible to comprehensively manage the energy by making it an integrated hybrid device. Multiple parachutes are installed between the duct fans on the outer periphery of the disk. This parachute is opened and dropped when it falls. At the same time, pulling the mouth of the upper part of the parachute with a wire induces the fall of the sphere disk, so that the flat bottom and the leaves fall down in the air and ease the collision with the ground. A heavy object is installed and suspended at the bottom like a ballast tank so that it can be moved up and down, and when the airflow is bad, the weight part such as generator and fuel of the ballast is suspended downward, the center of gravity is lowered, and the whole disk rotates to the top and bottom. This ballast part that prevents it from falling is to be dropped separately from the spherical disk body in a safe position in order to reduce the weight when falling The lower part of the sphere that can be suspended is cut off at the bottom of the sphere, and a shock absorbing layer is provided in the lower part of the sphere. 900 people in a single flight where the aircraft does not fall apart by crashing against the ground in the event of a crash, flying safely and comfortably and being used for multiple purposes partitioned by a wall or floor of a kite made of sandwich belt members or a honeycomb structure plate Fuel that has a structure that can be transported to the extent that heavy oil, light oil, or gasoline can be used, and exhaust gas passes through the muffler with built-in catalyst, so if it falls on the sea to mitigate quiet air pollution, it starts from the bottom of the disk part Although the float like an air bag inflates, this spherical disk is inherently a watertight and airtight structure that floats on water. In the event of a crash, it swells like an air bag and softens the impact of the crash. This function is applied to the ray simulated flying object together with the parachute and the central spherical outer disk flying object and ray simulated flying object are functionally similar. From now on, it is a description of the laminating technology. In the vacuum deposition laminating technology, the shape opposite to the pole that is charged by charging the metal thin wire as an electrode by drawing a figure using the metal thin wire in the shape to be deposited. The vacuum deposition material is charged in the crucible in which the crucible lid in the shape of a crane neck flask is in close contact with an ordinary crucible that prevents the entire diffusion of the deposition material made of porcelain in the crucible that prevents the entire diffusion of the deposition material. The electrode to be melted is evaporated and charged by inserting a rod-like electrode into the melting surface inside the crucible or inside the crucible, and the tip of the crane neck is deposited through a conduit having a reverse potential of the deposited material. Nozzle with the same quality of the electric potential prevents vapor deposition from occurring on the target figure with different electric potentials The vapor deposition material led to the nozzle evaporates and the electrostatic transport transports the nozzle from the movable conduit to reach the target electrode from the nozzle You can also move the crucible flask-shaped crucible like a three-dimensional printer and selectively and intensively focus the target fine line from the nozzle-shaped vapor deposition material outlet at the tip of the crane neck like a three-dimensional printer. By depositing and depositing the vapor deposition material, which is controlled by a device such as a camera shutter, on a target thin line at the top by electrostatic force, deposits and deposits the thin lines so that they do not scatter on other parts. Vapor deposition is carried out according to the shape of the electrode of the fine wire to be charged, and a three-dimensional solid shape is formed by the vacuum vapor deposition material, or conductive instead of the target fine wire. The method using the ink draws the target figure for vapor deposition like a three-dimensional printer, charges the figure, vacuum-deposits the figure as described above, and further laminates the figure you want to laminate on the target figure like a three-dimensional printer Stacked three-dimensional structures can be formed by vacuum-deposited materials by charging the drawn figure and evacuating it from the top to concentrate on the top figure, and repeating this process, or silver clay technology has been applied to three-dimensional lamination The method is paper or resin fiber placed on a manufacturing base using ink containing a mixture of fine powder of metal to be laminated with oil or water-soluble air contact curable curing agent on paper or resin fiber nonwoven paper Draw the figure you want to laminate on the non-woven paper like a 3D printer, and draw the figure you want to laminate another sheet of paper on the figure you want to laminate like a 3D printer. Draw a figure with a printer like a three-dimensional printer by adjusting the amount of ink so that the curable ink containing powder penetrates between the fibers of the paper and the ink of the upper paper and the lower paper is compatible Draw a figure with a curable ink containing fine metal powder that you want to superimpose and laminate the paper on the paper. Repeat this to obtain a paper or resin fiber nonwoven paper that is laminated and cured. The purpose of using paper or resin fiber nonwoven paper to burn a resin fiber nonwoven paper and sinter-bond the metal to obtain a three-dimensional structure is to shorten the lamination time, secure the width of the ink, and the surface of the three-dimensionally laminated method. For smoothness, a plurality of spot-like dots are printed at fixed positions around the figure to be laminated, and when a bundle of paper is cured, a set of points are stacked and cured to form a column. Protected shape until sintered and hardened paper Assuming that the three-dimensional structure shrinks due to sintering, which facilitates the transportation of the bundle, the size is corrected and the laminated figure is drawn. The aircraft structure is a description of the flying body structure. The flying body structure is made of resin, carbon fiber reinforced resin, glass fiber reinforced resin, fiber reinforced resin such as Kevlar fiber reinforced resin, or these metals or Use a combination of resin or fiber reinforced resin materials, use epoxy resin to layer metal and resin film layers like a stratum, or use fiber materials such as aramid fibers Use a combined material, or use a material in which a fiber material is knitted into a belt shape, solidified with a resin, or used as a member to knit the heel structure, or extruded with metal Or by using a material in which a thin metal pipe is assembled and press-fitted and solidified with resin, or sandwiching both sides of a honeycomb structure plate with a plate material such as fiber reinforced resin and bonding with epoxy resin Carbon fiber reinforced resin on the outer surface of a three-dimensionally machined product that uses a honeycomb sandwich structure with a sandwich structure, or a structure in which a honeycomb structure / plate material / honeycomb structure / plate material are alternately laminated in layers. Alternatively, there is a method of using, as a member, a material obtained by covering and reinforcing a fiber reinforced resin such as a glass fiber reinforced resin with a thickness of 3.3 to 195 mm, or a via that forms a Wierferan structure like a panel. -Ferran structure is a three-dimensional structure in which a polygonal member, which is the basic structure of a honeycomb structure, is bonded with epoxy resin. There is a method of forming a weir ferran structure into a panel shape, a weir ferran structure panel sandwiched between fiber reinforced resin plates, or a structure in which these are laminated in layers alternately There is a method in which a material obtained by covering and reinforcing the outer surface of a three-dimensionally machined object with a milling machine or the like with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm is used as a member. In order to prevent fatigue in a place where repeated fatigue is likely to occur by using a pipe-shaped member assembled according to the stress flow in the cross section and bundled into a bundle to prevent stress concentration by bonding with epoxy resin between the pipes Rheological deer such as muscle-tendon relationship with flexible and highly viscous mucous that absorbs the energy of stretchable fatigue fracture intentionally A layer of fibers, not simply a single wire, but a layer of membrane aggregates, not just a single compression material By providing a rheological layer like the relationship between muscles and tendons with viscous mucus properties, the stress concentration is diffused to each part of the assembly to prevent the progress of fatigue failure and these three-dimensional honeycomb structures that balance mechanically or these Combined layered hierarchical structure and three-dimensional aggregate structure combined with epoxy resin using pipe aggregate material or hierarchical structure object in the tension part and three-dimensional aggregate structure object that prevents fatigue failure in the compressed part This composite structure can also be used on aircraft, with a shock absorber between the composite structure walls, i.e., 195 millimeters to 330 millimeters in thickness 1.95 to 3. By providing a gathering layer of millimeter rubber rods, the impact energy to the passenger is reduced when the flying object or aircraft crashes against the ground, and the shock absorbing material sandwiched between the walls and the center of the wall is balanced Shock absorbers are made using rubber, resin, Kevlar fiber, silk, cotton fiber, chemical fiber, or a combination of these, including air, like a ball. An individual aerial work flying object, which is a description of the structure and a description of the safety or structural strengthening of the flying object or aircraft, is composed of an upper flying object and a lower suspension body. The upper flying body corresponding to the hair part uses a method of using an electric motor, a method of using an internal combustion engine, a method of using a balloon, a balloon, and a balloon. The description of the combined device is divided into the method of a combined device that combines a dynamic motor, an internal combustion engine, or an electric motor, an internal combustion engine, a generator, and a balloon. The balloon is a hot air balloon, a gas balloon, or a hot gas combined balloon method. Divided into professionals to increase climbing efficiency


This hot gas technology is also used in airships, which are used in the following ice cream cone-type flying bodies, including the method of sealed enclosed hot gas balloons that use helium mixed in a pan and burned to heat helium. The method of using an electric motor for the upper aircraft is a gyro that stabilizes the upper aircraft, and a parachute that can be used manually or automatically for emergency methods and a blower for obtaining a lifting force are installed in the upper aircraft. From here, the blower which is the description of the method of manufacturing the propeller or fan is the one formed by processing solid wood as a propeller or fan according to the description of the above composite material and cutting or pouring resin into the mold, or titanium, aluminum or stainless steel Or metal such as ultralight high-performance general-purpose magnesium alloy or carbon fiber reinforced resin This method consists of a combination of these materials. The method of combining the materials here is to use a propeller or fan that is perpendicular to the blade rotation direction, i.e., in the radial direction from the shaft to the outer periphery, A hollow pipe material with a diameter of 0.195mm to 3.3mm in the direction along the flow is assembled and the epoxy resin is hardened. A molecule manipulator that combines atomic implantation technology with molecular insulators and molecular beams, or a nano robot such as a ribosome that automatically transports and manufactures molecules, carries atoms or molecules, assembles molecules according to the molecular structure design method, and arranges them in three dimensions. Level 3D printer atom stacking technology (normal temperature superconducting material manufacturing Constructant along the flow of stress at the same time as weight reduction because the inside of the pipe is hollow with a three-dimensional shape in the shape of a propeller or fan blade using the technology to construct the molecule itself with It is tough because it is an assembly of thin pipe materials with a suitable arrangement according to the specific characteristics) Another composite method is to laminate paper, resin or metal honeycomb structure and cut with milling machine etc. Using a machine to form a three-dimensional shape in the shape of a propeller or fan blade, the outer surface has a thickness of 3.3 to 195 mm, and is coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin. In the composite method, the fiber material is aligned in the direction of the stress flow in the radial direction, the propeller or fan shape is formed, and then the resin is poured between the fibers. The solidified object is strong against rotation. The upper aircraft lift device is composed of these propeller or fan and electric motor. There is also a method of using a commercially available electric motor, which is a description of the overall heat dissipation of forced air blowing, but a new fiber reinforced resin electric motor is made of copper or gold or room temperature superconducting material such as enamel, glass fiber reinforced resin or wire Conductive coating material such as ceramic processed surface of glass, or wire coating material such as glass processed amorphous material, and the inside of the pipe of the wire is forced air-cooled or water-cooled, or heated through liquid helium or liquid nitrogen Superconducting coil or steel or aluminum or titanium that prevents melting Or a combination of metals such as ultra-lightweight high-performance general-purpose magnesium alloy or carbon fiber reinforced resin or these materials, the electromagnetic part of the electric motor is replaced with metal and carbon fiber, and other structural materials are replaced with fiber reinforced resin. Forced air cooling is a method of forced air cooling in which a coil is forcibly air-cooled by a small blade that forcibly blows air to the coil of a light and strong electric motor, and the coil is forcibly air-cooled directly. The fiber reinforced resin that is the structure of the electric motor has a plurality of small holes with a diameter of 0.195 mm to 3.3 mm, and the heat is released by releasing hot air from the entire electric motor. There are multiple brushes made of composite material considering heat dissipation, or multiple brushless electric motors or The upper flying object is a target and hierarchical arrangement of a plurality of electric motors combining these brushed motors and brushless motors, the above is a description of lightweight and powerful electric coils and forced air blowing overall heat dissipation, The blower of the upper flying body is a fan motor integrated type in which a fan and a motor are integrated, or a fan in which the air blow direction of the air blower or the air blower is adjusted upward, the exhaust air is adjusted downward, or a duct fan with a fan in the duct The lower suspension body, which corresponds to the dandelion seeds, is constructed to allow humans to work freely in the air so that they can carry them on or suspend them. A method of assembling and a method of stacking honeycomb structures such as honeycomb sandwich panels or via-ferran structure panels; It can be divided into a method of assembling objects of shape or a method of assembling a combination of pipe structure, honeycomb structure and dredging structure, and the method of using the pipe structure to form a framework as the structure of the upper flying body is assembling pipe members It is manufactured by integrally forming by autoclaving, etc., which is baked under pressure in a large kiln at a factory with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin As for the appearance shape of the upper aircraft, the outer shape is maintained in the range of 195 mm to 3300 mm in width and depth and 195 mm to 3300 mm in height, and the inside is formed with a cavity or a framework. The appearance shape of the upper aircraft is a sphere or donut shape, that is, an annular surface Or a toroid, a spheroid, a spheroid, a rotation quadratic curve, a rectangular parallelepiped, a cube, a polyhedron, a polygonal cylinder, a cylinder, or a cylinder of this size, or a conical or truncated cone Alternatively, combining the method of using a quadrangular pyramid alone and these three-dimensional shapes, the upper flying object has a conical shape with the sharp apex of the conical shape, or the upper and lower surfaces of a cylindrical shape with both ends of a short pencil sharpened. The shape of the conical base connected to the bottom, or the shape of the conical bottom connected to the lower surface of the cylinder, such as the bottom end of a short pencil, or the larger of the truncated cone like a large abacus ball A method of forming a solid with the bottoms bonded together and using it alone, or using this large abacus ball connected vertically Or it is the shape of an aggregate that uses a combination of a sphere or spheroid or a sphere or spheroid, or a combination of a sphere or spheroid. There is a method, the structure of the upper aircraft is a structure in which pipes are assembled. The framework of the upper aircraft is a horizontal member, a vertical member, a propeller or a fan guard member. On a wire that has been knotted by winding the members around the joint part 3 to 33 times with a wire material of 0.195 mm to 3.3 mm in diameter, such as wire, resin, chemical fiber, or carbon fiber reinforced resin The nodule is hardened with an epoxy resin or bonded with an epoxy resin, There is a method of rigid bonding by genus welding or fixing with aluminum screws or fixing tools. Fixtures are assembled by combining steel clips, resins, carbon fiber reinforced resin, glass fiber reinforced resin, etc. The upper part can be used to quickly and easily assemble a personal aerial work flying object at aerial work or flight leisure sites by fixing the detachable member to the rigidly connected member with a detachable fixing device that facilitates The horizontal member of the flying object is divided into a horizontal member for rigid connection, a horizontal member for attachment and detachment, and a horizontal member for the guard of a propeller or fan, the vertical member is divided into a central vertical member and a peripheral vertical member, and the upper flying object can be assembled and disassembled The detachable horizontal member that fixes the electric motor in this way is a detachable horizontal pipe inside the pipe of the horizontal member for rigid connection rigidly connected to the vertical member The center vertical member is passed through the middle of the detachable horizontal member, and then the rigid horizontal member and the detachable horizontal member are fixed by the fixing tool, and then the electric motor is fixed to both ends of the detachable horizontal member. Alternatively, the electric motor is first fixed to one end of the detachable horizontal member, and then the end other than the end of the detachable horizontal member to which the electric motor is fixed is rigidly connected to the vertical member. The center vertical member is inserted into the center of the central vertical member and fixed with a fixture and the two horizontal members for detachment are abutted at the center of the central vertical member, or the horizontal member for detachment with the electric motor fixed is attached to the central vertical member. There is a method of inserting into the rigid horizontal material like a cantilever beam, and the detachable horizontal member for fixing the electric motor is divided into two methods, a method of using a pipe member alone, or a wearing that supports the electric motor. There are two methods of assembling the horizontal member for an annular structure, that is, using a detachable horizontal member as a single unit or an annular structure. Is a triangle on the inside of a polygon such as an equilateral cross, a star of David (hexagram), a pentagram or a dodeca, twelve, sixteen, thirty-two petal, or octagon There are methods in which polygons with different shapes and sizes and meshes or meshes with diagonal lines are combined inside the polygons that combine diagonal lines, and these shapes can be disassembled and assembled. This is a horizontal member that can be stacked so that the steps are stacked vertically by combining the propellers or fans so that they do not touch each other by shifting the horizontal position or shifting the vertical position from aerodynamic considerations. Multiple electric motors on a horizontal member with an equilateral cross shape or a horizontal member with a combination of a triangle and a diagonal line inside a polygon such as an octagon. It is delicately positioned in the horizontal and vertical directions in consideration of the thrust of rising the wind and the stable balance of the flying object due to the interference of winds aerodynamically blown in the horizontal and vertical directions so that the propellers or fans do not hit each other. The upper flying object, which is arranged while shifting, is a structure that increases the thrust in the upward direction by laminating horizontal members of this equilateral cross shape or a combination of polygons and diagonal lines inside the polygon in multiple stages The vertical member is composed of a central vertical member, a peripheral vertical member, and a fixture described in the scope of claims. The pipe is rigidly connected by screwing, welding, adhesion with epoxy resin, etc., and the rigid part is reinforced by plate members or rib members. The shape of the central vertical member is a three-dimensional girder that is a prism or cylinder or a horizontal member and a vertical member. There is a method in which a horizontal member of a branch grows in an annular structure of an elongated square pyramid like a steel tower by combining a structure or a horizontal member and a vertical member, or a method in which these shapes are combined. The center member has a cross section of a Chinese character with a mouth or a rice field, and one side is 33 mm to 66 mm. The vertical length is about 195 mm to 3300 mm, aluminum, carbon fiber reinforced resin, glass fiber reinforced resin, or Resin, foamed resin, or these materials alone or in combination There is a method of using the pipe vertically, the meaning of combining this material is to include the method of pouring urethane foam or carbon fiber reinforced resins into the mouth part of the Chinese character of the aluminum pipe or the hollow part of the cross section of the rice field, and curing it. The cylindrical central member is made of waterproof paper having a diameter of about 66 mm to 99 mm, a thickness of 1 mm to 6 mm, and a length of about 195 mm to 3300 mm. Meaning that a cylinder is vertically used with a composite material in which the above film material is wound or made of aluminum, or a carbon fiber reinforced resin, a glass fiber reinforced resin, or a material made of the above composite material, which is a single material or a combination of these materials. Foams into the cavity of an aluminum cylindrical pipe Including the method of pouring fats or carbon fiber reinforced resins and curing them, holes are made in the sides of these prisms or cylinders, and horizontal members for rigid connections are formed on the vertical members and branches perpendicular to the central member. In order to produce a horizontal member for rigid connection in order from the direction of east, west, south, north, or eight directions
Pipe corner












Winding around the joint part between 3 and 33 times with a rod of 0.195mm to 3.3mm in diameter, such as metal, resin, chemical fiber, carbon fiber reinforced resin, etc. Wrapped around a piece of wire that has been knotted and hardened with an epoxy resin, or rigidly bonded with screws, welding, or epoxy resin bonding. Cylindrical center vertical material is a horizontal member for rigid connection, which has a structure in which multilaterally stacked cross-shapes of equilateral sides with branches at right angles and a combination of polygons and diagonal lines inside a polygon. The center vertical member is made from 3 times to 33 times with members of 0.195 mm to 3.3 mm in diameter such as metal, resin, chemical fiber, carbon fiber reinforced resin, etc. Then, the horizontal part and the vertical part for rigid connection are made by winding the joint part around the joint and winding it together with the epoxy resin or aluminum welding or epoxy resin or aluminum screw. The central vertical member of the solid girder structure that is rigidly fixed is made of aluminum, carbon fiber reinforced resin, glass fiber reinforced resin, or a combination of these, and a square cross section with a side of about 10 millimeters and a thickness. The center part of the horizontal member for rigid connection is sandwiched with four equilateral pipes with a length of 1.5mm and a length of 195mm to 3300mm in the vertical direction. The vertical center member and the horizontal member are rigidly assembled and rigidly connected to form a three-dimensional cross beam. An upper horizontal body is configured by inserting a horizontal member for attachment and detachment into the inside of the base and fixing with a fixture. The horizontal member for rigid connection fixes an electric motor to facilitate assembly and disassembly of the upper aircraft. The socket structure in which the horizontal member is inserted is a method of inserting the detachable horizontal member through the inside of the socket and a method in which the ends of the detachable horizontal member are attached to each other at the center of the central vertical member. Like the cantilever beam, the end of the horizontal member for attachment and detachment is divided into three methods, where the vertical center member is an elongated square pyramid ring method like a steel tower. As in the structure, a ring is formed in a diamond shape stiffened at the center so that the compression member does not buckle, and the horizontal member for rigid connection is rigidly connected. 16 to 3 to get An electric motor in which about six propellers or fans and a plurality of electric motors are stacked in multiple stages, and the electric motor base is fixed to the base of the detachable horizontal member with aluminum screws or the like. And propellers are targeted at each position on the horizontal member, and multiple propellers or fans inside the upper flying object are balanced by reversing the direction of rotation of each propeller or fan at the target position. The horizontal member of the upper flying object is 15 mm to 30 mm wide, 15 mm to 30 mm high, preventing the entire personal aerial working flying object from rotating horizontally when the aerial working flying object rises into the air. Thickness 1.5mm to 3.3mm Length 195mm to 3300mm Of non-equal sides or equilateral angles made of aluminum, carbon fiber reinforced resin, glass fiber reinforced resin or Kevlar fiber reinforced resin pipe or a combination of these, the rigid horizontal member and vertical member are welded joints of aluminum members, Horizontal parts and vertical members are welded with aluminum stiffening plate welding and aluminum rib reinforcement welding, and the rigid parts are strengthened and strengthened, and the upper flying object is epoxy resin, carbon fiber wire or netting material, carbon fiber tape, carbon A detachable propeller or fan guard member is fixed to the tip of a detachable horizontal member fixed with an electric motor, which is reinforced with fiber reinforced resin, glass fiber reinforced resin or Kevlar fiber reinforced resin, and fixed with a fixing tool. The material of the fan guard member is resin, carbon fiber reinforced resin, glass fiber This propeller or fan guard member, which uses reinforced resin, chemical fiber, Tegs, stainless steel wire, wire, or a combination of these, can damage the propeller or fan when a personal aerial work flying object comes into contact with other objects. Prevent propellers or fan guard members, including a fan motor or blower method that integrates a duct fan and motor into a cylindrical duct, and the structure in which the pipe is inserted into the pipe also serves as reinforcement for the upper aircraft In order to prevent the pipe from buckling in the pipe cavity, the horizontal member, the vertical member, the propeller, the fan, the fan motor in which the fan and motor are integrated, or the fan guard member where the stress of the pipe is concentrated. There is a method to reinforce the pipe by encapsulating and curing foamed resins. The body is lightweight and robust, the pipe is made of the above composite material, the simplest way of assembling the pipe, the width 15mm to 30mm, the height 15 to 30mm, the thickness 1.5mm long 195mm to 3300mm non-equal or equilateral angle aluminum, carbon fiber reinforced resin, glass fiber reinforced resin pipe or a combination of these, ladder shape, bird cage shape or jungle gym The frame shape is also an object included in the assembly method by fixing the pipe with a fixture. The method using the honeycomb structure for the upper flying body is a resin or paper diameter of 1.95 mm to 33 mm and a thickness of 0.195. A cylindrical pipe of millimeters to 3.3 millimeters The honeycomb structure according to the present invention is divided into a method of stacking honeycomb structures such as a honeycomb sandwich panel or a wire-ferran structure panel in which a honeycomb structure is produced by bonding and curing with a resin, and a plate material is bonded to both sides of the honeycomb structure. Hexagonal honeycomb structure, OX structure, flex structure, bisecting structure, feather structure, or other various shapes are laminated to form a laminated structure using adhesive, brazing material, 3D lamination technology, or 3D cutting. The material of the honeycomb structure in this claim is paper, non-combustible paper, metal such as aluminum, titanium or stainless steel, aramid paper, fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin, or these The combination A honeycomb structure such as a horizontal honeycomb sandwich panel or a weir ferran structure panel is formed by hollowing a hole having a diameter of about 330 mm to 990 mm for a propeller or fan in a honeycomb structure panel such as a composite honeycomb sandwich panel or a weir ferran structure panel. The inside of a honeycomb in which honeycomb structures such as a honeycomb sandwich panel or a weir-ferran structure panel are vertically layered in a vertical member of a pipe made of aluminum, carbon fiber reinforced resin or glass fiber reinforced resin to laminate the panels. Like the structure, multi-stage honeycomb structures such as honeycomb sandwich panels or via-ferran structure panels are stacked and connected to form a shape such as a rectangular parallelepiped, cylinder, disk, or donut. The upper aircraft forms the upper aircraft in the shape of the upper aircraft. The upper aircraft is a vertical member that can see a hexagonal set of honeycomb structures such as honeycomb sandwich panels or weir ferran structure panels when viewed from the top. A method of stacking at intervals of 195 mm to 330 mm in order to take in air from the periphery of a honeycomb structure such as a honeycomb sandwich panel or a weir-ferran structure panel, which is used in a direction to withstand the load during ascent and descent, or a honeycomb sandwich Holes with a diameter of about 330mm to 990mm, which are made by sticking and laminating honeycomb structures such as panels or via-ferran structure panels, are laminated like a fan motor or duct of a blower where the duct fan and motor are integrated. Direction As a raw material, pipes made of aluminum, carbon fiber reinforced resin, or glass fiber reinforced resin may be used for horizontal members and vertical members for the purpose of reinforcing honeycomb structures such as honeycomb sandwich panels or via-ferran structure panels. A honeycomb sandwich panel made of a honeycomb structure with a side of 19.5 mm to 330 mm and a thickness of 19.5 mm to 330 mm. A fan motor or blower in which an electric motor and propeller or fan or fan and motor are integrated in the space of a fan motor or fan in which a duct fan and motor are integrated by opening a hole of a certain degree Including the method of laminating honeycomb sandwich panels placed on each other, the word "belt member" is used as a belt-shaped member, ie, a member for knitting a ridge in this claim, and the sandwich belt member defined in this claim. Meaning, the method of gathering cocoon-shaped objects formed by weaving sandwich belt members has a structure like using multiple bamboo baskets formed by weaving bamboo belts. A composite member that combines flexibility and toughness, such as a bamboo material that weaves bamboo baskets using a sandwich belt member that combines aluminum, carbon fiber reinforced resins, glass fiber reinforced resins, and resins to form a composite member. The belt member used for the material for knitting the heel with a belt-shaped member is 0.33 to 1.95 millimeters in thickness and 3.3 millimeters in width. 19.5 mm metal such as aluminum or titanium, carbon fiber reinforced resin, glass fiber reinforced resin, or resin film made into a laminated belt, carbon fiber wire knitted like a knitted wool yarn, epoxy resin Bamboo knitting bamboo baskets glued with epoxy resin sandwiched between aluminum strips with a thickness of 0.33 to 1.95 millimeters and a width of 3.3 to 19.5 millimeters, centered on the belt-like material There is also a method of using a belt-shaped composite object with a shape like the above as a material for knitting a cocoon. Constructed and braided braided belts, and the members at the intersections of the belts are fixed with epoxy resin. The entire collar is tough and supple, and the collar structure is slightly deformed. This ridge that is flexible and strong enough to restore the strength is reinforced with a rod or pipe material that is a combination of aluminum, carbon fiber reinforced resin, glass fiber reinforced resin, or resin with a diameter of 1 to 5 mm. It can be processed into various shapes like a bamboo basket, and the sphere-shaped method that combines the hemispherical colander shape and the colander shape has a portion corresponding to the equator on the earth. It can be assembled and disassembled with a fixture, that is, a semi-circular material made of a bamboo sphere in a hemispherical shape with a sandwich belt member in a semi-spherical shape of a bamboo cocoon, and shaped like a family crest of Shimazu 丸 in a cross shape An electric motor and a pre-peller or fan are installed in the center of the cross beam of an object like a crest of Shimadzu with a hemispherical shape in the shape of a hemisphere with the object in the middle and the upper and lower hemispheres -Shaped saddle member and center circle An electric motor used for a flying object that can be easily assembled and disassembled like a spherical bamboo basket with an electric motor and a propeller or fan installed in the center. There is a method in which the fan and motor have a method in which the rotor is a disk-like wheel and the wheel becomes a propeller or a fan motor or fan in which the motor is integrated with the motor, like a wheel motor whose outer periphery is a motor. The manufacturing method of the integrated fan motor or blower is four, eight, twelve, sixteen, or thirty, by cutting radially from a location 33 mm away from the center of the disk and bending it into a blade shape. Fan motor or blower in which the fan and motor are integrated by forming two blades A ring-shaped member is welded to the outer periphery of a fan motor or blower that is formed into a shape or an integrated fan and motor, and a plurality of neodymium magnets and other permanent magnets are fixed along the outer periphery of the ring. A circle with multiple coils on the outer circumference of the ring to wrap













There is a method using a board-shaped electric motor. The shape of the kite is a method of using a plurality of kite spheres to gather like a kite kite. This includes a method in which a honeycomb structure such as a honeycomb sandwich panel or a weir ferran structure panel is stacked horizontally in multiple stages, which is exactly the shape of the internal structure of a natural round honeycomb. The kite will be the structure of the entire flying body and can protect people inside the kite, and it can also enter the inside of the spherical kite, and the kite will face down the wind generated by the electric motor. It can also be used as a propeller or fan guard and the structure of both the upper flying body and the lower suspension body.This kite can also be used as a boarding deck where you can feel the structure of the airship and the wind. The spherical spear has a structure that allows easy assembly and disassembly of the spear and spear by attaching and detaching the fixture. The method is to combine two hemispherical spears into a sphere, with a propeller or fan and electric motor inside. An electric motor and propeller or fan, which is a method of constructing a flying object by gathering cage-shaped spheres with propellers or fans and electric motors arranged together with fixtures like a cocoon tuft, is about the size of a fist Attach a propeller or fan to the shaft of a normal electric motor with a rotor and fix it to the center of the cross beam, and the horizontal plane passing through the center of the sphere is a disc-type motor and propeller or fan or fan and motor. There is a method to install a blower at the center of the fan motor or cross beam, and the rotor of a disk type motor is used as an electric motor. A permanent magnet such as a neodymium magnet is fixed around the outer periphery of this disk-shaped propeller or fan in the shape of a blade of a blade, and a ring-shaped member wraps around the outer surface of the disk-shaped rotor so that it encloses the magnet. A disk-type electric motor that includes a disk-type propeller with multiple coils or a method that combines a fan and a motor is included in the disk-type electric motor. The lower suspension body in which the lower suspension body is provided at the lower center position of the upper floating body of the personal aerial work flying object, which can be used in the stacked method, is a natural fiber or chemical fiber lobe or steel made of about 195 mm to 3300 mm in length. Wire or metal such as iron, steel, aluminum or titanium, resin, carbon The lower suspension body is composed of fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin or a combination of these materials, and the lower suspension part is composed of ropes, wires, wires, rods and pipes. The lower suspension body is connected to the center of the lower end of the upper flying body with a freely movable connecting device such as a chain link or universal joint, and is flexibly connected so that the center of gravity of the lower suspension body can be moved freely. For ropes, wires, rods, and pipes, a person who works in the air sits on a swing platform provided on a lower suspension body such as a rope or stands on a step fixed to the lower suspension body From here, it is a description of the safety measures of workers, humans who work in the air fall from about 33 meters above the ground A lightweight air bag with an air cap hardened with foamed foam so as not to damage the body, and a small air bag with the inside of a cloth or non-woven fabric made of natural fiber chemical fiber of the size of a small cocoon with rubber or silicone rubber Like a lightweight cotton garment with a 19.5mm to 33mm thick waterproof cotton garment dress or a collection of air-centered fibers. A human body protective bag such as a human sleeping bag or a human body protective clothing that allows humans to enter and exit with a simple waterproof and airtight zipper and Velcro (registered trademark) is connected to the lower suspension body with a fixing tool and belt that can be attached to and detached from the lower suspension body There is a way, here is a description of a waterproof and airtight zipper, waterproof airtight zipper is waterproof and airtight and the zipper will bite into the fabric The thickness of the zipper is about 0.195 mm to 3.3 mm thicker than the two base fabrics, and the width is about the width of the zipper's left and right seams when the zipper is viewed vertically. Resin fins of about two pieces on the back and front and four on each side of the zipper seam A little larger than the width of the zipper, each of the fins along the resin zipper is sewn one by one on the zipper seam The fabric prevents the fabric from biting into the zipper when pulled up. The back and front are airtight and waterproof. Even if the zipper is pulled up rapidly, the fabric does not bite into the zipper. The above is a description of a zipper that is airtight and waterproof inside the zipper, and the above is a waterproof and airtight catch, shock absorbing material and seat for human side protection are chemical fiber material or carbon fiber wire or There is a method that uses a carbon fiber reinforced resin fiber material to be processed into a three-dimensional mesh like a silk thread scrap of a plant. In the state where the step is provided on the lower suspension body, The fiber-shaped shock absorbers that are made to work or the human-type sleeping bag-type or clothes-type shock absorbers collide with the ground when the human-shaped head, shoulders, spine, hips, etc. fall. Acceleration sensors that detect natural fall detect the natural fall of the human body where possible, and the airbag is momentarily compressed by compressed air so that it wraps around the human body before it collides with the ground. There is a method to protect the human body, the method of high altitude that can descend parachute is the method of working in the air The parachute is equipped on the upper part of the gyro of the upper flying object, and free fall is detected by human will or by acceleration sensor Then, it is structured to open the parachute automatically, and as an emergency rescue method that the worker lost consciousness, the personal aerial work flying object is structured to safely descend with humans, the above is The gyro, which is a description of safety measures, is installed at the top of the upper aircraft and works to stabilize the upper aircraft in the air. The personal aerial work flying object suspends humans or robots or video cameras and radio control devices. Automatic flight enables observation of disaster areas and lifesaving, human or video camera and radio control device A shock absorber such as a balance ball made of rubber or silicon rubber at the lower end and sealed with air inside is installed for landing or unexpected accidents. Capacitor) or secondary battery (battery), from here it is a description of power storage device (capacitor) or secondary battery (battery), nano-between clusters in amorphous and crystalline alloys such as Ni-based and Si-based Specificity of capacitors and graphene using capacitors, and single-crystal nanocubes based on the placement, arrangement, bonding, and interface control technology of single-crystal nanocubes using nano-stacked capacitors and dielectric ceramic single-crystal nanocubes Originally bottom-up high-performance ceramic small-sized capacitor or nanotechnology ceramics, metal, carbon Accurately controlled at the atomic level of the structure of the electricity storage device for nanostructured storage capacitors, nano-stacked fuel cells, water electrolysis cells or AGM deep cycle batteries, large-capacity ceramic capacitors and solid hydrogen source type Compact and lightweight fuel cells such as fuel cells, all-solid-state electricity storage devices of complex hydride-based high-speed ion conductors, oxide-based bulk-type all-solid lithium secondary batteries, large-capacity laminated lithium batteries, lithium-ion air batteries, or lithium-ion batteries Alternatively, a nickel-hydrogen rechargeable battery, a magnesium storage battery, a non-lithium battery using a medium-low temperature ionic liquid, a metal and air battery using a high oxygen ion conductor nano thin film, a noble metal-free fuel cell using an anion exchange membrane, or an ion As a negative electrode material for a metal secondary battery in which a specific structure such as lithium and sodium is filled only in the interior of a tubular carbon nanofiber (CNF) with a unique structure that periodically possesses multiple nanogates that can only enter and exit A light, small, large-capacity battery or capacitor, such as a selectively prepared battery, described above for a capacitor or a secondary battery (battery), is placed under the shock absorber and is used for personal aerial work flights. Lower the center of gravity of the object, and the center of gravity is at the bottom to prevent the individual flying object flying from the top and bottom, preventing it from rotating in the vertical direction. Then, hang the wire or rope or wire for posture control from the bottom, and wire or rope or wire in the front, back, left or right direction Equipped with a geo-control device and a small computer with built-in automatic attitude control program, it can be controlled automatically, and the center of gravity of the flying object can be moved back and forth and left and right by pulling each rope or wire in the east, west, north, and south manually or mechanically. To control the horizontal movement of the flight, and simultaneously adjust and synchronize the motor current for levitation with the current adjustment device built in the computer to control the flight of the hovering and vertical movement. Radio control maneuvering device that enables forward, backward, ascending, descending, left and right movements as operations, such as transmitters, receivers, servos, motor amplifiers, speed controllers, wirings, connection tools, switchboards, etc. A method of automatically controlling while working with a device that combines switches and computers There are three methods for maneuvering an aerial work flying object: manual operation with a maneuvering switch provided at the hand of the passenger, radio operation with a radio control radio transmitter (propo), and automatic control with a personal computer. The rope or wire is suspended, the lower end is fixed to the ground, and the person on the ground moves by holding the lower end of the rope or wire suspended from the personal aerial work flying object to guide the movement of the personal aerial work flying object from the ground. There is a way to transmit electricity to the required height by placing a battery or power supply on the ground. Instead of using an internal combustion engine, a lightweight material such as titanium or aluminum is used instead of the electric motor of the flying object. There is a method of using a light-weight internal combustion engine made of a metal, and from here, it is a description of a forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine. High heat wear resistant parts, i.e. parts directly exposed to heat and explosion such as cylinder head, cylinder, piston, piston ring, connecting rod, crankshaft, etc. are layers of light weight metal such as titanium or aluminum around wear resistant heat resistant metal layer And steel wool rock wool glass wool thermal buffer layer and stress transmission rod that transmits explosive force to the fiber reinforced resin layer, stress is transmitted from the metal layer to the thermal buffer layer to transmit the stress to the fiber reinforced resin layer, and the metal part by forced air cooling Directly blows cold air on the casing and dissipates heat from a plurality of small holes opened in the entire casing. The casing of the entire engine has a structure in which a honeycomb structure of metal or fiber reinforced resin is shared. The outside of the titanium or aluminum layer is a thing like a heat radiating fin outside the engine of an air-cooled motorcycle. The thickness of the millimeter is about 1.95 to 3.3 mm, and a plurality of processing is performed so as to wrap the surface of the metal layer at intervals of about 1.95 to 3.3 mm. It is surrounded by a heat buffer layer in which a layer of steel wool compressed from the inside, a layer of rock wool, and a layer of glass wool is laminated to form a layer containing air, and this heat buffer layer is The inner surface of the fiber reinforced resin in contact is 19.5 millimeters to 33 millimeters high and 1.95 millimeters to 3.3 millimeters thick It is processed into a pleat shape like a heat sink fin of an air-cooled motorcycle engine at intervals of about 1.95 mm to 3.3 mm, and is wrapped with a layer of fiber reinforced resin such as heat resistant carbon fiber reinforced resin. The outside of the heat-resistant fiber reinforced resin is metal or fiber













A cylinder head made of a reinforced resin and wrapped around a honeycomb structure that takes charge of the mechanical structure related to the strength of the internal combustion engine. The steel wool layer and the rock wool layer are formed from a support portion of the metal layer to a support portion of the heat-resistant fiber reinforced resin layer, and a plurality of metal rods having a diameter of 6 to 9 mm are spaced at intervals of about 33 to 195 mm. And the glass wool layer penetrates radially like a sea urchin thorn, and the explosive force is transferred from the metal layer to the heat-resistant fiber reinforced resin layer to the metal or fiber reinforced resin honeycomb structure layer. Both ends of the bar are supported by bearings provided in the metal layer and heat-resistant fiber reinforced resin layer. There is a method in which the stress transmission rod is screwed as a bolt into the screw hole cut in the groove of the support, and the steel wool layer, rock wool layer and glass wool layer are supported by the tips of the inner and outer radiating fins from the compressed inside In response to stress, the two-dimensional or three-dimensional honeycomb structure, such as metal or fiber reinforced resin, wraps the outside of the heat-resistant fiber reinforced resin responsible for the mechanical burden. The heat-resistant fiber reinforced resin that bears a large thickness and a plurality of small holes with a diameter of about 0.195 millimeters to 3.3 millimeters that realize the overall heat dissipation in the entire honeycomb structure are spaced at intervals of about 1.95 millimeters to 33 millimeters. It is an internal combustion engine with a composite structure of open metal, fiber reinforced resin and honeycomb structure. A thin trachea with a diameter of 0.195 mm to 3.3 mm, like a feather wing, is radiated from the inside to the outside of the internal combustion engine at intervals of about 1.95 mm to 33 mm for heat dissipation. Passing through the rotating force of the internal combustion engine or the power of the turbocharger using the exhaust exhaust of the engine, the blades of the opening opened in the front part of the internal combustion engine are rotated to blow air and the diameter of the air from 19.5 mm to 33 There is a forced air cooling dedicated pipe that is distributed and branched so that air is directly blown to the metal fins of the cylinder using a millimeter forced air cooling dedicated pipe, and air is directly blown to the metal radiating fins such as titanium or aluminum surrounding the internal combustion section for forced air cooling. Titanium or aluminum radiating fins dissipate heat, and the heat dissipated air is steel wool rock woo The whole air is radiated through the heat buffer layer in the order of lugras wool, and the radiated air has a radial diameter of 0. 0 mm like a feather of a dragonfly that penetrates the honeycomb structure of heat-resistant fiber reinforced resin and metal or fiber reinforced resin. Through a thin tube of 195 mm to 3.3 mm, a plurality of heat-resistant fiber reinforced resin layers and a plurality of diameters inside the honeycomb structure layer having a diameter of about 0.195 mm to 3.3 mm or about 1.95 mm to 33 mm, or This is to dissipate the heat from the entire internal combustion engine through the small holes. This is to disperse the heat so that the resin does not melt with heat. The lower suspension body uses the internal suspension engine to place the battery and fuel tank under the shock absorber. There is a method to install the battery and the gasoline tank together, forced air cooling whole heat radiation fiber reinforced resin metal composite internal combustion machine Seki can be used as a gasoline engine or a diesel engine. Heavy electric control devices and batteries and gasoline tanks that can be placed on the ground are placed on the ground, and power transmission and fuel are supplied from the ground to the aircraft in the air. A piston engine-type or rotary engine-type internal combustion engine, combined with a generator and an electric motor, and integrated with a forced-air-cooled whole heat-dissipating fiber-reinforced resin-metal composite internal combustion engine with adjustable angular momentum Forced air cooling overall heat dissipation fiber reinforced resin metal composite rotor permanent magnet stator Electric coil disk stacked generator Motor output power transmission transmission integrated hybrid device is forced air cooling overall heat dissipation when the internal combustion engine is started up by the motor and the output of the internal combustion engine increases Inside fiber reinforced resin metal composite internal combustion engine generator motor hybrid device The torque of the internal combustion engine with a torque converter and clutch. The inner disk is made of fiber reinforced resin and the outer periphery of the disk is made of metal fiber reinforced resin. Peripheral metal detachable bouncer The metal part on the outer circumference of this bullwheel is divided into 360-degree segments of 16 degrees along the circumference, like the shield method segment. The method of increasing the amount of metal on the outer periphery, which has a structure in which the layers are radially concentrically as shown in Fig. 1, is to hook a metal segment on the outer periphery of the rotating metal and form a circular arc like a claw The claw can be moved in and out by rotating the claw.When removing the metal segment, the claw is pulled in. A segment separated by a rotatable claw provided on the outer circumferential wall of the circumferential wheel is fixed. In order to make the rotation smooth, an equally divided metal segment covering 360 degrees on the outer circumference is attached and detached at once. This mechanism can be used to adjust the rotational force of a rotating machine.An angular-momentum-adjustable flywheel is linked to a computer to adjust the angular momentum and stabilize the angular momentum, and then a part of the output of the internal combustion engine is There is a method of sending power to a dual-purpose generator and transmitting the electric power to a plurality of external electric motors. To obtain electric power, this is obtained by an internal combustion engine and then electric power is generated and fine adjustment of the output such as thrust gets thrust Combining the output of the internal combustion engine as necessary to control the energy of the electric motor as needed, the energy is totally controlled by a computer and distributed, and the motor motor angular momentum adjustment This is the description of the forced air-cooled overall heat-dissipating fiber-reinforced resin-metal composite internal combustion engine, which is a hybrid device that can be combined with a torque-driven bouncer torque converter clutch computer. Rotor permanent magnet stator electric coil disk stacking type electric motor forced air cooling whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor combined use generator and forced air cooling Total heat radiation fiber reinforced resin Metal composite internal combustion engine Angular momentum adjustable spring wheel torque converter clutch forced air cooling Whole heat radiated fiber reinforced resin Metal composite generator Motor output power transmission transmission integrated hybrid device, from here forced air cooling whole heat radiated fiber reinforced resin Metal composite rotor permanent magnet fixed The disk stacking type electric motor, which is a description of the electric coil disk stacking type electric motor, is a disk-shaped and circular shape of a metal or fiber reinforced resin whose rotor is 19.5 mm to 330 mm in diameter and 1.95 mm to 33 mm in thickness. A plurality of holes that fits into three, six, twelve, sixteen, or thirty-two discs are formed in a concentric radial position from the shaft on the inner side of a circle having a diameter of 1.95 to 33 mm. A disk that fixes a permanent magnet radially and regularly on the circumference of a concentric circle from the axis toward the axis of the axis, and a permanent magnet is fixed in as many permanent magnets as possible. The permanent magnet is embedded and fixed, and the permanent magnet is fixed so that the magnetic flux is perpendicular to the disk surface. The disk is an electric coil disk fixed to the rotating shaft of the electric motor. The electric coil magnetic flux is orthogonal to the disk and is the same size as the magnet disk, but the electric motor shaft part is a hole. An electric coil thicker than the permanent magnet is fixed at a position corresponding to the permanent magnet at a position where the permanent magnet and the electric coil face each other with a gap of 0.195 to 0.33 mm through the shaft of the electric motor. Coated copper enameled wire or a laminated ceramic type coil with nitrogen circulation glass amorphous or ceramic coating in the room temperature superconducting pipe is not formed by winding a coil but by three-dimensionally stacking a coil and an insulator to form a coil Three-dimensional solid atomic lamination technology of room temperature superconducting ceramic type ceramic coil and insulating coating ceramic at the same time There is a method that is a product formed by or making a coil female mold with a glass or ceramic with a high melting point, and a conductive material with a low melting temperature is kept in the female mold of the glass or ceramic coil and kept inert There is a method of manufacturing a heat-resistant coil made of glass or ceramic insulator by press-fitting with gas gas. A disk-stacked electric motor has holes in the central axis in which electric coils are arranged radially on the circumference along multiple circumferences. The disk is fixed to the casing of the electric motor. The disk that fixes the electric coil is made of metal or fiber reinforced resin. The permanent magnet disk and the electric coil disk are alternately stacked. The permanent magnet is fixed. The disc is sandwiched by electric coils from both sides, and the electric coil is a brushless motor that rotates the permanent magnet in phase with the rotating direction. The principle of may be a brush motor method in which a disk with a permanent magnet fixed to the casing of the electric motor and a disk with an electric coil fixed to the shaft of the electric motor may be used. Stator electric coil disk laminated electric motor has metal and carbon fiber at the top, and other parts are fiber reinforced resin and forced air cooling with blades fixed to the shaft of the electric motor. The forced air-cooled air passing through a plurality of holes opened obliquely at an angle of 90 ° to cool the disc and dissipate the heat, and the hot air radiated from the entire casing has a diameter of 0.195 mm to 3.3 mm with a diameter of 19.95 mm. Permanent magnet compared to conventional electric motor that radiates heat from the whole electric motor through a plurality of small holes opened at intervals of about 5mm to 33mm The number of electric coils is arranged with respect to a plurality of axes and the casing, and the problem of heat dissipation is solved, and the coil is inclined at an angle of 19.5 to 33 degrees with respect to the rotating surface with respect to the rotating direction of the disk. The problem of heat dissipation is solved by forming a kind of blower by rotating a plurality of holes with a diameter of about 0.195 millimeters to about 3.3 millimeters opened at intervals of about 1.95 millimeters to 33 millimeters. Depending on the method, there is a method of cooling the inside with the above method by making the electrical lead into a pipe shape.Also, the disk is a disk of a powerful electric coil, and the disk has a fixed axis with the direction of the magnetic flux of the coil being reversed for each disk. This method may provide an alternating current with a phase that rotates, all of which is a brush electric motor of an electric coil, the above is forced air cooling whole heat radiation fiber reinforced resin metal The description of the combined rotor permanent magnet stator electric coil disk stacking type electric motor, from here the bird strike prevention device fiber reinforced resin metal composite turbine stacking type electric motor, the turbine stacking type electric motor is the above disk stacking Type electric motor disk is processed into a complete blade shape, and a permanent magnet layer and an electric coil layer fixed on the blade are laminated alternately with a permanent magnet layer and an electric coil layer to make it like an intake turbine of a jet engine Can be used as a substitute for a jet engine. From here, it is a description of a bird strike avoidance device. The blade for a bird strike is made of steel, stainless steel or aluminum alloy steel with the tip that cuts the wind of the blade in order from the entire intake blade. Multistage blade shape when a bird strike occurs using a sharp blade By cutting the bird with a steel blade, the piece of meat that has been cut into pieces or minced meat pieces is provided with grooves that are likely to scatter toward the sides of the engine or motor by centrifugal force, and is guided to the position where the pieces of meat are to fly. A sensor that detects bird strikes leads the flesh of an electric motor or jet engine to a position where the flakes are likely to scatter. The conventional jet engine method is designed to minimize the damage of the engine due to bird strike by preventing the flesh of the bird from reaching the burning part of the jet engine. This is a description of the pitch angle using this device and placed diagonally The shape of a jet engine intake turbine in which permanent magnets such as neodymium magnets and layers of electric coils are alternately laminated at positions where the direction of magnetic flux is parallel to the blade rotation axis Electric motors make it easy to replace every single turbine
Complicated machine












By using fiber reinforced resin as a turbine that can control the output freely and eliminate noise problems without requiring a structure, it becomes a jet turbine-shaped electric motor without weight and noise, preventing noise that can also be used on passenger aircraft It is possible to produce a flying body using a jet turbine-shaped electric motor for noise reduction by generating electricity with a lightweight internal combustion engine of gasoline, light oil or heavy oil. Instead of aviation fuel, gasoline engine, heavy oil or light oil diesel engine can be used. It is possible to generate electricity and purify the exhaust through a soundproofing muffler and exhaust gas purification catalyst ceramic. At the same time, the aircraft can attach silicon type solar cells or polymer organic thin film solar cells to the whole or part of the aircraft on the sea of clouds to obtain electric power. Prevention of air pollution or economic fuel explosion safety It can be used to drive a jet turbine-shaped heat fiber reinforced resin-metal composite electric motor that uses a fuel-efficient internal combustion engine to generate flight thrust, or at the same time as a hybrid type jet turbine Forced air-cooled overall heat-dissipating fiber-reinforced resin metal composite internal combustion engine angular momentum adjustable flywheel torque converter clutch forced air-cooling overall heat-dissipating fiber-reinforced resin metal composite generator motor output power transmission integrated hybrid By combining the devices, the output from the internal combustion engine, power generation and transmission can be integrated and computer management can be performed, and energy distribution and sharing can be controlled, and the internal combustion engine can transmit the power to the electric motor while obtaining thrust and power. It is possible to assist battery power The above is the description of the bird strike prevention device fiber reinforced resin metal composite turbine laminated type electric motor, which can charge the battery with surplus power. From here, the turbine laminated type electric motor was used as a personal aerial work flying object The blade electric motor, which is a description of the method, is composed of permanent magnets and electric coils on the blades arranged concentrically around the circumference, and the magnets and electric coils are stacked alternately. The simplest method of the upper flying body is a method in which the upper blade and the lower blade are sandwiched so that the upper blade and the lower blade are rotated in reverse by a blade having a permanent magnet fixed above and below a disk to which the electric coil is fixed. The disk is a fiber reinforced resin, metal or metal with a thickness of 19.5 to 33 mm and a diameter of about 3300 mm And a disk reinforced with fiber reinforced resin Concentric circles along the circumference of the inner circumference of the disk and the electric coil radially, the direction of the magnetic flux from N to S is on the surface of the disk, that is, the magnetic flux is orthogonal to the surface of the disk In other words, the disk parallel to the rotation axis and radially arranged in double to triple concentric circumferences distributes mechanically to the honeycomb structure through which the wind passes (the honeycomb through which the unblocked wind passes) or fiber reinforced resin. In consideration of the wind, it has a shape in which a plurality of holes having a diameter of about 0.195 millimeters to 3.3 millimeters, which are opened at intervals of about 1.95 millimeters to 33 millimeters, or a mesh shape to support an electric coil. The path that passes is for the passage of wind that is arranged diagonally according to the pitch angle of the blade. There is an axis at the center of the disk, and the axis protrudes from the center of the two faces of the stator disk. Is a two-blade windmill with a hole through which the shaft passes in the center so that the disk of the stator's electric coil is sandwiched from above and below A permanent magnet such as a neodymium magnet faces the electric coil on the blade of this blade windmill Two blade wind turbines, in which alternating current is sent to the electrical coil located at a position where the rotation direction of the upper and lower blades are opposite to each other, are rotated on the electric coil located between 0.19 mm and 0.33 mm A blade guard that protects the blade from damage by a frame-shaped or net-shaped blade guard that prevents the entire flying object from rotating due to the air flowing in the opposite direction. An internal combustion engine generator-motor hybrid device, in which a lower suspension body is attached to the lower part of the axis of the disk of the child electric coil and constitutes a personal aerial work flying object, Air-cooled overall heat-dissipating fiber reinforced resin-metal composite internal combustion engine can be combined with the lower flying body attached to the lower part of this upper flying object to make it an individual aerial working flying object. The method of using a balloon is divided into a hot air balloon, a gas balloon, a hot air balloon and a gas balloon combined with heat and gas balloon, and the individual aerial work flight using the balloon is an upper flying body and a lower suspended body. The upper flying body that uses hot air balloons is composed of an envelope (ball skin) that contains hot air, a load tape, and a wire. The envelope material is mainly nylon or polyester that is airtightly coated with polyurethane. Gore that is made of the chemical fibers of the above and is the minimum unit of the envelope, stitched horizontally and vertically joined together. It is shaped like a sphere, bag, cylinder, or teardrop upside down that is reinforced with load tape, and the load receiving part is a load tape or carbon fiber reinforced resin made of several nylon or polyester vertically. The load tape that supports the load is sewed to the crown ring at the top of the emperope, the lower end is connected to the following backpack by the suspension cable, and the load is shared. Made of stainless steel or carbon fiber reinforced resin wire or twisted wire or Kevlar fiber reinforced resin wire or twisted wire, multiple load tapes are used in the horizontal direction to prevent the envelope from tearing. At the periphery of the burner at the opening of the envelope There is a method to replace this skirt or scoop by using a glass-squirted net of a kerosene lamp with a supplementary cloth called a triangle-shaped scoop or skirt-shaped skirt for introducing hot air. There is a method of covering the upper hemisphere of the squirt sphere made of mesh with an auxiliary cloth to make it easy to collect hot air. The part that receives heat uses a material called Menox, and the method of using a hot air balloon that is also used as a gas balloon is an envelope. Airtightly tied to the following torch with a belt, the floating gas is ejected from the torch. This envelope is mainly sewn with a thread such as polyester, and the place where heat resistance is required is sewn with a thread such as Nomex. A solenoid valve made of carbon fiber reinforced resin that exhales hot air at the top or middle of the envelope Opening and closing is controlled by manual, wireless, and automatic control. The shape of the envelope is a cylindrical shape with a diameter of about 195 to 9900 mm and a length of 1950 to 99000 mm. The body is the size of a backpack used by elementary school students, and the backpack is the size of the backpack that is carried when climbing to Everest. The belt can be joined using the buckle at the front position, the belt is wrapped from the backpack's back to the belly, the front part of the belly is fixed to the lower suspension with the buckle etc., and the part of the backpack hits the human back The belt hangs down on the seat part and the person on the two wheels provided on the seat part belt Between you can pass both feet, you can stabilize the buttocks from the shoulders to the chest and stomach and the hips will be fixed with a belt The central part of the back of this belt extends further downward and the person who carries the backpack To describe in detail how to fix the occupant to the backpack hanging the shock absorber under the legs of the backpack, the backpack is like a school bag used by elementary school students, and the occupant passes his arms through the left and right belts The left and right belts that fix the body and backpack are structured so that they can be fixed using the buckle at the chest.Because the belt extends from the left and right sides of the backpack to the left and right to fix the abdomen of the passenger You can fix the abdomen part of the passenger with a buckle at the belly, and the belt extends downward from the part where the back of the backpack hits. Two belts that can be fixed are fixed. Passing both feet through this wheel can fix the heel of the passenger. The belt extends further beyond the wheel that passes both feet. Alternatively, the center of gravity is suspended by hanging a propane gas cylinder and digestive liquid cylinder and a battery, a condenser, a power supply control device, an autopilot device, a video camera, etc. The peripheral device of the backpack is a horizontal cylindrical envelope take-up device with a horizontal length of about 1950 mm located at the top of the backpack and a guide for taking up the envelope (ball skin). There is a guide with a link shape through the envelope (ball skin) and a hopper shape with resin etc. The top end of the winder is connected to the winder by a string or wire, and is like a winder winder that winds and winds a fishing boat net. As a detailed description of the winder, the envelope winder is an envelope. The guide or hopper for winding the winder is behind the winder, and the cable that guides the wind from the top of the envelope passes through the hopper and the envelope is fixed to the rotary shaft of the winder. The envelope can be taken up together with the envelope. The envelope can be taken out by rotating the envelope winder in reverse and carrying out the envelope. Winder The envelope take-up device, which has a built-in parachute in the center of the rear and opens manually or automatically, can be moved by the motor in the backpack, and the right lever is viewed from the right side of the backpack as seen from the passenger. The right lever is extended and the switch that unwinds and winds up the envelope is attached to the right lever, and the right lever is structured to move up and down, left and right and back and forth like the control stick of a Zero-type warship fighter, and personal aerial work Since the movement of the flying object is linked to the movement of the top, bottom, left, and right, the method with multiple propellers or fans is linked with the device that changes the position of the flying object. The method with one propeller or fan on the back is the movement of the right lever back and forth. Is linked with the propeller or fan front / rear direction output and linked with the vertical / left / right rudder behind the fan guard. The position of the flying object for personal aerial work can be operated.Also, it is electrically connected to the autopilot device, and the right lever that realizes autopilot with radio control changes the vertical and horizontal positions and the left lever is roughly From the center of the upper part of the backpack, which is structured to change the vertical position, from 19.5 millimeters to 33 millimeters in length and from 195 millimeters to 3300 millimeters in length, here is a pipe-shaped metal or resin or carbon fiber called a torch. There is a cylinder that leads propane made of reinforced resin or glass fiber reinforced resin, and a small burner is installed at the top end of this torch cylinder, and an ignition device and a fire extinguishing nozzle are installed near the small burner. The left handle controls the general vertical movement of the flying object The left handle extends from the left side of the backpack, and the left lever is in a position where it can be operated with the left hand as seen from the person carrying it, and the amount of gas can be adjusted by turning the grip of the left lever. The left lever with the switch of propane gas and helium gas for raising or propane helium mixed gas has the switch of the ignition device and the fire extinguishing device. These switches and the left lever are electrically wired with the automatic control device. A valve that adjusts the amount of propane in the torch is installed on the left lever as seen from the backpack side that is in contact and realizes steering and automatic steering by radio control, and hot air or floating above the valve A valve that adjusts the amount of propane and a hot air exhaust solenoid valve that are equipped with an open / close button for the gas exhaust valve are electrically connected to the autopilot. The lower end of the torch is connected to the line and realizes manual, wireless, and automatic maneuvering. The propane gas that is connected to the maneuvering shock absorber installed under the foot of the man to be maneuvered or connected to the floating gas cylinder Around the burning part of the lead pipe is a heat-resistant material called a combustion guard net.













A net-shaped tube made of metal or fiber reinforced resin and having a diameter of 66 mm to 195 mm and a length of 195 mm to 3300 mm is installed around a small burner. When storing the envelope, the cylinder that sends propane completely fits in the center of the net tube and when using a burner, this cylindrical net extends to the top of the small burner. The combustion guard net that prevents the burner envelope from burning with the heat of the burner prevents the envelope of the kerosene lamp from igniting the glass so that the envelope does not burn with the heat of the burner. So that the lowest part of the net swells into a sphere with a diameter of 330 to 990 mm, the largest cylindrical net In the extended method, the bottom of the cylindrical mesh is attached to the periphery of a small burner that protects the periphery of the burner, and the digestive juice is ejected from the nozzle when the envelope (ball skin) burns with the heat of the burner From the center of the back surface of the backpack that is structured, the diameter of the shaft from which the shaft that rotates the prober or the fan extends is about 19.5 mm to 33 mm, and the length is about 19.5 mm to 66 mm. The electric motor described in the scope of claims of the present invention is installed horizontally in the middle of the pack. The fan guard of the domestic electric fan in which the propeller or fan of the previous period is fixed to the tip of the shaft of this electric motor A fan guard with a similar shape has a cross-shaped rudder in the direction in which the air blows out, and the side of the backpack The lever extends from the side of the backpack to the position of the right hand on the right side of the person who rides, and by moving this right lever up, down, left, and right, the rudder fixed to the fan guard guides the air blown backward, up, down, left and right The personal aerial work body moves up, down, left and right.This lever is electrically connected to the autopilot device, and the radio control and autopilot are realized. Rise and fall are roughly the passenger left hand lever valve. Adjusting the heating power of the burner at the tip of the torch by adjusting the hot air balloon's buoyancy The left lever valve adjusts the amount of floating gas such as helium and the gas balloon's method, rescue by automatic control by radio control Can be taken by aerial photography with a video camera, and can be controlled manually, wirelessly, or automatically. Equipped with shock-absorbing air bag, the upper part of the envelope unwinding / winding device is equipped with a ballet chute that detects free fall with a sensor and opens automatically by the will of the person, gas balloon method Envelope woven fiber material The base material of the balloon using a net and cloth hermetically treated with latex rubber or natural rubber is a carbon fiber reinforced resin wire having a diameter of 0.195 millimeters to 3.3 millimeters and a square having a square of 330 millimeters to 1950 millimeters. The shape of the braided net is about the same size as the hot-air balloon method. The thickness is 0.195 mm to 3.3 mm woven with polyethylene terephthalate cloth inside the mesh of carbon fiber reinforced resin wire. From the inside of a polyethylene terephthalate cloth bag Alternatively, the gas balloon is sealed with natural rubber or urethane resin to form a gas balloon. The gas balloon is heat-resistant and can be diverted to a hot balloon. It is airtight and is equipped with a helium gas or hydrogen gas cylinder instead of a propane gas cylinder, that is, the gas inside the balloon, that is, hot air is changed to hydrogen (explosion is prohibited because it explodes) or helium. Can be used, the balloon opening is a hot air balloon method that spreads and collects heated air, and the gas balloon method has a gas outlet tube inside the envelope and the gas balloon method is the tip of the opening. It is like a flare skirt that is hermetically processed with thin silicon rubber-based or rubber-based resin fibers, which can be banded This bundling method that prevents gas from leaking as much as possible in an airtight manner is only required to obtain air working time or air floating time, so it is assumed that gas leaks to some extent, an electric motor or an internal combustion engine The flying object of the personal aerial work that combines the air balloon and the balloon is divided into the upper flying body and the lower suspension body, the ice cream cup cone shaped vertical envelope storage device method is the ice cream that stores the envelope and envelope of the upper flying object An electric motor or an internal combustion engine is attached to the end of an arm that extends in a cantilever shape around a cup cone-shaped kite and a universal joint that can freely change the direction of the electric motor. Yes A propeller or fan is attached to the shaft of an electric motor or internal combustion engine. This motor motor or internal combustion engine changes the direction and moves the balloon up, down, front, back, left, and right. The lower suspension is attached to the tip of the lower part of the cup cone shape. Engine and hot air balloons or gas balloons or heat and gas combined balloons are manually, wirelessly, and automatically operated ice cream cup cone shaped bottles are made as follows. A circle with a small radius is the bottom, a circle with a large radius is the top surface, and a circle with a small radius on the bottom is a circle with a central angle of 120 degrees of the lower link where the lower ring is made of metal or fiber reinforced resin From the three pipe-divided points whose circumference is divided into three, the branch forming the ridge is about 30 to 60 degrees with respect to the ring surface Since there are two from three locations extending from left to right at an angle, there are six in total, each one forming a helix according to each angle, the tip of the helix is at 60 degrees with the upper link The six spirals connected at the outer peripheral points constitute a mesh and are regularly knitted. The intersection of the mesh is fixed with epoxy resin, etc. The lower link is divided into three parts, and the upper part is divided into six parts. The three divisions connected by the belt members knitted to each other are for description. Actually, the method in which the lower ring is divided into 12 is divided into 24 divisions, which is 12 times the upper ring. Thirteen divisions are 36 divisions. The number of lower link divisions may be any number that is dynamically adapted, and the upper part is double the number anyway. This way, the structure of the envelope and the upper flying body with the side of the frustum knitted into a bowl shape. Combine body A large trash-like object is formed in a truncated cone with a flat bottom. If you compare the point inside the tape, that is, the balloon to the earth, the balloon is reinforced with a load tape like a meridian and parallel, and it also serves as a suspension cable of metal or resin or carbon fiber reinforced resin from the intersection of the meridian and parallel Multiple flexible suspension cable wires inside this envelope where the flexible wire is suspended Rotate this roller fixed to the roller of the suspension cable take-up device installed at the lower inside of the cup cone shaped cage A cup cone with the envelope opened up by winding and unwinding the suspension cable The space between the envelope and the burner that takes heat into consideration so that the envelope does not melt with heat at the bottom of the cup cone shaped bowl that can be stored inside the cup bowl or taken out from the cup cone shaped bowl The method of using gas and heat in combination with the open burner is the tip of the burner where the gas outlet is provided inside the cup cone-shaped bowl and the gas outlet is also used as a gas outlet inside the envelope. The cup cone-shaped kite that has been guided to carry out and stored the envelope, and the small cone burner surrounded by the combustion guard net is installed at the bottom of the envelope at a distance where the envelope does not burn, the cup cone-shaped kite rises the balloon As mentioned in the scope of claims, the ice cream cup-cone type flying body is used to transmit power to the lower suspension body. It can also be used as a sealed hot gas balloon with a mixture of ropan gas and helium gas, and this technology can also be applied to airships. Manufacturing methods and constituent materials combined with each other.

The drawings are described according to the claims. Claims 1 and 2 are as follows. The personal aerial work flying object has a structure simulating the seeds of dandelions flying in the sky. FIG. 1 is an overall configuration diagram of a personal aerial work flying object simulating a dandelion seed. This figure shows the concept. FIG. 2 is an overall configuration diagram of a personal aerial work flying object of a hot air balloon and a gas balloon or a combination of a hot air balloon and a gas balloon or a helium mixed propane gas combustion hot gas balloon simulating the shape of an ice cream cone. FIG. 3 is an overall configuration diagram of an individual aerial work flying object of a hot air balloon and gas balloon or a hot air balloon and gas balloon combined type or helium mixed propane gas combustion hot gas balloon simulating the shape of an ice cream cone. It is the figure which showed that the base part of a motor became a hinge and the free position change of a personal aerial work flying object was attained by changing the inclination of an electric motor freely. From here, it is a description of the light and strong material of the personal aerial work flying object, the material form of the material of the personal aerial work flying object is equivalent to an amino acid, which has a structure simulating a chemical structural bond model of protein Primary structure, secondary structure, tertiary structure, etc., in which the basic structure such as metal, resin, or fiber reinforced resin forms a three-dimensional structure by combining multiple branches such as peptide bonds. Computer-aided mechanical structural mechanics analysis to form various forms of folds (folding) like quaternary binding side chain conformation domains (conformations), motifs (super-secondary structures), and fold proteins In order to determine and manufacture a three-dimensional structure in consideration of tension members and compression members so as to meet the mechanical needs, cutting three-dimensional modeling technology or three-dimensional three-dimensional lamination technology The term “honeycomb” used in this claim means a broadly defined honeycomb structure such as a weir ferran structure, and a hexagonal honeycomb structure, an OX structure, a flex structure, a bisecto structure, or a feather structure is laminated. The term fiber reinforced resin, including composites, is defined as a term that refers to carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin, etc. In order to achieve this, we have invented a lightweight and toughened laminated composite material using a large amount of honeycomb structure and fiber reinforced resin, and the term flying object used in the claims is defined as an object flying in the air. Various fighters or passenger planes or helicopters or airships or spacecrafts There is a method of using a waterproof paint or a weather resistant resin on the outer surface of the flying object including a method in which technology and materials of a personal aerial work flying object are applied to an artificial satellite or a space station. FIG. 55 is a cross-sectional view of a surface of a resin or fiber reinforced resin that is formed into a shape like a sea urchin spine by laser processing and a weather-resistant substance is vacuum-deposited thereon as necessary. The weather-resistant resin is made of epoxy resin, etc. on the surface using laser technology, and a large number of thicknesses and depths from 3.3 nanometers to 1.95 millimeters are cut into multiple squares on the side of the grid. The surface of a square of about 1.95 mm is cut by laser technology and cut, and the diameter of the sea urchin is about 3.3 nm to 1.95 mm and the height is about 3.3 nm to 1.95 mm. Lasers are formed by laminating layers of metal or glass such as titanium or aluminum alternately on the surface of many processed objects such as elongated thorns, or by laminating a single material to form a film and vacuum-deposited film This is a product that has improved the weather resistance of the resin by filling up the part cut out by technology as much as necessary for weather resistance and creating a laminated film with anti-oxidation and ultraviolet protection in amorphous state Resin can be a resin body weatherability surface treatment of civil engineering structures, such as steel or reinforced concrete permanent not only aircraft as because killing mold by a fiber-reinforced resin. FIG. 65 is a view showing a state in which the hopper performs weathering processing in all directions like an octopus sucker in a movable vacuum hopper vapor deposition laser sintering laminated spraying apparatus. FIG. 66 is a cross-sectional view showing the inside of the movable vacuum hopper vapor deposition laser sintered laminated spraying apparatus. Surface treatment of flying objects can be done with a movable vacuum hopper vapor deposition sintered laminate spraying device, which can be used as a substitute for painting. The problem of layer separation and layer delamination in the layered method, in which the electrostatic coating is replaced with laser technology and applied with a combination of electrocoating, is solved by cutting technology such as sea urchin spines. There is a method in which the weathering substance is made into a fine powder with a device that has a larger octopus suction cup and mixed with the solvent solvent of the adhesive and fixed on the processing surface from the nozzle to the spray processing surface and baked by the method described below or A conventional vacuum evaporation system crucible with a gimbal structure and a vacuum evaporation direction of 360 degrees is possible. -Welding sintering Laser cutting spine processing Laminating method Surface weathering processing method creates a vacuum and uses a square or conical funnel-shaped hopper with a bottom of about 195mm to 3300mm and a bottom of the silicon base Use a resin or rubber-based resin that keeps the airtightness of the octopus sucker everywhere, suck the hopper's square or conical bottom to the surface you want to weatherproof, and evacuate the internal air to create a vacuum From the top of the square or cone toward the bottom processing surface, weathering fine particles are sprayed from the nozzle at high pressure for weathering processing on the surface processing site like a cathode ray tube electron gun or charged necessary for weather resistance Atoms, molecules, or fine particles can be electrically electrostatically transported to the processing surface where the weather resistance is to be secured. Or, molecules or fine particles are driven by movement like an electron gun, and laser processing moves like an electron on the scanning line of the scanning surface of an electron gun's cathode ray tube to weld and fix objects on the processing surface. Alternatively, there is a powder electrostatic transport laser welding sintering method in which the electrostatically transported material is welded or sintered or vapor-deposited by laser technology as described above, and the weather-resistant material is fixed and fixed on the processing surface. There is also a method of vacuum vapor deposition. Resin layer or metal layer by electrostatically transporting fine powder with a resin or metal size of about 3.3 nano to 0.195 millimeters to the surface to be weathered. The resin layer or metal layer is formed by melting the surface of the metal with a laser technique and then welding and fixing or bonding by sintering. The size is from 3.3 nanometers to 0.195 millimeters. Laser technology is applied to the surface of the resin or metal laminated by laminating the resin layer or metal layer by the method described above by electrostatically transporting the fine fiber fragments charged to the order of 1 torr to the processed surface electrostatically. A number of grooves with a thickness of 3.3 nanometers to 0.195 millimeters are cut into a plurality of grooves, and a square surface with a square side of about 3.3 nanometers to 1.95 millimeters is observed with a laser technology. A number of objects such as sea urchin elongated spines having a diameter of about 3.3 nanometers to about 1.95 millimeters and a height of about 3.3 nanometers to about 1.95 millimeters are machined and cut. Attaching and removing the metal necessary for weather resistance, such as titanium or aluminum metal or glass, with a gimbal crucible and evaporating it to form a vacuum space by charging these metal vapors. This method includes the method of vapor-depositing a weathering substance directly after laser spine processing on a substrate, which is a method of performing weathering processing on the surface of a resin, fiber reinforced resin or metal by vacuum deposition inside a movable hopper. The above-described series of processes that can be applied not only to a flying object but also to an existing structure can be performed by an automated robot. The above is a description of the light and strong material of the flying object for personal aerial work. FIG. 79 shows a method for manufacturing dentures applying the beam theory on an elastic floor, which is a description of a silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part metal ceramic composite laminated denture manufacturing method. Shock absorption layer Honeycomb structure layer Fiber resin layer Interlocking part Metal ceramic composite laminated denture manufacturing method is to place on the gypsum male mold manufacturing base around the gums and gum roots in the human oral cavity Spraying a layer of release material onto a gypsum gum mold and then laminating from a soft resin to a hard resin, the layering method is elastic so that when the force is applied to the denture, the force is applied to the entire gum. The first layer in which the denture contacts the gums is a medically safe silicone rubber sucker layer that is foamed over it. A relatively thin thickness of 1.95 mm to 3.3 mm made of a fiber reinforced resin on a honeycomb structure provided with a honeycomb structure layer as an intermediate layer on a stress buffer layer such as a tongue. This is a denture surface layer made of fiber reinforced resin, and the fiber reinforced resin also has a tooth portion at the tooth portion. FIG. 81 is a diagram showing a layer of only a joint portion made of metal, porcelain or ceramic safe for medical use. Only the meshing portion at the top end of the tooth is a metal having a thickness of about 0.195 to 3.3 mm, sintered metal, metal ceramic, porcelain, ceramic, or a composite of these metals and ceramic. The entire denture is soft enough to move about 0.195mm to 0.33mm when the fingers are pinched like a mouthpiece made of resin, metal, and ceramic. When a force is applied to the denture with a denture that can be deformed, a shock absorber is applied to the shock absorbing material that can transmit the force to the fiber reinforced resin through the honeycomb structure and distribute the force to the entire gum. A denture with the characteristics of medical foaming resin, and the inner surface of the denture of medical foam resin is made of medical silicone rubber and has good adhesion By removing the air inside the dentures from the gums, it has a structure that sucks into the gums just like a suction cup, and a piece of rice cracker etc. enters between the gums and dentures and has a structure that does not hurt, laser cutting technology The metal or ceramic or metal-ceramic composite that forms the complete tooth shape of the engagement portion is only the engagement portion, and the resin of the engagement portion is processed like the sea urchin spine described in the claims. Apply the necessary amount of titanium on the resin, or apply adhesive to the meshing part and apply titanium powder, sinter the denture surface with laser technology, or make the meshing part thin with a thin horseshoe shape. A method may be used in which the fiber-reinforced resin is fixed using an adhesive with an insertion device in which the center of the teeth is returned. Fig. 80 is a metal that gently stabilizes the dentures on the upper and lower sides of the dentures of the silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part metal ceramic composite laminated denture, and the surface of the temporomandibular joint is covered with a shock absorbing material It is the figure which showed that can be moved freely. Steel or spring material or body temperature with a shock absorber attached to the back of a shape memory alloy coated with resin so that the upper and lower dentures can move softly at the end of the dentition and memorized at the temporomandibular joint along the temporomandibular joint A metal material coated with a shape memory alloy wire or plate resin or shock absorbing material that has been memorized in (3) is embedded in the denture, and the force of adhering the denture to the palate with the viscosity of saliva is gently applied by the restoring force of the metal Functional dentures with a denture that stabilizes the denture in the palate and infiltrate the denture resin with a medical effect or a refreshing substance are also included in this method. It is possible to manufacture functional dentures that are comfortable without being damaged by tough and hard objects. Silicone rubber sucker layer Shock absorption layer Honeycomb structure layer Fiber resin layer Interlocking metal ceramic A manufacturing method in which a metal, a resin, a shock absorber, and a silicone rubber sucker layer that stabilize dentures on and under the metal layer are separately manufactured and assembled using a medical adhesive such as an epoxy resin is also included in the scope of the present invention. The above is a laminated sectional view showing a silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part metal ceramic composite laminated denture manufacturing method. The application of laminated honeycomb structure fiber reinforced resin composite technology of personal aerial work flying object described in this claim can be applied to denture manufacturing method applying beam theory on elastic floor. From here, silicon rubber sucker layer impact Absorption layer Honeycomb structure layer Fiber resin layer










Mating section metal ceramic composite laminate


Silicone rubber sucker layer Impact absorbing layer Honeycomb structure layer Fiber resin layer Interlocking metal ceramic composite laminated denture manufacturing method is a description of the denture manufacturing method. The method of laminating from a soft resin to a hard resin on top of spraying a release material layer on the male mold of gypsum gum after placing it on the male mold manufacturing base received force by engaging the denture The first layer in which the dentures contact the gums is a medically safe silicone rubber sucker layer on top of it that uses the theory of beams on elastic floors to force the force across the gums. A relatively thin layer of 1.95 mm made of fiber reinforced resin is provided on the honeycomb structure by providing a honeycomb structure layer as an intermediate layer on the stress buffer layer such as urethane foam. This is a denture surface layer made of fiber reinforced resin with a thickness of about 3.3 mm from the tower. The fiber reinforced resin is also made of fiber reinforced resin, and only the engagement portion at the top end of the tooth is 0.195 mm. To 3.3 mm thick metal, sintered metal, metal ceramic, porcelain, ceramic, or a composite of these metals and ceramic, and the entire denture is like a mouthpiece made of resin, metal and ceramic When the denture is pressed with a denture that is soft enough to move about 0.195mm to 0.33mm when the fingers are pinched, and the resin part can be bent at the same time. The shock absorber transmits the force to the fiber reinforced resin through the honeycomb structure and distributes the force to the entire gum. A denture with a stress buffer layer made of shock absorbing material, and the inner surface of the dentures of the medical foam resin is made of medical silicone rubber and has good adhesion. Metal or ceramic or metal ceramic that has a structure that sticks snugly, and a piece of rice cracker etc. enters between the gums and dentures so that it does not hurt and forms a complete tooth shape with laser cutting technology Only the meshing part becomes a composite, and the resin of the meshing part is processed like sea urchin spine as described in the claims on the resin to deposit the necessary amount of titanium in the meshing part. Apply adhesive, apply titanium powder, sinter the denture surface with laser technology, or make only the meshed portion into a thin horseshoe shape with titanium It may be fixed by using an adhesive with an insertion device with a reinforced resin with a return at the center of the teeth. The upper or lower dentures are covered with resin so that the upper and lower dentures can be moved softly along the temporomandibular joint. A steel or spring material with a shock absorber attached to the back of a shape memory alloy memorized at body temperature, or a metal material coated with a resin or shock absorber of a shape memory alloy wire or plate material memorized at body temperature. The force of attaching the denture to the palate with the viscosity of saliva by gently embedding it in the denture is gently supplemented by the restoring force of the metal, and the denture resin is stabilized in the palate and penetrates the substance that makes the denture resin have a medical effect or refreshment Functional dentures are included in this method, and it is possible to produce functional dentures that are comfortable, strong, light and tough and hard to bite. Silicon rubber sucker layer Shock absorption layer Honeycomb structure layer Fiber resin layer Interlocking metal ceramic layer Metal, resin, shock absorber and silicon rubber sucker layer that stabilize dentures on the upper and lower sides are manufactured separately for medical use such as epoxy resin The manufacturing method of assembling using an adhesive is also included in the scope of claims of the present invention. The above is the description of the manufacturing method of the metal-ceramic composite laminated denture of the silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part. The following is a description of a material in which the surface of a honeycomb structure made of wood, paper, resin, foam resin, etc. is reinforced and reinforced with fiber reinforced resin. Fig. 67 shows how the resin is pressed into a wood conduit or a teacher's tube and hardened to process the wood, then a number of holes are drilled like a honeycomb structure to reduce the weight, and then the periphery is covered with fiber reinforced resin. It is sectional drawing reinforced. As the structure of the flying body, curable resin is press-fitted into a solid wood conduit and a teacher's tube, and a small number of hexagonal holes such as honeycomb structures with sides of about 1.95 to 33 mm are made. Thickness on the surface is filled with foaming resin such as urethane foam, or the outer surface is made of fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin instead of foamed resin. It is a product that is hardened by coating reinforcement with millimeters. Fig. 68 shows 1 to 3 atmospheres in the adhesive between wood and wood made of plywood, laminated wood, or the above-mentioned solid wood reinforced with resin and made numerous holes to make a honeycomb structure. Spheres made of resin, such as spherical or polyhedral polyethylene terephthalate, with a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 3.3 millimeters, encapsulated in compressed air or gas The outer surface of the product which is cured by sandwiching and reducing the weight by mixing and adhering the material of the particle shape of 3.3mm thick with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin It is sectional drawing of the thing hardened by covering reinforcement from 195 millimeters. Alternatively, plywood, laminated wood, or the above-mentioned solid wood is reinforced with resin and innumerable holes are drilled into a honeycomb-like wood-to-wood adhesive that is compressed from 1 to 3 atm. Spherical or polyhedral resin spheres such as polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and a diameter of 0.195 millimeters to 3.3 millimeters encapsulated in air or gas are small crushed egg grains The outer surface of the product cured by sandwiching the material reduced in weight by mixing and adhering the material of the material with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin is 3.3 mm to 195 mm thick It is a thing hardened by covering reinforcement with. FIG. 69 shows a structure in which paper such as corrugated board is laminated and air is contained and hardened with an adhesive, and a structure like a honeycomb structure, that is, a hexagonal hole or round hole like a hexagonal hole in the honeycomb structure is made into corrugated cardboard. In order to make a plurality of holes with an interval of 19.5 millimeters to 33 millimeters, a plurality of small holes such as hexagons or circles with one side of a hexagon or a circle having a diameter of about 1.95 millimeters to 33 millimeters are formed to reduce the weight. The surface of the reduced material is reinforced with foamed resin such as urethane foam, or the structure of the honeycomb structure in which a plurality of small holes in the paper are provided with a plurality of holes spaced from 19.5 millimeters to 33 millimeters. The outer surface of the foamed resin that is reinforced by replacing the square holes with circular holes is wrapped with a metal or paper honeycomb structure, and then the carbon fiber reinforced resin There is a cross-sectional view of what hardened coated reinforced at 195 millimeters thick 3.3 mm in fiber reinforced resin such as glass fiber reinforced resin. Or, paper such as cardboard is laminated and hardened with an adhesive such as epoxy resin to reduce the weight by making many small holes such as hexagons with sides of 1.95mm to 33mm in the honeycomb structure etc. The outer surface of the object reinforced with foamed resin such as urethane foam or the foamed resin reinforced with paper is made of fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin with a thickness of 3.3 to 195 mm. It is a thing hardened by covering reinforcement with. FIG. 70 shows that a paper having a thickness of about 0.195 mm to 3.3 mm is used in a corn flake shape of food having a square or rectangular side of about 1.95 mm to 33 mm or used in office work. Add paper to the paper shredded with a shredder and stir to make the paper crumpled or wrap around the curled air, making it half soft and fluffy with the fibers of the paper loosened. About half soft and fluffy paper fibers are loosened and mixed with air with an epoxy resin adhesive and stirred, compressed and solidified appropriately and molded into a member of the required strength is light and internal There is a cavity in the paper, and the required strength is obtained by adjusting the amount of adhesive, and the paper is cut into this cone flake shape and mixed with air and stirred. In order to reduce the weight after forming a member compressed by mixing the adsorbent into the mold, a small hole with a side of about 1.95 mm to 33 mm, such as a circle diameter or a hexagon, from 19.5 mm A thing similar to the honeycomb structure with a plurality of intervals of 33 mm, that is, a hexagonal hole in the honeycomb structure is replaced with a circular hole, and the outer surface is covered with foamed resin and the outer surface is resin, fiber reinforced resin or paper Alternatively, a cross-sectional view of an object in which a metal honeycomb structure is attached and wrapped and then the surface is coated and reinforced with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm. It is. Stir paper that is 0.195 mm to 3.3 mm thick and cut into cornflakes of square or rectangular foods of about 1.95 mm to 33 mm, or shredded with paper shredder used in office work Then, the paper is crumpled or curled up and wrapped in air to make it soft and fluffy by half and this object is stirred with an adhesive such as epoxy resin and compressed appropriately and hardened The molded material is light and has a cavity inside, and the required strength can be obtained by adjusting the amount of adhesive, and the hexagonal shape is obtained by compressing the agitated paper and adhesive, cut into a cone-flake shape. For example, the outer surface of the surface is reduced in weight by drilling a number of small holes with a side of about 1.95mm to 33mm. A method using a material obtained by solidifying coated reinforced at 195 millimeters thick 3.3 mm in fiber reinforced resin such as fiber reinforced resin or glass fiber reinforced resin as a member. FIG. 71 shows a tape in which paper or a fiber-containing tape or a film material such as a fiber reinforced resin is wound while winding the material between the tapes so as to wind nori-maki sushi in a cylindrical shape, and a tape to be wound from now on. Pressure gas made of resin such as polyethylene terephthalate having a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 330 millimeters, in which compressed air or gas of 1 to 3 atmospheres is enclosed between Is encapsulated in the shape of a small crushed egg with a number of children, or a sphere or polyhedron with a size of about a tennis ball to a volleyball or a diameter of a polyhedron and a fiber shape of 0.195 microns to 3.3 mm Chemical fiber or natural fiber with a tensile force of the size of cotton Mix together the appropriate amount of an adhesive such as epoxy resin, soak in the air and stir the resin-filled pressure gas into the gap between the cotton-like fiber and resin. A honeycomb structure made of paper, resin, or metal on the outer surface of a fiber reinforced membrane material tape or a commercially available tape that is filled with air and packed with air and packed with air. The outer layer of the honeycomb structure is 3.3 mm to 195 mm thick and coated with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin. FIG. Compressed air or gas of 1 to 3 atmospheres is enclosed between a tape in which paper or a fiber-containing tape or a tape of a membrane material such as fiber reinforced resin is wound in a cylindrical shape and a tape to be wound from now on. An object encapsulated in a resin pressure gas such as spherical or polyhedral polyethylene terephthalate having a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 330 millimeters is like a small crushed egg grain shape A sphere or polyhedron with a size of about 10 to 10 inches or a volleyball, and a fiber made of a chemical fiber or natural fiber having a pulling force of about 0.195 mm to 3.3 mm in diameter, such as cotton. Mix together an appropriate amount of adhesive such as epoxy resin Stir and solidify the gap between the products filled with pressure gas made of resin by packing the material filled with cotton-like fibers and adhesive such as resin between the tapes of fiber reinforced membrane materials or commercially available tapes. Paper or tree around the outside of the object










Made of fat or metal


The layer of the honeycomb structure is formed by bonding with an adhesive such as an epoxy resin, and the outer surface of the honeycomb structure has a thickness of 3.3 to 195 mm, and fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin The structure of the flying body is paper, incombustible paper, aramid paper, resin or metal honeycomb structure, and the outer surface of the honeycomb structure is made of fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin. There is a method of using as a member a material which is reinforced by covering and reinforcing at a thickness of 3.3 mm to 195 mm. FIG. 72 is made of resin such as spherical or polyhedral polyethylene terephthalate having a diameter of 1.95 to 33 mm and a thickness of 0.195 to 3.3 mm in which compressed air or gas of 1 to 3 atm is enclosed. Spherical shape of a small crushed egg like a number child and a fiber-like diameter of 0.195 microns to 3.3 millimeters of pulling chemical fibers or natural fibers like cotton Mix an appropriate amount of an adhesive such as epoxy resin and stir it while containing air, and then the cotton-like fibers and the adhesive such as resin moderate the air between the objects filled with resin pressure gas. It is a white thin film that is an aggregate of eggs of a number of children as a result of forming the shape of the member and containing air in an adhesive with an appropriate amount of air. An object that is shaped like an elongated lump of as many litters as it is encased and put into a mold before the adhesive hardens to form the necessary parts and contains air to harden the object FIG. 2 is a cross-sectional view of the outer surface of the substrate wrapped with a honeycomb structure and coated with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin with a thickness of 3.3 to 195 mm. Spherical or polyhedral polyethylene terephthalate such as polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and encapsulated with compressed air or gas of 1 to 3 atmospheres is a numerator. A small crushed egg-like product such as the above and a fiber-like diameter of 0.195 microns to 3.3 millimeters of chemical fiber or natural fiber in the form of cotton are suitable. Mix the amount of adhesive such as epoxy resin and stir to form the shape of the member that is filled with cotton-like fibers and resin or other adhesive in the gap between the objects filled with resin pressure gas As a result of being hardened with adhesive, the shape is like an elongated lump of a litter of a litter of a litter encased in a thin white film that is an assembly of a litter of litters The outer surface of the object formed in the shape of the required member by putting it in the mold before the adhesive is cured is 3.3 mm to 195 mm in thickness with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin. There is a method of using a covering-reinforced object as a member. FIG. 73 shows a honeycomb structure formed by bonding a layer of a honeycomb structure made of foamed resin such as polystyrene foam or urethane foam and made of paper, resin or metal around the foamed resin with an adhesive such as epoxy resin. FIG. 2 is a cross-sectional view of a product whose outer surface is coated and reinforced with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin having a thickness of 3.3 to 195 mm. The center member inside the flying body is made of foamed resin such as styrene foam or urethane foam, and the honeycomb structure layer made of paper, resin or metal is bonded around the foamed resin with adhesive such as epoxy resin. The outer surface of the honeycomb structure is 3.3 to 195 mm in thickness and coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin, or compressed air of 1 to 3 atm. Alternatively, gas encapsulated resin spheres such as spherical or polyhedral poly (ethylene terephthalate) with a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 330 millimeters may be small crushed eggs or tennis The size of the ball is about the size of a volleyball A shape or polyhedron with a fiber diameter of 0.195 micron to 3.3 mm in size, a chemical fiber or a natural fiber made like cotton and mixed with an appropriate amount of adhesive and stirred. Adhesives such as epoxy resin with a honeycomb structure layer made of paper, resin or metal around this outer surface that fills and hardens the gap between spherical or polyhedron filled with chemical fiber cotton and adhesive agitated The outer surface of the honeycomb structure is 3.3 to 195 mm thick and coated with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin, or paper, resin or metal The above is a description of a light and tough composite material. There is a method of using the above-mentioned members in combination as a member of the air vehicle, which is a description of totalization and structural strengthening. The surface of these air vehicle members has a diameter of 1.95 mm to 33 mm for the purpose of reinforcement or lightning protection. The aircraft wire is embedded with piano wire or steel wire rod for prestressed concrete, pre-tensioned, and then the fiber resin is hardened, and then the stress is controlled by the computer using a strain gauge or the like. In this method, the air pressure drops and the force that causes the member or body to swell and the force that suppresses the pretension bulge of ano wire or prestressed concrete steel wire may be antagonized. Prevents the aircraft from tearing apart In the event of a crash, the flight structure is made of steel, steel, aluminum, stainless steel, titanium, ultra-light, high-performance, general-purpose magnesium alloy, or other materials that have been rolled or forged. Use. FIG. 74 shows a method of using a three-dimensional three-dimensional lamination technique using a framework structure of a three-dimensional honeycomb structure such as a wire-ferran structure with a metal such as steel using a molten metal lamination forging fixation technique. The technology is a net-like laminated metal that can be poured into the molten metal that is to be laminated with a mesh shape of about 0.195 mm to 33 mm in height using a ceramic mold as in the 3D printer laminating technology. The bottom surface of the ceramic mold that can be extruded and kept at a high temperature below the melting point is a mesh-shaped nozzle-shaped mold with a cross-section of the honeycomb structure cut horizontally, and the upper surface of the ceramic mold is a hopper-shaped ceramic. A ceramic mold is placed horizontally on the production base using a mold, and a small amount of metal such as molten steel is poured into the inert gas from above. It is a cross-sectional view of the ceramic molding frame for forming a shape of the quick withdrawal mesh of metal cold lump ceramic molding frame, such as molten steel subjected to press-injection towards the underside. From here, there is a method of using a framework of a three-dimensional honeycomb structure such as a wire-ferran structure with a metal such as steel using a molten metal lamination forging and fixing technique, which is a description of a three-dimensional three-dimensional lamination technique. Lamination forging fixation technology uses a ceramic mold like the lamination technology of a three-dimensional printer, and has a net shape into which molten metal to be laminated can be poured in a mesh shape of about 0.195 mm to 33 mm in height for each layer. The bottom surface of the ceramic mold form that can be extruded is a nozzle-shaped mold form with a cross section that is cut horizontally through the honeycomb structure to be formed, and the top face of the ceramic mold form is formed on the production base using a hopper-shaped form form. A ceramic mold is placed horizontally, a small amount of molten steel or other metal is poured into it, and injection injection is performed from the top to the bottom with an inert gas. A machine that adjusts the metal such as steel of the mesh shape drawn on the production base to the extent that the mesh shape becomes slightly thicker according to the shape of the mesh of the ceramic mold, and the metal such as the molten steel quickly cooled and solidified The mesh figure to be formed with a driving computer controlled hammer is forged while maintaining its three-dimensional shape, and a large number of thicknesses and depths of about 3.3 nanometers to 0.195 millimeters using laser technology on the upper surface of the forged metal A square surface with a side of about 3.3 nanometers to about 1.95 millimeters is cut out by laser technology, and the long and narrow sea urchin diameter is about 3.3 nanometers to about 1.95 millimeters. The ceramic mold, which was cut out like a thorn with a length of 3.3 nanometers to 1.95 millimeters and then laser-processed and lifted, gives high-frequency vibrations and is made of extra metal. After cleaning the ribs, the ceramic mold is lowered onto the forged mesh-shaped metal layer, a small amount of molten metal is poured into it, and press-injection is performed with an inert gas. The tip of a plurality of elongate barbs laser-processed to the above-mentioned dimensions is poured into the eye-shaped metal, and some of the barbs are melted by the heat of the molten metal and are bonded to the next layer, whereby the previous layer and the next layer A machine-driven computer-controlled hammer that adjusts the degree of striking and the upper layer that has been fixed is forged with a three-dimensional shape, and the surface of the grid is cut with the above-mentioned dimensions by laser technology on the surface. Weer-Ferrand structure made of metal, such as steel, forged by repeating this series of operations to improve the bite with the next molten metal by forming a plurality of elongated barbs and changing the plurality of ceramic molds Which metals by the three-dimensional honeycomb structure, such as forged steel can be obtained. FIG. 75 shows a method of exchanging a plurality of ceramic molds in accordance with the type of each layer to be laminated in a three-dimensional honeycomb structure. The ceramic molds move up and down, front, back, left and right while connecting the ceramic molds as many as the number of faces in a continuous manner and shifting the position of the ceramic molds up, down, front, back, left and right. After pouring the molten metal to be laminated onto the base with the substrate, pulling up the ceramic mold, cleaning of the ceramic mold by vibration of the ceramic mold, forging of the laminated metal surface and laser cutting spine machining It is a figure which shows that the process of a series of flow work is possible by shifting a formwork up and down, front and back, and right and left. The method of exchanging a plurality of ceramic molds according to the type of each layer of the three-dimensional honeycomb structure is a continuous strip of a plurality of forming molds corresponding to one unit of the honeycomb structure, which is formed into a strip shape Move the metal mold up, down, front, back, left, and right while shifting the position of the molding mold, and then pour the molten metal onto the substrate, clean the ceramic molding mold by the vibration of the ceramic molding mold, perform forging and laser processing In addition, the series of flow work steps can be automated by shifting the mold form vertically and horizontally. FIG. 76 shows a steel sheet laminating laser melt forging laminating technique in which a sheet of metal to be laminated such as a mesh shape of steel or the like is laminated like a three-dimensional printer, and the laminating surface is partially melted by the laser technique and then forged. A 3D honeycomb structure to be virtually formed on the manufacturing base is virtually placed on the manufacturing base, and the virtual 3D honeycomb structure is cut into a cross-sectional shape cut by the first horizontal plane and punched and sheared. Place a sheet of metal, such as steel, with a thickness of about 1.95 microns to 33 millimeters, such as a mesh-shaped steel, on the manufacturing base, and place it on the first level. A sheet of metal, such as steel, with a thickness of about 1.95 microns to 33 millimeters in the shape of a cross section of a three-dimensional honeycomb structure cut horizontally A metal sheet such as steel that has been punched and sheared by Ng shear is placed on the second stage, and the center of the mesh is melted by laser technology along the shape of the second stage sheet, and the upper stage This second stage of forging while maintaining the solid shape by hitting the mesh of a metal sheet such as steel that has been cooled and brought to an appropriate temperature after being melted and fixed to the lower sheet with a machine-driven computer-controlled hammer with an appropriate hitting condition On top of this, a virtual three-dimensional honeycomb structure on the third horizontal plane is cut horizontally, and a sheet of steel, such as steel with a thickness of about 1.95 microns to 33 mm, is punched with a punching shear. Lay the center of the mesh with laser technology along the shape of the mesh of this third stage sheet with a sheet of metal such as steel that has been meshed into the upper stage.













Repeat the operation of forging while holding the solid shape by hitting the mesh of a metal sheet such as steel, which has been cooled and brought to an appropriate temperature after being melted and fixed to the corrugated sheet, with a mechanically driven computer controlled hammer This is a diagram showing a steel sheet laminating laser melt forging laminating technology that can automate a series of flow work processes that can be replaced with metal sheet layers while forging a virtual three-dimensional structure. is there. Laminated steel sheet melting and forging technology is a method of laminating and forging a metal sheet to be laminated, such as a mesh shape of steel, like a 3D printer. It is a 3D honeycomb that you want to form virtually on the manufacturing base. The structure is virtually placed, and a virtual three-dimensional honeycomb structure is cut in the horizontal plane of the first stage. A metal sheet is placed on the production base and the first level is the first level. On this first level, the virtual three-dimensional honeycomb structure on the second level is cut horizontally. This second sheet net is made by punching a sheet of metal such as steel with a punching shear and placing a sheet of metal such as steel made into a second stage. A machine-driven computer with moderate hitting of the mesh of a metal sheet such as steel that has been cooled to an appropriate temperature after melting and fixing the upper and lower sheets by laser technology along the shape of the steel The virtual three-dimensional honeycomb structure on the horizontal plane of the third stage is horizontally cut on this second stage, which is forged while maintaining the three-dimensional shape by hitting with a control hammer. A metal sheet such as steel is punched out with a punching shear and a metal sheet such as steel is placed in the third stage, and the center of the mesh is formed by laser technology along the shape of the third stage sheet. After melting and fixing the upper and lower sheets, the mesh of a metal sheet such as steel that has cooled down to an appropriate temperature is hit with a machine-driven computer-controlled hammer with an appropriate hitting condition. Laminated forged steel that can automate a series of flow work processes that replace a metal sheet layer while forging a virtual three-dimensional structure by repeating this operation of forging while maintaining a solid shape A three-dimensional honeycomb structure such as a forged ferrule structure made of metal such as can be applied to a flying body or a frame member of a large passenger aircraft. From here, it is a description of aircraft design method and aircraft technology. The design philosophy of aircraft must be strong to some extent with a lightweight structure that contains many cavities inside a passenger aircraft, etc. The outer shell of the passenger plane that must be strong is deformed by the deformation of the skeleton of a three-dimensional honeycomb structure such as Weir Ferran structure in which metal such as laminated forged steel is forged when the passenger plane crashes with the ground There are three-dimensional honeycomb structures such as Wier-Ferrand structures that absorb and reduce the impact energy to some extent. FIG. 57 is a cross-sectional view of an aircraft fuselage and exoskeletons of both wings in a skeleton like a kite woven with bamboo members using a belt member. You can see the floor and the wall that supports the floor under the ceiling and the wall that supports the ceiling. In order to conserve fuel, both wings are divided into a three-section wall-like skeleton, and the joints between the wings are reinforced with belt material. Fig. 58 shows an exoskeleton such as a kite braided with bamboo members using belt members, reinforcement of the aircraft fuselage, both wings, fuselage, belt members of the wings, and reinforcement of the fuselage, tail, fuselage, and tail members of the belt. The appearance of the entire exoskeleton can be seen. FIG. 59 is a cross-sectional view of the exoskeleton of the aircraft fuselage. The exoskeleton is wrapped like a bamboo basket with a belt member. The belt member is a bundle of wires bundled in parallel with each other, and has a honeycomb structure for receiving a compressive load. A buffer is visible on the inside and outside of the belt member. On the outside of the cushioning member, a fiber reinforced resin skin is visible and a piano wire or prestressed concrete steel wire net is visible in the skin. The inner surface of the fiber reinforced resin can be seen inside the buffer member. A skeleton wing that is processed into a belt-shaped member and that forms the outer wall of the aircraft is knitted while laminating heat insulating materials and fiber reinforced resins to the outside of the skeleton like an aircraft heel and toward the inside of the skeleton The intersection of the belt and the belt is cured and fixed using epoxy resin etc. when the aircraft's kite is completed The belt member knitting this kite is first knitted into the shape of the aircraft and can be stroked as a whole On the outside of the skeleton of the belt member that is shaped like an aircraft, industrial gel material, kanenite (registered trademark), urethane foam, or a resin ball that can withstand changes in atmospheric pressure between the ground and the sky. 1.95 to 33 millimeters in diameter, filled with compressed air or gas at 3 atmospheres, 0.195 to 330 millimeters in sphere Or a polyhedral polyethylene terephthalate or other resin-filled pressure gas is a small crushed egg particle shape or a ball or polyhedron with a size from about tennis ball to volleyball. Mix the chemical fiber or natural fiber like cotton with a pulling force of 0.195 microns to 3.3 millimeters in diameter, and mix with an appropriate amount of an adhesive such as epoxy resin. Using a material filled with an appropriate air containing a cotton-like fiber and an adhesive such as a resin in the gap between the materials filled with pressure gas made of resin and stirred, the resin used as a shock absorber When the ball crashes due to a collision with the ground, a shock absorber more than absorbs energy by sticking is stuck, and a fiber resin is placed outside the shock absorber Skin is kept the safety of the passengers is pasted endothelial inner wall of fiber reinforced resin sandwiching the shock absorber inside the backbone of it and the cage and the outer wall. FIG. 60 is a cross-sectional view of a belt member that knits a basket like a bamboo basket. The tension portion is enclosed in the mantle with a rheological body that is bundled by assembling steel wires. The compression part has a honeycomb structure, and a flexible honeycomb structure such as a resin surrounds a rigid section such as a metal. In the middle you can see the substrate of fiber reinforced resin. A steel wire and a honeycomb structure are attached to the base material with an epoxy resin or the like. The belt member is strong and can knit the structure like a fold. FIG. 101 is an enlarged view of a cross-sectional view of a sandwich belt member, which is a belt member for knitting a ridge structure in which a honeycomb structure in which wires such as front and back steel are bundled in parallel is fixed with an epoxy resin or the like. FIG. 102 is a cross-sectional view of a fuselage of a flying object having an exoskeleton obtained by knitting a sandwich belt member like a bamboo basket. From the analogy of H-shaped steel, it was found that sandwiching a honeycomb structure with a steel wire like a sandwich is more advantageous for deformation. This is called a sandwich belt member. This skeletal belt is like a hand-knit sweater made of aggregate steel wire or wire manufactured by a method in which metal wires such as piano wire or prestressed concrete steel wire are bundled in parallel, like muscle fibers on the outside. A strong belt member with a metal honeycomb structure and a fiber reinforced resin honeycomb structure arranged in a balanced manner such as the hard and soft parts of the turtle shell. There is a method in which the wire pulling part of the belt, which is a bamboo-like skeleton knitting bamboo bamboo, is bound in a belt shape like a muscle fiber in parallel like a bundle, and the wire is hand-knitted There is a method of knitting like a sweater. Between the wires processed by these two methods, a rheology body is filled and the rheology body is made from a resin mantle. There is a method of wrapping the wire so that it does not leak. There is a method of replacing the rheological body that is reducing the fatigue failure of the wire with a fiber reinforced resin, that is, a wire such as steel bundled in a parallel bundle and a hand-knitted sweater. The wire is knitted like a wire or hand-knit sweater, the outer side receiving the tensile force of the belt, which is a method of placing the knitted wire in the fiber reinforced resin, bundled in parallel with the belt shape The honeycomb structure in which the honeycomb material is used for the inner part of the belt that receives compressive force with the wire rod is surrounded by the resin honeycomb structure so as to surround the section of the metal honeycomb structure from the surroundings. Look at the turtle shell here Around this hard hexagonal shell with a turtle shape, a soft growth layer surrounds the hard hexagonal section to form a honeycomb structure. Combined by the belt member of the honeycomb structure is a slight, bendable supple. FIG. 56 shows that a portion subjected to tension with a material corresponding to a bamboo material of a bamboo basket knitting a cocoon member is a material obtained by binding a steel wire material in a bundle or a material knitted like a hand knitted sweater is a portion subjected to compressive force By placing a flexible honeycomb structure around the rigid honeycomb structure, this belt-like member can bend flexibly and the middle of the honeycomb structure is a substrate such as a fiber reinforced resin belt with epoxy A steel wire fixed with an adhesive such as a resin is one in which a rheological body that suppresses fatigue failure is encased in a resin mantle or contained in a fiber reinforced resin. Furthermore, like the H-shaped steel, the rheological body, the steel wire, then the fiber reinforced resin substrate, then the rigid and flexible honeycomb structure, so that the member can withstand the alternating stresses of compression and tension Next, the belt member is used in a more mechanically advantageous manner by the method in which the honeycomb structure is sandwiched with the wire material such as steel from both sides. In this claim, which is an easy-to-use material, this member is called a sandwich belt member. The rheological body of a sandwich belt member has a method of replacing it with a fiber reinforced resin. Mainly refers to the sandwich belt member, and the inside of the cage where the skeleton of the aircraft made by knitting bamboo baskets is made by the belt member is a wide sky It is a cave, as if the fuselage, both wings, and the tail are all mechanical structures. It is designed so that the entire aircraft, which is the masterpiece of bamboo bamboo weaving so that it can withstand fatigue of repeated loads, is distributed in a distributed manner as seen in the workmanship, is well balanced. FIG. 61 is a cross-sectional view of the outer wall of an aircraft, which is formed by knitting the shape of an aircraft with a belt member like a bamboo fence, and wrapping the skeleton like a fence with a belt member from inside and outside with a shock absorber. Piano wire or prestressed concrete steel wire is embedded in the outermost skin where fiber reinforced resin is bonded to the outside and inside with epoxy resin, etc., preventing the members from being shredded when the aircraft collides with the ground. This piano wire or prestressed concrete steel wire counteracts the force of the aircraft expanding above. This metal net prevents lightning strikes. This method is like a float of a Nebuta Festival. Fiber-reinforced resin such as paper is covered on a skeleton like bamboo fence, and piano wire or prestressed steel wire is pretensioned inside the fiber-reinforced resin of the outermost skin. (Technology to harden the fiber reinforced resin after applying tension to the steel wire in advance) It is embedded in the fiber reinforced resin layer in the form of a mesh, that is, the outermost skin is centered on the network of piano wire or prestressed steel wire Because it is made of fiber reinforced resin, it will not break into fine dust at the end of the crash.In addition, the outer skin is a fiber reinforced resin sandwich structure with a shock absorber sandwiched around the kite skeleton as described for the safety of the flying object, so it will clash Fiber reinforced resin skin wall shock absorber 籠 shape skeletal shock absorber fiber reinforced resin inner wall is deformed in the order of energy to absorb and crush energy However, in order to reduce the weight of the conventional aircraft, the design method is outward from the center, where the skeleton is rigid and the outer skin is fragile. Traditional aircraft design methods that wrap up from the outside should be revised with respect to human life rather than the economy. FIG. 82 is a cross-sectional view showing that there is a method in which the internal space, which is a cross-sectional view of a sandwich belt member-exoskeleton spherical flying object, is used for multiple purposes and used in multiple stages on a honeycomb structured floor. FIG. 83 shows a sandwich belt member-applied exoskeleton sphere-shaped flying object having a configuration in which a head portion, both wings and a tail portion are attached to a spherical passenger portion, and has a size of about a jumbo jet (registered trademark). The large space is used for multiple purposes and has a bowl shape













It is possible to construct a plurality of floors by supporting the floor of the honeycomb structure with the walls and floors of this structure. It is an external view of a skeleton. As an application of the sandwich belt member, the sandwich belt member 籠 exosphere spherical flying object has a configuration in which the head, both wings and tail are attached to the spherical passenger part, and has a size similar to a jumbo jet (registered trademark) The wide space is used for multiple purposes, and it is possible to construct a plurality of floors by supporting the honeycomb structure floor with the ridge-shaped walls and floors.This method is versatile because the inside of the wing can take a large space Used. FIG. 84 shows an application of a sandwich belt member. Thick flying squirrel simulating the total lift. A flying object simulating a thick flying squirrel with a skeleton-like exoskeleton is a stubby body with a rounded body like a goldfish and thick wings. FIG. 2 is a cross-sectional view of the fuselage of this flying object that obtains lift by generating a pressure difference between the upper and lower parts of the entire flying object according to Bernoulli's theorem. FIG. 85 shows an application of a sandwich belt member. Thick flying squirrel simulated whole body lift acquisition Flying object is a flying object simulating a thick flying fish with a skeleton-shaped exoskeleton. Is a diagram in which the entire flying object has a structure like a cross section of a wing according to Bernoulli's theorem, and the body of this flying object that obtains lift by generating a pressure difference between the upper and lower parts is cut in the direction in which the flying object travels . FIG. 86 shows an application of a sandwich belt member. Thick flying squirrel simulated overall lift acquisition The flying object is a flying object simulating a thick flying fish with a skeleton-like exoskeleton. According to Bernoulli's theorem, the entire flying object has a structure like a cross section of the wing, and the flying object that gains lift by generating a difference in pressure between the upper and lower parts is knitted into a saddle shape using a sandwich belt member. FIG. As an application of a sandwich belt member, a thick flying fish model gains overall lift.The flying object simulates a thick flying fish with a skeleton-like exoskeleton, and the flying object has a rounded trunk like a goldfish and both thick wings are Bernoulli's theorem The entire flying object is structured like a cross section of the wing, and the difference between the upper and lower air pressure is generated and lift is obtained. The tail of this flying object obtains rotational force by forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine Forced air cooling Overall heat dissipation fiber reinforced resin metal composite rotor Permanent magnet stator Electric coil Disc stacked type Electric motor is used as a generator to obtain power, and then using that power, the bird strike prevention device fiber reinforced resin metal composite turbine A large internal space where a flying object simulating a thick flying fish can move forward by sending wind backwards with a laminated electric motor A wall or floor or honeycomb structure of cage-shaped knitted sandwich the belt member can be utilized to partition versatile. FIG. 87 is an application of a sandwich belt member. Thick flying squirrel simulated whole body lift acquisition The flying object is a flying object simulating a thick flying fish with a skeleton-shaped exoskeleton. Is a diagram in which the entire flying object has a structure like a cross section of a wing according to Bernoulli's theorem, and the body of this flying object that obtains lift by generating a pressure difference between the upper and lower parts is cut in the direction in which the flying object travels . FIG. 88 is a diagram in which a bird strike prevention device fiber-reinforced resin-metal composite turbine laminated electric motor is attached to the tip of both wings of a flying object simulating a large flying fish simulation overall lift. FIG. 89 is a diagram in which a bird strike prevention device fiber-reinforced resin-metal composite turbine laminated electric motor is attached to the rear end of the fuselage and the horizontal tail wing of a flying object that has obtained a total flying force simulation of a thick flying fish. FIG. 90 is a diagram in which a bird strike prevention device fiber reinforced resin-metal composite turbine laminated electric motor is attached to the tip of both wings, the rear end of the fuselage, and the tip of the horizontal tail of a flying object that has obtained a total flying force simulating a large flying fish. At the tail of this flying object, a forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine is used to obtain rotational force, and a forced air-cooling whole heat-dissipating fiber-reinforced resin metal composite rotor permanent magnet stator electric coil disk stacked electric motor as a generator A flying object that simulates a thick flying fish can move forward by sending wind backward with a bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor using that power after obtaining power with the method used It is the figure which showed that. Bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor is attached to the tip of both flying wings, the tip of the horizontal tail and the tail of the fuselage simulating this flying skeleton with a thick skeleton. Can do. FIG. 91 is a cross-sectional view of a flying object that can be suspended from a ballast suspended fuel generator ballast with a parachute installed on a part of the outer periphery of a sphere center disk, a plurality of duct fans, and a disk part of the outer periphery of a fan disk. It is. FIG. 92 is a cross-sectional view of a wing-shaped portion of a disk around a sphere of a flying object that can be dropped with a fuel generator ballast suspended by a parachute-installed fuel generator ballast with a wing-shaped part of the outer periphery of a sphere center disk and a plurality of duct fans. FIG. 93 is a cross-sectional view of a sphere-centered disc outer peripheral plural duct fan disc outer peripheral part wing-shaped leaf fall falling mitigation parachute installed fuel generator ballast suspended falling flying object horizontally at the center of the disc. FIG. 94 shows a ball center disk outer peripheral multiple duct fan disk outer peripheral part wing-shaped leaf fall falling mitigation parachute installation fuel generator ballast hanging dropable flying object disk outer peripheral part duct fan multiple installations between duct fans This parachute is opened at the time of fall, and the parachute upper part is opened with a wire at the time of fall to induce the fall of the spherical disk, falling down like a flutter and a leaf fluttering, and reducing the collision with the ground It is a storage part. This contains a float that spreads like an air bag when it touches the sea. Fig. 95 shows the ball center disc outer peripheral multi-duct fan disc outer peripheral part wing-shaped leaf fall falling mitigation parachute installation fuel generator ballast hanging dropable flying object disc outer peripheral part duct fan multiple installations between duct fans This parachute is opened at the time of fall, and the parachute upper part is opened with a wire at the time of fall to induce the fall of the spherical disk, falling down like a flutter and a leaf fluttering, and reducing the collision with the ground It is a figure that a spherical disk dances in the air, like a flutter and a leaf flies in the air. In FIG. 96, the bottom end of the sphere has a structure in which heavy objects such as generator fuel can be installed and can be suspended at the bottom like a ballast tank. This ballast part that suspends the center of gravity and prevents the entire disk from rotating to the top and bottom can be dropped separately from the spherical disk body in a safe position to reduce the weight when falling. It is the figure which showed the thing which relieve | moderates the impact at the time of the fall by providing the impact-absorbing layer in the part of the ball | bowl which the lowermost periphery of this ball | bowl which can be suspended was cut off. Fig. 97 shows the outer periphery of the spherical disk of the spherical disk of the sphere center of the spherical disk of the fuel generator ballast suspended fallable fuel generator ballast suspended parachute installation parallax installation part of the outer periphery of the sphere center disk multiple duct fan disk outer periphery part wing shape FIG. FIG. 98 is a cross-sectional view of a wing of a disk portion of a flying object that can be dropped with a fuel generator ballast suspended by a parachute installed fuel generator ballast with a parallax installed part of the outer periphery of a sphere center disk and a plurality of duct fan disks. 99 shows that the duct engine is structured such that a plurality of duct engines are blown to the lower part of the outer periphery of the disk part, and a cross-shaped beam is provided in the middle of the cylindrical height, and above and below the center of the cross. Forced air-cooling of two rotary engines or twin-type horizontal pistons, fixed heat-dissipating fiber reinforced resin-metal composite internal combustion engine, fixed around the outer periphery of this disk with two upper and lower fans rotating inside a cylindrical shape It is sectional drawing of the duct fan which obtains levitation | floating force with several duct fans. FIG. 100 shows a duct engine having a structure in which a plurality of duct engines are blown and floated on the outer peripheral portion of a disk portion, and a cross-shaped beam is provided in the middle of a cylindrical height and above and below the center of the cross. Forced air-cooling of two rotary engines or twin-type horizontal pistons, fixed heat-dissipating fiber reinforced resin-metal composite internal combustion engine, fixed around the outer periphery of this disk with two upper and lower fans rotating inside a cylindrical shape It is the figure which looked at the duct fan which obtains levitation force with a plurality of duct fans from above. As an application of the sandwich belt member, the center of the sphere-shaped exoskeleton is a sphere and the outer periphery of the sphere has a disk shape. The dropable flying object has a structure in which the exoskeleton of the flying object is blown to the lower part by a plurality of duct engines and floats on the outer periphery of the disc part where the exoskeleton of the flying object is knitted with a sandwich belt member. A cross-shaped beam is provided in the middle of the center, and two rotary engines or a forced-air-cooling whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine of a twin-type horizontal piston is fixed above and below the center of the cross. A long runway is necessary to obtain levitation force with a plurality of duct fans around the outer periphery of this disk, which is a duct fan that rotates inside the shape. Instead, the four upper, lower, left, and right bird strike prevention devices fixed at the boundary between the spherical surface and the disk with respect to the direction of travel of the sphere The fiber reinforced resin metal composite turbine laminated electric motor moves forward by sending the wind backward and the outer periphery of the spherical disk The left and right sides of the wings are processed into wing shapes, and there is also a method of extending both the left and right wings long.There are four bird strike prevention devices Fiber reinforced resin Metal composite turbine Stacked electric motor According to getting forward speed by sending wind backward Multiple ball chutes are installed between the duct fans on the outer periphery of the disk, which can reduce the burden on the duct fan by obtaining the buoyancy of the wings. Opening the mouth of the top of the parachute with a wire during the fall induces the fall of the sphere disk, crashes like fluttering leaves and leaves flutter, and collides with the ground The bottom of the sphere to be summed is a structure that can be suspended at the bottom like a ballast tank by installing heavy objects such as generator fuel, and when the airflow is bad, the weight part such as generator and fuel of the ballast is The ballast that prevents the whole disk from rotating to the top and bottom by lowering the center of gravity of the suspension, and the structure that can be dropped separately from the spherical disk body in a safe position to reduce the weight when falling The ball part where the lowermost periphery of this suspendable sphere is cut off is provided with a shock absorbing layer, and the inside of the sphere is a sandwich belt member that alleviates the impact when falling It is partitioned by a wall or floor of a kite made of or a honeycomb structure plate and is used for multiple purposes Safely and comfortably about 900 people in a single flight that does not collide with the ground and crash into the ground in the event of a crash Fuel that has a structure that can be transported can use heavy oil, light oil, or gasoline, and exhaust gas passes through a muffler with a built-in catalyst, so if it crashes on the sea to mitigate quiet air pollution, air back from the bottom of the disk part This spherical disk is essentially a watertight and airtight structure that floats on water, but is a description of aircraft design methods and aircraft technology. FIG. 77 shows that the vacuum deposition layering technique draws a figure using metal fine wires in the shape to be vapor-deposited, charges the metal thin wires as electrodes, and charges the vacuum-deposited material on the opposite pole to the porcelain vapor-deposited material. The crucible lid in the shape of a crane neck flask is brought into close contact with a normal crucible that prevents the entire diffusion of the material to melt and evaporate in the crucible that prevents the entire diffusion of the deposited material, and the tip of the crane neck is opposite to the potential of the deposited material. There is a method of drifting the nozzle from the movable conduit with the diffusive force to evaporate the deposition material led to the nozzle having the reverse potential of the deposition material through the conduit having the nozzle and reaching the target electrode from the nozzle. Like a crane-shaped flask-shaped three-dimensional printer, the nozzle-shaped vapor deposition material outlet at the tip of the crane-neck selectively and intensively descends directly above the target thin line and scatters to other parts. In accordance with the shape of the electrode of the fine wire that is charged by concentrating and depositing the vapor deposition material that manages a small amount with a device such as a camera shutter on the target fine wire at the top by electrostatic force and depositing the thin wire on top of each other Vapor deposition is performed and a three-dimensional solid shape is formed by the vacuum vapor deposition material, or the method of using conductive ink instead of the target thin line draws the vapor deposition target figure and charges the figure like a three-dimensional printer.













The figure is vacuum-deposited as described above, and a figure to be laminated like a three-dimensional printer is drawn on the target figure so that it is further laminated, and the figure is charged, and the top figure is intensively vacuum-deposited from directly above. It is the figure which showed that the laminated three-dimensional structure by a vacuum evaporation substance can be formed by repeating this. The vacuum deposition lamination technology draws a figure using metal thin wires in the shape to be deposited and charges the metal thin wire as an electrode and charges the electrode on the opposite side of the electrode to form a vacuum-deposited material like a three-dimensional printer. The shape of the electrode of the fine wire that is charged by lowering it from the jet outlet directly above the target fine wire and concentrating it on the target fine wire at the top by electrostatic force and depositing the thin wires on top of each other. Vapor deposition is carried out according to the above, and a three-dimensional solid shape is formed by the vacuum vapor deposition material, or the target figure is drawn by drawing a vapor deposition target figure using a conductive ink instead of the target thin line like a three-dimensional printer. Draw a figure to be laminated like a three-dimensional printer on the target figure so that it is further vacuum-deposited and further laminated as described above, and charge the figure to concentrate on the topmost figure from directly above Laminate the three-dimensional structure by vacuum deposition material by repeating this vacuum deposited can be formed. FIG. 78 shows that a method of applying silver clay technology to three-dimensional laminating mixed paper or resin fiber nonwoven paper with a fine powder of metal to be laminated with an oily or water-soluble air contact curable curing agent. Draw a figure that you want to stack on paper placed on a manufacturing base using ink or resin fiber nonwoven paper like a 3D printer, and 3D the figure you want to stack and stack another piece of paper on the figure you want to stack Like a three-dimensional printer, the amount of ink is adjusted so that the curable ink drawn like a printer penetrates between the fibers of the paper and the ink of the upper paper and the lower paper is blended. Draw a figure with a printer.Draw a figure with a curable ink containing fine metal powder to overlap the paper on this paper. Repeat this to obtain a paper or resin fiber nonwoven paper that is laminated and cured. The sintering furnace with paper The purpose of using paper or resin fiber nonwoven paper to burn a resin fiber nonwoven paper and sinter-bond the metal to obtain a three-dimensional structure is to reduce the lamination time, secure the ink width, and the three-dimensionally laminated method. Paper that has been printed in a fixed position around the figure to be laminated for smoothness of the surface, and a plurality of spot-like dots are printed to harden the bundle of paper and the point cloud is laminated to form a column. The above is a cross-sectional view showing a new three-dimensional lamination technique, in which the shape is protected and the bundle of cured paper is easily transported until the bundle is sintered. The method of applying silver clay technology to three-dimensional lamination is to use ink containing a fine powder of metal to be laminated with oily or water-soluble air contact hardener on paper or resin fiber nonwoven paper. Draw a figure you want to laminate on paper or resin fiber nonwoven paper placed on the manufacturing base like a 3D printer, and add another sheet of paper on the figure you want to laminate like a 3D printer Adjust the amount of ink so that the curable ink containing fine metal powder penetrates between the fibers of the paper and the ink of the upper paper and the lower paper fits in, and shapes it with a printer like a three-dimensional printer Draw a figure with a curable ink containing fine metal powder that you want to laminate and laminate the paper on this paper. This is repeated to obtain a product in which paper or resin fiber nonwoven paper is laminated and cured. With paper or tree The purpose of using paper or resin fiber non-woven paper to obtain a three-dimensional structure by burning fiber non-woven paper to sinter-bond the metal is to reduce the lamination time, ensure the width of the ink, and smooth the surface of the method of three-dimensional lamination For this reason, by printing a plurality of spot-like dots at fixed positions around the figure to be laminated, when the bundle of paper is cured, the point group is laminated and cured into a columnar shape to form a laminated bundle of paper. Protecting the shape until it is sintered and making it easy to transport a bundle of hardened paper. The above is a description of the new three-dimensional stacking technology. This is the description of the aircraft structure. Is a fiber reinforced resin such as resin, carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin, or a combination of these metals, resin or fiber reinforced resin materials, or epoxy resin. for A layer of metal and resin layers that are layered together like a ground layer, or a combination of fiber materials such as aramid fibers, or a braided fiber material As a member for knitting a material solidified with resin as a member for knitting into a cocoon structure, using a material formed by extruding with metal, or by assembling thin metal pipes into a resin, and using a resin solidified by sealing, or using a honeycomb Use a honeycomb sandwich structure in which both sides of the structure plate are sandwiched between plate materials such as fiber reinforced resin and bonded with epoxy resin, or the honeycomb structure / plate material / honeycomb structure / plate material are alternately layered. Also, the outer surface of the three-dimensionally machined material that has been laminated with a milling machine etc. is a fiber reinforced tree such as carbon fiber reinforced resin or glass fiber reinforced resin. There is a method of using a material that is hardened by covering and reinforcing with a thickness of 3.3 mm to 195 mm with a fat, or a weir ferran structure in which a weir ferran structure is formed like a panel is a basic structure of a honeycomb structure There is a method of forming a panel shape using a weir ferran structure which is made of a three-dimensional structure by bonding polygonal members that form a structure with an epoxy resin, sandwiching a weir ferran structure panel between fiber reinforced resin plates The outer surface of the structure or three-dimensionally machined one obtained by laminating these layers alternately with a milling machine is 3.3 mm thick with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin. There is a method of using a material that has been hardened by covering and reinforcing at 195 millimeters as a member. In order to prevent fatigue in places where repeated fatigue is likely to occur, the energy of fatigue rupture that can be expanded and contracted intentionally is prevented so as to prevent stress concentration where the pipes are aggregated according to the flow of stress in the bundle and bonded with epoxy resin between the pipes. Rather than just a single wire with a rheological layer like the muscle-tendon relationship that absorbs soft and highly viscous mucous, it is not a single fiber, but a simple aggregate, not a single compact Dispersion of stress concentration in each part of the assembly by providing a rheological layer such as a muscle-tendon relationship that absorbs fatigue fracture energy and absorbs the energy of fatigue fracture in the gap between the body laminate and none 3D honeycomb structure that prevents the progress of fatigue failure and balances the mechanical strength, or a combination of these layered hierarchical structure and 3D aggregate structure. This composite structure can also be used for aircraft using a composite structure made of a three-dimensional aggregate structure object that prevents fatigue failure in the compression part and bonded with epoxy resin as a composite structure. The impact energy to the passenger when the air vehicle or aircraft crashes against the ground by providing a layer of shock absorbers, ie a rubber heel assembly with a diameter of 195 to 330 millimeters and a thickness of 1.95 to 3.3 millimeters The shock absorbing material sandwiched between the wall and the center of the wall that relaxes and secures the passenger's living space encloses air like a balance ball, rubber, resin, Kevlar fiber, silk, cotton fiber, chemical fiber, etc. The above is a description of the structure of the aircraft and the above is the description of the aircraft or aircraft. The personal aerial work flying object, which is a description of totalization and structural strengthening, is composed of an upper flying body and a lower suspension body, and the upper flying body corresponding to the fluff (crown) part of the dandelion ascends as its configuration form A method of using an electric motor, a method of using an internal combustion engine, a method of using a balloon, a method of using a balloon and an electric motor, or an internal combustion engine, or a combined device combining an electric motor, an internal combustion engine, a generator and a balloon The description of the combined device is divided into the following, the balloon is divided into hot air balloon, gas balloon or hot gas combined balloon method, in order to increase the rising efficiency, helium is mixed and burned and heated to use helium This hot gas technology used on ice cream cones below, including the enclosed sealed hot gas balloon method, is also used on airships. The upper aircraft is equipped with a gyro that stabilizes the upper aircraft, a parachute that can be used manually or automatically for emergency methods, and a blower to obtain lifting force. From here, the method of manufacturing a propeller or fan, the blower is a propeller or fan that is made by processing solid wood according to the description of the above composite material and cutting or pouring resin into a mold, or titanium or aluminum or Made of metal such as stainless steel or ultralight high-performance general-purpose magnesium alloy, or carbon fiber reinforced resin, or a material that is a combination of these materials. The method of combining the materials here is the propeller or fan. In the cross section in the radial direction from the axis to the outer circumference Cutting materials such as milling machines, laser technology, scanning electron microscope technology, and tunnels with pipes with hollow diameters of 0.195 mm to 3.3 mm gathered in the direction along the flow of force and epoxy resin hardened Using a molecular manipulator that combines effects, atom implantation technology, molecular insulators and molecular beams, or a nanorobot such as a ribosome that automatically transports and manufactures molecules, the atoms or molecules are carried and the molecules are assembled and arranged in three dimensions according to the molecular structure design method. The inside of the pipe is a three-dimensionally formed into the shape of a propeller or fan blade using a technology that constructs the molecule itself with a three-dimensional printer atomic layering technology at the molecular level (can be used for manufacturing room temperature superconducting materials, especially ceramics). Because it is a hollow, it is lightweight and at the same time conforming to the stress flow Another composite method that is tough because it is a collection of thin pipe materials with a holder is a three-dimensional formation of a honeycomb structure of paper, resin or metal into the shape of a propeller or fan blade using a cutting machine such as a milling machine The outer surface has a thickness of 3.3 mm to 195 mm and is coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin, and another composite method is the flow of stress in the radial direction of the fiber material. The propeller or fan is formed in the direction along the direction, and then the resin is poured between the fibers and hardened. The lifting device of the upper flying object is strong against rotation. These propeller or fan and electric motor The above is the manufacturing method of the propeller or fan, and from here is the description of the lightweight and powerful electric coil and the entire forced heat radiation, Some motors use commercially available motors, but new fiber-reinforced resin electric motors use copper, gold, room-temperature superconducting materials, etc. Superconducting coil or steel that prevents melting by heat through a conductor coating material such as an amorphous processed object or the like where the center of the conductor is formed into a pipe shape and the inside of the conductor pipe is forcibly air-cooled or water-cooled or liquid helium or liquid nitrogen Metal or carbon fiber reinforced resin such as aluminum or titanium or ultralight high-performance general-purpose magnesium alloy, or a combination of these, the electromagnetic part of the electric motor is replaced with metal and carbon fiber, and other structural materials are replaced with fiber reinforced resin Lightweight and strong motor coil There is a method of forced air cooling in which the blades forcibly air-cooling with a small blade that forcibly blows air into the electric motor and forcibly air-cooling the coil directly are forced air cooling from the outside of the electric wire and the inside of the pipe of the electric wire. The fiber reinforced resin that is the structure of the composite material is a composite material that considers weight reduction and heat dissipation by opening a small hole with an infinite number of diameters from 0.195 mm to 3.3 mm and releasing hot air from the entire electric motor There are multiple brushes made of material, or multiple brushless electric motors, or multiple electric motors that combine these brushless motors and brushless motors. The air blower of the upper flying object, which is a description of the powerful electric coil and the entire heat dissipation of forced air, has a fan and a motor. Fan motor integral or fans there into the blower or those exhaust intake is upward as blowing direction of the blower was adjusted downward or ducts became
Ductow












The lower suspension corresponding to the seed of dandelion is constructed in a structure that allows humans to work in the air freely, allowing the person to carry or suspend the air, The assembled method, the method of stacking honeycomb structures such as honeycomb sandwich panels or weir ferran structure panels, the method of assembling cocoon-shaped objects, or the method of assembling a combination of pipe structure, honeycomb structure and cocoon structure The method of using a pipe structure to form a framework as a structure is divided into a method of assembling a pipe member and fixing it with a rigid connection or a fixture, and a method such as carbon fiber reinforced resin or glass fiber reinforced resin. Manufactured with fiber reinforced resins and integrally formed by autoclave formation, etc. that is baked under pressure in a large kiln at the factory As for the outer shape of the upper aircraft, the outer shape is maintained in the range of 195 mm to 3300 mm in width and depth and 195 mm to 3300 mm in height, and the inside is formed with a hollow or a framework. There is a method, the appearance shape of the upper flying body is a sphere. FIG. 15 is a sphere of the upper flying object of the personal aerial work flying object. FIG. 24 is a diagram in which a plurality of horizontal disks are installed inside a sphere in which the upper flying object of the personal aerial work flying object is framed by the meridian and latitude lines of the globe, and a plurality of propellers or fans are installed in the disk. . FIG. 25 is a diagram in which a plurality of horizontal disks are installed in the frame of the upper flying object of the personal aerial work flying object along the rotation quadratic curve, and a plurality of propellers or fans are installed in the disk. FIG. 26 is a diagram in which a plurality of propellers or fans are installed along the inner side of the semicircular net of the upper flying object of the personal aerial work flying object. FIG. 27 is a diagram in which the upper flying object of the personal aerial work flying object vertically connects the spheroids. FIG. 28 is a diagram in which the upper flying object of the personal aerial work flying object has a spheroid shape. The upper flying object has a donut shape, that is, a torus, a torus, a spheroid, a spheroid, a quadratic surface, or a cuboid. FIG. 16 is a diagram in which the upper flying object of the personal aerial work flying object is a rectangular parallelepiped. FIG. 63 is a diagram showing an internal skeleton in the case where the upper flying object of the personal aerial work flying object is a cylinder. FIG. 62 is a diagram showing the relationship between the internal skeleton and the propeller or fan and the electric motor when the upper flying object of the personal aerial work flying object is a quadrangular prism. FIG. 17 is a cross-sectional view of the upper flying body of the personal aerial working flying object, which is a rectangular parallelepiped. The horizontal member for rigid connection rigidly connected to the vertical center member is passed through the horizontal member for fixation and fixed with a fixture. Then, it is the figure which installed the electric motor and the propeller or the fan in the both ends of the horizontal member for attachment or detachment. The upper flying object is a cube, a polyhedron, or a polygonal column or a cylinder of this size. FIG. 19 is a diagram in which the upper flying object of the personal aerial work flying object is cylindrical. FIG. 23 is a diagram in which the upper flying object of the personal aerial work flying object connects a plurality of cylindrical shapes horizontally. FIG. 21 is a conical view of the upper flying object of the personal aerial work flying object with the conical bottom surface up and the apex down. FIG. 29 is a diagram of a shape in which the upper flying body of the personal aerial work flying object is formed by connecting the bottom of the cone to the upper and lower surfaces of a cylindrical shape in which both ends of a short pencil are sharpened. FIG. 30 is a diagram in which a cylindrical portion is shortened in a shape in which an upper flying body of a personal aerial working flying object is formed by connecting a cylindrical bottom surface to upper and lower surfaces of a cylindrical shape in which both ends of a short pencil are sharpened. . FIG. 31 shows a combination of a cone and a cylinder in which the upper flying object of a personal aerial work flying object has a short pencil core facing upward. Combining these three-dimensional shapes with a method of using a cone, a truncated cone, or a quadrangular pyramid as the upper flying object, the upper flying object is cut into a cone shape with the sharp apex of the conical shape or the ends of a short pencil. A shape with a conical bottom connected to the upper and lower surfaces of a cylinder, or a shape with a conical bottom connected to a lower surface of the bottom of a short pencil, or a large abacus ball A method of forming a solid having a shape in which the bottom surfaces of the larger ones of the truncated cones are bonded together and using them alone. FIG. 36 is a view of an upper flying object in which abacus balls are vertically connected. The upper flying object is a method that uses large abacus balls connected vertically, or spheres are vertically connected, or spheres or spheroids are assembled like a large bunch of grapes, or a cylindrical and conical solid. There is a method that is the shape of an assembly using a combination of a sphere or a spheroid, the upper aircraft is a method of assembling pipes, the framework of the upper aircraft is a horizontal member, a vertical member, a propeller or a fan guard member As a method for joining members, metal members such as stainless steel wire, piano wire, resin, chemical fiber, carbon fiber reinforced resin, etc., having a diameter of 0.195 millimeters to 3.3 millimeters are used. The joint is wound around the joint and is knotted, and the nodule is hardened with epoxy resin from the top of the knotted wire. Or, there is a method of bonding with epoxy resins, rigid bonding by welding between resins or metals, or fixing with aluminum screws or fixing tools. Fixtures are steel clips, resins, carbon fiber reinforced resin, glass fiber reinforced resin This is an assembled method that combines, etc. This is a personal aerial work flying object at the site of aerial work or flight leisure by fixing the detachable member to the rigidly connected member with a detachable fixing device that facilitates disassembly It can be assembled quickly and easily. The upper diagram in FIG. 18 is a diagram in which the horizontal member for attachment / detachment is inserted into the horizontal member for rigid connection at the center of the vertical member and fixed with a fixing tool. A horizontal member for attachment / detachment is inserted from the center and two attachment / detachment horizontal members are brought into contact with each other in the center and then fixed with a fixing tool. The figure below shows one attachment / detachment horizontal member in one horizontal attachment member. It is the figure which was fixed with the fixing tool after inserting. The horizontal member of the upper flying body is divided into a horizontal member for rigid connection, a horizontal member for attachment / detachment, and a horizontal member for guard of a propeller or fan. The vertical member is divided into a central vertical member and a peripheral vertical member. As shown in FIG. 18, the detachable horizontal member for fixing the electric motor so that the upper flying body can be assembled and disassembled is a detachable horizontal pipe in the pipe of the rigid horizontal member rigidly connected to the vertical member. The center vertical member is passed through the middle of the detachable horizontal member, and then the rigid horizontal member and the detachable horizontal member are fixed by the fixing tool, and then the electric motor is fixed to both ends of the detachable horizontal member. Alternatively, the electric motor is first fixed to one end of the detachable horizontal member, and then the end other than the end of the detachable horizontal member to which the electric motor is fixed is rigidly connected to the vertical member. The center vertical member is inserted into the center of the central vertical member and fixed with a fixture and the two horizontal members for detachment are abutted at the center of the central vertical member, or the horizontal member for detachment with the electric motor fixed is attached to the central vertical member. Of rigid horizontal materials There are two methods for attaching and detaching the horizontal member for fixing the electric motor. One method is to use the pipe member alone, or the horizontal member for supporting the electric motor is a truss structure. There are two methods of assembling, that is, using a detachable horizontal member alone or a method of assembling a truss structure. The shape of a horizontal member stacked in multiple stages from the top down is the shape of an equilateral cross, Star shape (hexagram) or pentagram, or the inside of a polygon that combines a triangle and a diagonal line inside a polygon such as a ten-valve, twelve-valve, sixteen-valve, thirty-two-valve flower pattern, or octagon There are methods that have a mesh or mesh shape combining polygons and diagonals with different shapes and sizes, these shapes can be disassembled and assembled, these various objects The horizontal shape of the shape is shifted or the vertical position is shifted so that the propellers or fans do not come into contact with each other and are stacked so that the steps are stacked vertically. Multiple propellers or fans are installed on a horizontal member or a horizontal member that is a combination of a triangle and a diagonal line inside a polygon such as an octagon. The flow caused by the interference of wind aerodynamically blown in the horizontal and vertical directions is arranged while slightly shifting the position in the horizontal and vertical directions, taking into account the thrust of ascending and the stable balance of the flying object. The upper aircraft is constructed by stacking horizontal members of this equilateral cross shape or a polygon that combines polygons and diagonal lines in multiple layers. The vertical member is composed of the central vertical member, the peripheral vertical member, and the above-mentioned fixture, and the rigid horizontal pipe is screwed to the central vertical member. Further, it is rigidly connected by welding or adhesion by epoxy resin, and the rigidly connected portion is reinforced by a plate member or a rib member. FIG. 64 is a cross-sectional view of a horizontal member when an upper flying body of a personal aerial work flying object is assembled in a well beam. The shape of the central vertical member is a prism or cylinder, or a three-dimensional girder structure in which a horizontal member and a vertical member are assembled. There is a method in which these shapes are combined. In the method in which the central vertical member is a prism, the cross-section of the central member is a Chinese character mouth or a rice field. One side is 33 mm to 66 mm. The vertical length is 195 mm to 3300. There is a method of using an equilateral angle pipe made of aluminum of about millimeters, carbon fiber reinforced resin, glass fiber reinforced resin, resins, foamed resins, or a combination of these materials vertically. The meaning of combining materials is the empty of the kanji mouth of the aluminum pipe or the cross section of the rice field. The method of the central member of the cylinder, including the method of pouring urethane and carbon fiber reinforced resin into the part and curing it, is from about 66 mm to 99 mm in diameter, from 1 mm to 6 mm in thickness and 195 mm in length. 3300 mm waterproof paper, rolled paper tape rolled into a cylindrical shape, or a composite material or aluminum made of the above film material, carbon fiber reinforced resin, glass fiber reinforced resin, or the above composite material This means that the cylinders are vertically used with a single material or a combination of these materials, and the meaning of combining is to include a method of pouring foamed resins or carbon fiber reinforced resins into the hollow part of an aluminum cylindrical pipe and curing it. Do these holes on the sides of these prisms or cylinders Open the horizontal member for rigid connection to the vertical member and insert the pipe of the horizontal member for rigid connection into the prism or cylinder in order from the direction of east, west, south, north, or eight directions so that the branch is perpendicular to the center member. The members are wound around the joint part 3 to 33 times with a wire of 0.195 mm to 3.3 mm in diameter, such as metal, resin, chemical fiber or carbon fiber reinforced resin. When the upper flying object is seen from the top to the bottom, the branches grow at right angles from the center vertical material. Cylindrical central vertical members with multi-layered cross-shaped equilateral shapes or polygons combined with diagonal lines inside the polygon are also used for rigid horizontal members and central vertical parts. The material is knotted by winding the members 3 to 33 times around the joint part with a wire of 0.195 mm to 3.3 mm in diameter such as metal, resin, chemical fiber or carbon fiber reinforced resin. The center of a three-dimensional girder structure that rigidly fixes a horizontal member and a vertical member for rigid connection by being hardened with epoxy resin from above the knotted wire part, or being rigidly bonded with aluminum welding or epoxy resin or aluminum screw. The vertical member is made of aluminum, carbon fiber reinforced resin, glass fiber reinforced resin, or a combination of these, and has a square cross section with a side of about 10 millimeters, a thickness of 1.5 millimeters, and a vertical length. The central part of the horizontal member for rigid connection is made in a cross-girder structure with four equilateral-angle pipes of about 195 mm to 3300 mm. To rigidly with pinching screws, welding or epoxy resin adhesive or fasteners, vertical central member and the horizontal member are assembled rigidly connected rigidly so as Crossed stereoscopic curb. FIG. 4 is a view showing an upper flying object in which square pipes are assembled in a cross-beam shape. In the figure, the method is a two-layer horizontal member, but usually three to nine layers.













Degree. FIG. 5 is a view of FIG. 4 as viewed from the top down. A horizontal member for attachment / detachment is inserted into the rigid horizontal member pipe and fixed with a fixture to constitute the upper aircraft. The horizontal member for rigid connection is electrically driven to facilitate assembly and disassembly of the upper aircraft. The socket structure is a socket structure that inserts a horizontal member that fixes the motor. The socket structure penetrates the inside of the socket and the end of the horizontal member is attached to the center of the center vertical member. There are three methods in which the end of the horizontal member for attachment and detachment is stopped at the center of the central vertical member like a cantilever beam. Like the truss structure of the truss structure, the truss is assembled in a diamond shape stiffened at the center so that the compression member does not buckle, and the horizontal member for rigid connection is rigidly connected. Get For this purpose, a plurality of propellers or fans of about 16 to 36 and a plurality of electric motors are stacked in multiple stages, and this arrangement method uses an aluminum screw or the like to mount the base of the electric motor on the base of the detachable horizontal member. The electric motor and the prober to be fixed are targeted at each position of the horizontal member, and a plurality of propellers or fans inside the upper aircraft can reverse the rotation direction of each propeller or fan at the target position. The horizontal member of the upper flying body is 15 mm to 30 mm wide and 15 mm high to prevent the entire individual aerial working flying object from rotating horizontally when the individual flying work object floats in the air. Mm to 30 mm, thickness 1.5 mm to 3.3 mm, length 195 mm to 33 Using non-equal sides or equilateral angles of aluminum of about 0 mm, carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin pipes, or a combination of these, the rigid horizontal member and vertical member are made of aluminum members. Welding joint, aluminum stiffening plate welding of horizontal member and vertical member, aluminum rib reinforcement welding, the necessary parts are rigidly bonded while strengthening, upper aircraft is epoxy resin, carbon fiber wire or netting material, carbon fiber A detachable propeller or fan guard member is fixed to the tip of a detachable horizontal member fixed with an electric motor, which is reinforced with tape, carbon fiber reinforced resin, glass fiber reinforced resin or Kevlar fiber reinforced resin, and fixed with a fixing tool. The material of the propeller or fan guard member is resin or carbon fiber This propeller or fan guard member uses plastic resin, glass fiber reinforced resin, chemical fiber, Tegs, stainless steel wire, wire or a combination of these, when a personal aerial work flying object comes into contact with other objects The propeller or fan guard member prevents damage to the propeller or fan, including a fan motor or blower method in which the duct fan and motor are integrated into a cylindrical duct. A horizontal member, a vertical member, a propeller, a fan, a fan motor in which a fan and a motor are integrated, or a blower guard member, which also serves as a reinforcement for the flying object, has a pipe seat in the pipe cavity. In order to prevent bending, encapsulate and cure foamed resins to reinforce the pipe There is a method to make the upper aircraft lightweight and robust, the pipe is made of the above composite material, the simplest method of assembling the pipe, the width 15 to 30 mm, the height 15 Elongated ladder shape using pipes of unequal sides or equilateral angles of aluminum, carbon fiber reinforced resin, glass fiber reinforced resin, or a combination of these, having a thickness of about 30 mm, a thickness of 1.5 mm, and a length of about 195 mm to 3300 mm In addition, the method using a honeycomb structure for the upper flying body, including a bird cage shape, a jungle gym frame shape, and a method of assembling a pipe with a fixture, is a resin or paper made of 1.95 mm in diameter to 33 mm in thickness. 195mm to 3.3mm cylinder Divided into the method by laminating a honeycomb structure such as honeycomb sandwich panels or Weir Ferran structure panel adhered to the printing plate on both sides of the honeycomb structure produced a honeycomb structure is cured adhesive with resin is set the type. FIG. 54 is a cross-sectional view showing a honeycomb structure, an OX structure, a flex structure, a bisecting structure, and a feather structure. The structure of the honeycomb in the present claim is made by using an adhesive or a brazing material by laminating a hexagonal honeycomb structure, an OX structure, a flex structure, a bisecting structure, a feather structure, or other various shapes. The material of the honeycomb structure in the section is paper, non-combustible paper, metal such as aluminum, titanium or stainless steel, aramid paper, carbon fiber reinforced resin, glass fiber reinforced resin, or a combination of these, honeycomb sandwich panel or via A honeycomb structure panel such as a ferrule structure panel is laminated with a honeycomb structure panel such as a horizontal honeycomb sandwich panel or a weir ferran structure panel obtained by hollowing out propeller or fan holes. FIG. 34 is a diagram in which honeycomb sandwich structure plates are stacked as an upper flying object. FIG. 35 is a diagram of FIG. 34 viewed from the top down. The large round part has a hole in the honeycomb sandwich structure plate, and a propeller or fan and an electric motor are installed inside. There is a method in which the electric motor is a blade-laminated electric motor. The small circle is a vertical member for stacking honeycomb sandwich structure plates. The vertical members of pipes made of aluminum, carbon fiber reinforced resin, or glass fiber reinforced resin are multi-stage like the honeycomb internal structure where honeycomb structures such as honeycomb sandwich panel or weir ferran structure panel are vertically layered in multiple layers. By stacking and connecting honeycomb structures such as a honeycomb sandwich panel or a weir ferran structure panel, the upper flying object is configured in the shape of an upper flying object combined with a rectangular parallelepiped, a cylindrical shape, a disk shape, a donut shape, or the like. FIG. 22 is a diagram in which the upper flying object of the personal aerial work flying object is a horizontal disk, and a plurality of propellers or fans are installed inside the disk. The upper flying object is used in a direction that can withstand the load when rising and falling in the vertical direction where hexagonal aggregates of honeycomb structure such as honeycomb sandwich panel or weir ferran structure panel can be seen when viewed from the top on a horizontal member In order to take in air from the periphery of a honeycomb structure such as a sandwich panel or a weir ferran structure panel, a method of laminating at intervals of 195 mm to 330 mm or a honeycomb structure such as a honeycomb sandwich panel or a weir ferran structure panel is closely attached Honeycomb structures such as honeycomb sandwich panels or weir-ferran structure panels, including a method of laminating and stacking holes such as fan motors with duct fans and motors integrated or ducts of blowers For the purpose of strengthening, pipes made of aluminum, carbon fiber reinforced resin, or glass fiber reinforced resin may be used for horizontal members and vertical members. One side made of honeycomb structural material is 19.5 mm to 330 mm thick. Holes above and below the hexagonal column cavity of the honeycomb sandwich panel with a hexagonal structure material of 19.5mm to 330mm, and it looks like a fan motor or a blower unit with a duct fan and motor integrated. Including a method of laminating honeycomb sandwich panels in which an electric motor and propeller or fan or fan motor or fan in which the fan and motor are integrated are laminated inside the space. The method of assembling the formed bowl-shaped objects is The belt shape is made of a combination of aluminum, carbon fiber reinforced resins, glass fiber reinforced resins, and resins that are assembled using a plurality of bamboo baskets formed by weaving a bamboo braid. The belt member for knitting the heel is 0.33 to 1.95 mm in thickness, which is used as a material for knitting the cocoon with a composite belt member having both flexibility and toughness, such as a bamboo material knitting bamboo cocoon using Metals such as aluminum or titanium with a width of 3.3 mm to 19.5 mm, carbon fiber reinforced resins, glass fiber reinforced resins, or a resin film made of a laminated belt, and carbon fiber wires made of knitted wool. The core material is a braided epoxy resin belt and is 0.33 to 1.95 millimeters thick and 3.3 to 19.5 millimeters wide. There is also a method of using a belt-like composite object in the shape of a bamboo that weaves bamboo baskets that are sandwiched by a lumi band and bonded with epoxy resin and used as a material for knitting bamboo baskets. Combining these composite members into various shapes of heels Combining these heels to form a three-dimensional shape, knitting the heels Adhering between the members at the intersection of the belts and belts with epoxy resin, making the entire heel strong and supple籠 Flexible and tough, with the ability to restore the structure even if it is slightly deformed. This 籠 is a combination of aluminum, carbon fiber reinforced resins, glass fiber reinforced resins and resins with a diameter of 1 to 5 mm. It can be processed into various shapes like bamboo baskets reinforced with rods or pipes. Figure 32 shows the shape of a crest of a Shimadzu crest in the shape of a circle with a hemispherical bamboo basket knitted into a bowl shape with a belt-shaped member like a colander in the kitchen. It is a figure with an electric motor and a prepeller or a fan installed in the center of the cross beam of a hemispherical shape sandwiched up and down and shaped like a crest of Shimadzu crest in a circle shape. FIG. 6 is a view showing that the collar member and the mark-shaped member of the center Maruta are fixed by a fixture and can be easily assembled and disassembled. FIG. 33 shows a blade-stacked electric motor or a blade outer peripheral permanent magnet fixed outer circle with a hemispherical bamboo rod like a hemispherical bamboo basket knitted with a belt-shaped member like a colander in the kitchen. It is the figure which showed that the assembly and decomposition | disassembly of the spherical bowl shape fixed with the fixing tool on both sides of the circumference ring electric coil fixed electric motor could be performed easily. A hemisphere-shaped method that combines the hemispherical colander shape and the colander shape together, the earth's equivalent to the equator on the earth can be assembled and disassembled with a fixture, that is, the bamboo sphere's hemispherical shape In addition, a semi-circular braid knitted into a hemispherical collar shape with a belt-shaped member, and a circle-shaped object like a crest of Shimadzu clan in the middle with a hemispherical shape sandwiched vertically up and down An electric motor and a prepeller or fan are installed in the center of the cross beam of the object shaped like the family crest of the Shimazu clan in the shape of the figure. The upper and lower hemispherical cicada members and the crest of the Shimadzu clan in the center circle Such a member is fixed with a fixture and can be easily assembled and disassembled like a spherical bamboo fence with an electric motor and propeller or fan installed in the center. Like a wheel motor with a rotor disk There is a method in which the wheel is a propeller or a fan motor or blower in which the fan and fan and motor are integrated. The fan motor or blower method in which the fan and motor are integrated is 33 mm away from the center of the disk. A fan motor or blower in which a fan and a motor are integrated by forming four, eight, twelve, sixteen, or thirty-two blades by cutting radially from a place and bending it into a blade shape. A ring-shaped member is welded to the outer periphery of a fan motor or blower that is formed into a shape or an integrated fan and motor, and a plurality of neodymium magnets and other permanent magnets are fixed along the outer periphery of the ring. Disc shape with multiple coils on the outer circumference of the ring There is a method of using the electric motor. FIG. 20 is a diagram in which the upper flying object of the personal aerial work flying object is like a bunch of kites. For the upper flying object, the method of gathering the shape of the kite using a plurality of kite spheres and gathering like a tuft of bunch is also included in the configuration of the upper flying object. This includes a method of laminating honeycomb structures such as panels or weir ferran structure panels horizontally in multiple layers, which is exactly like the internal structure of a natural round honeycomb.













The flying kite is the structure of the entire flying vehicle, which can protect people inside the kite and can enter the inside of the spherical kite. The kite was raised by an electric motor. It can also be used as a propeller or fan guard and the structure of both the upper flying body and the lower suspension body by allowing the wind to pass downward. This kite can also be used as a boarding deck that can feel the skeleton of the airship and the wind. The spherical spear has a structure that allows easy assembly and disassembly of the spear and spear by attaching and detaching the fixture. The method is to combine two hemispherical spears into a sphere, with a propeller or fan inside and an electric motor. The electric motor, propeller or fan is a method of constructing a flying object by assembling a spider-like sphere with a propeller or fan and electric motor together with a fixture like a kite A method of attaching a propeller or fan to the shaft of a normal electric motor having a rotor with a size of a fist and fixing it to the center of a cross beam, and a horizontal plane passing through the center of the sphere is a disc type motor and propeller or There is a fan or a fan motor in which the fan and the motor are integrated, or a method of installing a blower at the center of the cross beam. As an electric motor, the rotor of a disk type motor has a three-blade prober shape, and this disk-like propeller or fan A disk-shaped propeller or fan in which a permanent magnet such as a neodymium magnet is fixed to the periphery of the outer circle and a ring-shaped member is wrapped around the outer surface of the disk-shaped rotor so that a plurality of coils are arranged inside the ring. A disk-type electric motor that includes a method that combines a motor with a motor is also a method that combines pipes. A lower suspension body having a lower suspension body provided at a lower central position of an upper floating body of a personal aerial work flying object, which can be used in a method of stacking honeycomb structures such as sandwich panels or via-ferran structure panels, is 195 mm to 3300 in length. Millimeter natural fiber or chemical fiber lobe, steel wire, metal such as iron, steel, aluminum or titanium, resin, carbon fiber reinforced resin, glass fiber reinforced resin or Kevlar fiber reinforced resin or a combination of these materials The lower suspension body, which is made up of rope members, wires, wires, rods, and pipe materials, is freely movable such as a chain link or universal joint at the center of the lower end of the upper aircraft. It is connected with a connecting device that can move the center of gravity of the lower suspension body The lower suspended body rope or wire or bar or pipe material that is flexibly connected so that it can be freely carried on a person who works in the air sits on the swing platform provided on the lower suspended body such as the rope or the lower part There is a method of standing on a step fixed to the suspension body. From now on, it is a description of the safety measures of workers so that humans who work in the air do not damage their bodies even if they fall from about 33 meters above the ground There are many air bags such as lightweight helmets with air caps solidified with styrofoam and small air bags like small air bags covered with rubber or silicon rubber inside the cloth or non-woven fabric of natural fiber chemical fiber of the size of a small bag Shaped like a waterproof cotton garment with a clogged thickness of 19.5 to 33 mm Human body protection bags such as humanoid sleeping bags or human body protective clothing that can be entered and exited by humans can be attached to and detached from the lower suspension body with a waterproof and airtight zipper and a Velcro tape (registered trademark) that is a lightweight waterproof processed cotton case of a collection of fibers There is a method of connecting to the lower suspension body with a simple fixture or belt. Figure 103 shows that the waterproof and airtight zipper is waterproof and airtight, and the thickness is about 0.195mm to 3.3mm thicker than the two underlying fabrics, and the width is viewed vertically from the zipper for the purpose of preventing the fabric from getting into the zipper When the width of the zipper is about the width of the left and right seams and the length of the resin zipper is about the length of the zipper, two on the back and the front, a total of four zipper seams with a width slightly exceeding the width of each zipper When the fins along the zipper are sewn into the zipper seam one by one and the zipper is pulled up, the fabric prevents the fabric from biting into the zipper, and the fin and fin that cover the zipper overlap from the zipper seam on both sides of the zipper Airtight waterproofing of the back and front of the zipper by overlapping the part exactly with silicon resin or rubber resin Even if you pull up the zipper quickly There is a cross-sectional diagram of a zipper that waterproof and airtight internal simultaneously zipper can be pulled pulling the lightly zipper without Kamikomu the zipper, or not catch waterproof and airtight. Here is a description of a zipper that is not waterproof and airtight. The waterproof and airtight zipper is 0.195mm to 3.3mm thicker than the two underlying fabrics for the purpose of waterproofing and airtightness and preventing the fabric from getting into the zipper. When the zipper is viewed vertically, the width is about the width of the seam on the left and right sides of the zipper, and the length of the zipper is about the length of the zipper. When the fins along the resin zipper are stitched one by one in the zipper seam and pulled up, the fabric prevents the zipper from biting into the zipper and the zipper seams on both sides of the zipper The area where the fins that cover the zipper overlap with the fins is covered with silicone resin or rubber resin so that the back and front of the zipper are airtight and waterproof. Even if the zipper is pulled up rapidly, the fabric does not bite into the zipper, it can be pulled up and down easily, and at the same time the inside of the zipper is airtight and waterproof, the above is the description of the zipper that is not waterproof and airtight Shock absorbers and seats for human side protection are processed into a three-dimensional mesh like chemical scraps of plant silkworms using chemical fiber material, carbon fiber wire, or carbon fiber reinforced resin fiber material. There is a method that allows you to work in the air while standing on a step provided on the lower suspension body. Absorbing material is an acceleration that senses natural fall on parts that may collide with the ground when falling, such as a human head, shoulders, spine or hips There is a method in which the intelligent device detects the natural fall of the human body and wraps the human body before it collides with the ground, and the air bag instantly inflates with compressed air to protect the human body. The method of working is equipped with a parachute at the top of the gyro of the upper flying object, and it is structured to open the parachute automatically when a free fall is detected by the human will or with the acceleration sensor, so that the worker lost consciousness The emergency method is a mechanism that safely descends with a personal aerial work flying object and a human, the above is a description of the worker's safety measures, the gyro is installed above the upper aircraft and the upper aircraft The airborne flying object that works to stabilize the air in the air suspends humans or robots or video cameras and radio control devices. It is possible to observe disaster-stricken areas and save lives by automatic flight, and a shock absorber like a balance ball with rubber or silicon rubber sealed inside at the lower end of a human or video camera and radio control device. The following power storage device (condenser) or secondary battery (battery) is used on the lower surface of the shock absorber, which is installed in the event of accidents or accidents. From here, the power storage device (condenser) or secondary battery ( Battery), specificities of capacitors and graphene using nanocapacitors between clusters in amorphous and crystalline alloys such as Ni-based and Si-based, and single-crystal nanocubes of capacitors and dielectric ceramics by nano-stacking Single-crystal nanocubes using technology to place, arrange, bond, and interface control single-crystal nanocubes bottomed up from two to three dimensions Capacitors using high-performance ceramic small-sized materials, or capacitors using nanotechnology to precisely control the structure of ceramics, metals, carbon, etc. at the atomic level, and using specially-structured nanocrystals for power storage devices, and fuel cells and water electrolysis cells using nano-lamination methods Or small and light fuel cells such as AGM type deep cycle batteries, large-capacity ceramic capacitors, solid hydrogen source fuel cells, complex hydride-based fast ion conductors, or oxide-based bulk all-solid lithium batteries Secondary battery, high capacity laminated lithium battery, lithium ion air battery, lithium ion battery, nickel / hydrogen rechargeable battery, magnesium storage battery, non-lithium battery using medium / low temperature ionic liquid or high oxygen ion conductor Metallic and air batteries using cell membranes, precious metal-free fuel cells using anion exchange membranes, or synthesized tubular carbon nanofibers (CNF) with a unique structure that periodically holds a large number of nanogates that can only enter and exit ions The above is a description of a capacitor (capacitor) or a secondary battery (battery), such as a battery selectively prepared as a negative electrode material for a metal secondary battery in which only a specific metal such as lithium and sodium is filled. A small, large-capacity battery or battery is placed under the shock absorber, and the center of gravity of the personal aerial work flying object is lowered. From the east, west, south, and north directions of the outer peripheral lower end of the bottom horizontal member of the upper levitated body, A rope or wire is hung at the lower end, and this wire or rope or wire in the front / rear / right / left direction is equipped with a human or radio control device and a small computer with a built-in automatic posture control program. By manually or mechanically pulling the aircraft, the center of gravity of the flying object for personal aerial work is moved back and forth, left and right, and flight control of horizontal movement is performed. The transmitter (propophone) is a radio-controlled piloting device that controls the hovering and vertical movement of the flight by adjusting and synchronizing, enabling the forward, backward, ascending, descending, and left-right movements of the individual work squadron. ) ・ Receiver ・ Servo ・ Amplifier for motor ・ Speed controller ・ Distribution There is a method of automatically controlling while working with a device that combines wires, wiring tools, switchboards, switches, and computers. The control of personal aerial work flying objects is manual and radio controlled by a control switch provided at the hand of the passenger It is divided into three methods: wireless control by transmitter (propo) and automatic control by personal computer. A rope or wire is hung from the bottom of the battery to the ground and the bottom is fixed to the ground. It is possible to guide the movement of flying objects for personal aerial work from the ground by moving with the lower end of the rope or wire.For work only, place a battery or power supply on the ground and use electricity to the required height An electric motor is used for the upper flying body of a personal aerial work flying object that has a method of transmitting power There is a method of using a lightweight internal combustion engine made of a lightweight metal such as titanium or aluminum instead of the electric motor of the above-mentioned flying object, from here, forced air-cooled whole heat radiation fiber reinforcement It is a description of a resin metal composite internal combustion engine. FIG. 8 is a cross-sectional view of a forced air-cooled overall heat-dissipating metal fiber reinforced resin composite internal combustion engine, in which the cylinder and cylinder head are color-coded in black and white so that the configuration can be clearly understood by the left and right cylinders. Forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine is a high heat wear resistant part that covers the internal combustion part, that is, the part that directly receives heat and explosion such as cylinder head, cylinder, piston, piston ring, connecting rod, crankshaft is wear resistant and heat resistant A lightweight metal layer such as titanium or aluminum and a thermal buffer layer of steel wool rock wool glass wool and a stress transmission rod that transmits explosive force to the fiber reinforced resin layer are placed around the metal layer of the metal layer to create a thermal buffer layer from the metal layer Casing through the internal combustion engine such as an oil pan by penetrating through the fiber reinforced resin layer and directing cold air directly to the metal part by forced air cooling to dissipate heat from the numerous small holes opened in the entire casing. Is composed of metal or fiber reinforced resin honeycomb structure, outside of titanium or aluminum layer 3 to 33 millimeters thick 1.95 mm such things from a height 19.5 mm radiating fin air-cooled motorcycle engine outside













. Steel that is compressed from the inside provided as a heat buffer layer on the outside of the metal radiating fins, which is processed in large numbers so as to wrap the surface of the metal layer at intervals of about 1.95 mm to 3.3 mm in about 3 mm The inner surface of the fiber reinforced resin, which is surrounded by a heat buffer layer in which a wool layer, a rock wool layer, and a glass wool layer are laminated to form an air-containing layer and is in contact with the heat buffer layer from the outside, has a height of 19 .5mm to 33mm Thickness 1.95mm to 3.3mm, with 1.95mm to 3.3mm spacing and processed into pleats like air cooling bike engine radiating fins It is wrapped with a layer of fiber reinforced resin such as heat resistant carbon fiber reinforced resin, and the outside of the heat resistant fiber reinforced resin is metal or fiber reinforced Cylinder head that receives the explosive force of the internal combustion chamber, which is in charge of the mechanical structure related to the strength of the internal combustion engine, is wrapped in a honeycomb structure made of fat, etc., and is about one commercially available disposable chopstick A steel wool layer and a rock wool layer with a large number of metal rods having a diameter of 6 mm to 9 mm and a distance of about 33 mm to 195 mm from the support portion of the metal layer to the support portion of the heat-resistant fiber reinforced resin layer. A rod that penetrates the glass wool layer and spreads radially like a sea urchin thorn to transmit the explosive force from the metal layer to the heat-resistant fiber reinforced resin layer and to the honeycomb structure layer made of metal or fiber reinforced resin. Both ends of the material are supported by a support provided in the metal layer and heat-resistant fiber reinforced resin layer. There is a method in which the stress transmission rod is screwed into the hole of the bearing as a bolt. The steel wool layer, rock wool layer and glass wool layer are supported by the tips of the inner and outer radiating fin groups from the compressed inside, and the overall heat dissipation In the two-dimensional or three-dimensional honeycomb structure such as metal or fiber reinforced resin to wrap the outside of the heat resistant fiber reinforced resin responsible for the mechanical burden, the mechanical part is borne by the thickness according to the stress. This heat-resistant fiber reinforced resin and a metal having an infinite number of small holes with a diameter of about 0.195 mm to 3.3 mm that are open at intervals of about 1.95 mm to 33 mm to achieve overall heat dissipation throughout the honeycomb structure, It is an internal combustion engine with a composite structure of fiber reinforced resin and honeycomb, and the overall heat dissipation is like a wing of a dragonfly. A thin trachea having a diameter of 0.195 mm to 3.3 mm passes radially from the inside of the internal combustion engine to the outside at intervals of about 1.95 mm to 33 mm for heat dissipation, and the internal combustion engine rotates. Using the force or the power of the turbocharger that uses the exhaust of the engine, the blades of the opening opened in the front part of the internal combustion engine are rotated to blow and use a dedicated air-cooled tube with a diameter of 19.5 to 33 mm dedicated to blowing There is a dedicated forced air cooling pipe that is distributed and branched so that air is directly blown to the metal fins of the cylinder, and air is directly blown to the heat radiating fins of metal such as titanium or aluminum surrounding the internal combustion section to perform forced air cooling. Dissipate heat and dissipate the heat in the order of steel wool rock wool glass wool The entire air radiated through the thermal buffer layer and further radiated air has a radial diameter of 0.195 mm to 3.95 mm like a feather of a dragonfly piercing through a honeycomb structure of heat resistant fiber reinforced resin and metal or fiber reinforced resin. An internal combustion engine through a thin tube of 3 mm and through a small tube or small hole with an infinite number of diameters of about 0.195 mm to 3.3 mm inside the honeycomb structure layer through a heat resistant fiber reinforced resin layer and a honeycomb structure layer. The overall heat dissipation is to disperse the heat so that the resin does not melt with heat. The method using the internal combustion engine is a battery and gasoline in which the lower suspension body installs the battery and fuel tank under the shock absorber. There is a way to install a tank, forced air cooling whole heat radiation fiber reinforced resin metal composite internal combustion engine is a gasoline engine However, it can also be used as a diesel engine, and heavy objects such as electric control devices, batteries, and gasoline tanks that can be placed on the ground are placed on the ground, and power is transmitted from the ground and fuel is pumped through an oil supply pipe to an air vehicle. Forced air-cooled whole heat-dissipating fiber-reinforced resin-metal composite internal combustion engine with adjustable piston momentum torque converter clutch generator motor with piston engine type or rotary engine type internal combustion engine combined with generator and motor. The hybrid power generation / transmission integrated hybrid system starts the internal combustion engine with an electric motor, and if the output of the internal combustion engine increases, the forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine generator. The inner disk is made of fiber reinforced resin and the outer periphery of the disk is metal. A metal reinforced plastic-metal compound wheel is a metal wheel that can be increased and decreased while automatically rotating by computer control. A metal wheel that can be removed and attached to the metal. The metal part on the outer periphery of this wheel is round like a shield method segment. Accordingly, the segments that are equally divided into about 360 degrees into 16 divisions increase the amount of metal on the outer periphery that has a structure in which layers are formed radially and concentrically like the sector and track relationship of the floppy disk cluster area. The method is that the metal segment is hooked on the outer periphery of the rotating metal, and the nail has a circular arc like a claw, so that the nail can be inserted and removed by rotating the nail. The segments are separated from the flywheel by centrifugal force, and the segments separated by the rotating claws provided on the wall of the circumferential wheel are fixed. In order to make it smooth, an equally divided metal segment covering 360 degrees on the outer circumference is attached and detached at once. This mechanism can be used for adjusting the rotational force of a rotating machine. There is a method of adjusting the angular momentum and securing the angular momentum stably, then sending a part of the output of the internal combustion engine to a motor / generator and transmitting the power to a plurality of external electric motors. In order to obtain, fine adjustment of the output such as thrust by generating electric power after it is obtained from the internal combustion engine combines the output of the internal combustion engine as needed to control the energy of the electric motor that obtains thrust and distribute the total with a computer Shared internal combustion engine generator Motor angular momentum adjustable spring wheel torque converter clutch computer integrated hybrid device, the above is forced air cooling The rotary engine method, which is a description of the body heat radiating fiber reinforced resin metal composite internal combustion engine, is by laminating and combining the rotary engine and forced air cooling whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor. Forced air cooling overall heat radiating fiber reinforced resin metal composite internal combustion engine Angular momentum adjustable spring wheel torque converter clutch Forced air cooling overall heat radiating fiber reinforced resin metal composite generator motor output power transmission integrated hybrid device, from here forced air cooling whole heat radiating fiber This is a description of a reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor. FIG. 9 is a diagram of a forced air-cooled overall heat radiating permanent magnet rotor electric coil stator disk stack type fiber reinforced resin metal composite electric motor. FIG. 10 is opened for forced air cooling that becomes a kind of air blower by rotating a hole that is inclined at an angle of about 19.5 to 33 degrees with respect to the rotation surface with respect to the rotation direction of the disk. It is a figure of the disk-shaped rotor fixed to the axis | shaft arrange | positioned radially along the concentric circle | round | yen with the permanent magnet opened by inclination so that the air which sent may be sent back. FIG. 11 shows that the rotor is rotated through a hole that is inclined at an angle of 19.5 to 33 degrees with respect to the disk surface, so that forced air-cooled air that is a kind of blower is sent backward. The electric coils that allow air to pass through the holes are fixed in a radial manner along the concentric circles of the stator disk, and fixed to a casing with a hole through the shaft of the electric motor in the center of the stator. It is a figure of a disk-shaped stator. The disk-type electric motor has a circular rotor with a diameter of 1.95 to 33 mm and a metal or fiber-reinforced resin disk with a rotor diameter of 19.5 to 330 mm and a thickness of 1.95 to 33 mm. Permanent magnets with 3 or 6 or 12 or 16 or 32 holes on the inside, and holes that are regularly and radially radiated from the shaft to the concentric circumference from the shaft to the shaft of the electric motor. The disk that fixes as many permanent magnets as possible is fixed by embedding permanent magnets such as neodymium magnets in the holes and fixing the permanent magnets so that the magnetic flux is perpendicular to the disk surface. The electric coil disk fixed to the rotating shaft of the electric motor is such that the magnetic flux of the electric coil is orthogonal to the disk. It is the same size as the disk of the magnet, but the shaft part of the electric motor is a hole, and the permanent magnet and the electric coil are passed through the shaft of the electric motor with a gap of 0.195 mm to 0.33 mm. A multilayer ceramic type coil is formed in which an electric coil thicker than the permanent magnet is fixed at a position corresponding to the permanent magnet at the position where the electrodes face each other, and the copper enameled wire of the electric coil or the nitrogen circulating glass amorphous or ceramic coating in the room temperature superconducting pipe is distributed Rather than winding a coil, the coil and insulator are three-dimensionally laminated to form a coil, and a room-temperature superconducting ceramic type ceramic coil and insulation-coated ceramic are simultaneously formed using a three-dimensional solid atomic layering technique. There is a method or melting by making a female mold of the coil with glass or ceramic with high melting point A disc-stacked type that has a method of manufacturing a heat-resistant coil made of glass or ceramic with an insulating gas press-fitted with an inert gas gas while keeping a low-conductivity, highly conductive metal in a female mold of glass or ceramic coil The electric motor has a plurality of electric coils arranged radially on the circumference of the circumference. A disk with a hole in the central shaft is fixed to the casing of the electric motor. The disk that fixes the electric coil is a metal or fiber reinforced resin. This permanent magnet disk and electric coil disk are alternately laminated, the disk with the permanent magnet fixed is sandwiched between the electric coils from both sides, and the electric coils are in phase with the rotating direction. This principle is a brushless motor that rotates a permanent magnet. This principle is based on fixing a disk with a permanent magnet to the casing of the electric motor, and powering the disk with an electric coil. The method of the brush motor fixed to the shaft of the motor may be the forced air cooling whole heat dissipation rotor permanent magnet stator electric coil disk laminated electric motor, the electromagnetic part is metal and carbon fiber and the other part is fiber reinforced resin Forced air cooling is performed with blades fixed to the shaft of the electric motor. The hot air radiates heat from the entire electric motor through an infinite number of small holes with a diameter of 0.195 to 3.3 mm that are drilled in the entire casing, and has a larger number of permanent magnets and electric coils than the conventional electric motor. And the heat dissipation problem has been solved, and it was tilted at an angle of 19.5 to 33 degrees with respect to the rotating surface with respect to the rotation direction of the disk. Depending on the method of solving the problem of heat dissipation by becoming a kind of air blower by rotating the hole, there is a method of cooling the inside with the above method by making the electric conductor a pipe shape. An electric coil disk may be provided with an alternating current in a phase in which the direction of the magnetic flux of the coil is reversed and the disk with the axis fixed is rotated for each disk. The above is a description of forced air cooling overall heat dissipation fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor, from here it is a description of bird strike prevention device fiber reinforced resin metal composite turbine stacking type electric motor is there. FIG. 12 is a cross-sectional view of a bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor. FIG. 13 shows a blade type in which a blade is fixed to a shaft of an electric motor in which a permanent magnet is embedded in and fixed to a blade along a concentric circle with respect to a shaft of a bird strike prevention device fiber reinforced resin / metal composite turbine laminated type electric motor. FIG. FIG. 14 shows a bird strike prevention device with a fiber reinforced resin-metal composite turbine laminated electric motor and a blur along a concentric circle with respect to the axis of the electric motor.
Electricity












It is a figure of the braid | blade type stator with which the braid | blade which had the hole which lets the axis | shaft of an electric motor pass in the center of the braid | blade fixed by embedding a coil was fixed to the casing of the electric motor. Turbine stack type electric motor is a jet in which a disk of the above-mentioned disk stack type electric motor is processed into a complete blade shape, and a permanent magnet layer and an electric coil layer are alternately stacked on a blade, and a permanent magnet layer and an electric coil layer are stacked on the blade. Things like the intake turbine of an engine can be used as a substitute for a jet engine. From here, it is a description of a bird strike avoidance device, the blade for blade strike is the tip that cuts the wind of the blade in order from the entire intake blade When a bird strike occurs using steel, stainless steel, or aluminum alloy steel, and when a bird strike occurs, the bird is cut into multiple minced steel blades, and then the birds are shredded or crushed into minced meat pieces. The blade is provided with a groove on the blade that tends to scatter toward the side of the engine or motor due to centrifugal force. A small window-shaped discharge port that can be opened and closed on the side of the casing by guiding the pieces of meat to a position where the pieces of the electric motor or jet engine are easily scattered by a sensor that detects the bird strike by guiding the pieces to the desired position. The normal jet engine method is designed to minimize the damage of the engine due to bird strike by preventing the flesh of the bird from reaching the burning part of the jet engine. The above is the description of the bird strike avoidance device. The position where the direction of the magnetic flux is parallel to the blade rotation axis on the blades of the blades of the turbine having a pitch angle and obliquely arranged using this device. Of a jet engine in which permanent magnets such as neodymium magnets and electric coil layers are alternately laminated The electric motor in the shape of a gas turbine is easy to replace each turbine, eliminating the need for complicated mechanisms, and can freely control the output and eliminate noise problems. Production of a flying body using a jet turbine-shaped electric motor for noise reduction by generating electricity with a lightweight internal combustion engine of gasoline, light oil or heavy oil that has become a jet turbine-shaped electric motor without noise and can also be used on passenger aircraft It is possible to generate electricity with a gasoline engine, heavy oil or light oil diesel engine instead of aviation fuel, and it is possible to purify the exhaust through a soundproof muffler and exhaust gas purification catalyst ceramic, and at the same time the aircraft is a silicon solar cell on the sea of clouds Or the polymer organic thin film solar cell In addition, it is convenient to obtain electric power by attaching it to a part, which is convenient for preventing air pollution or economically and for the safety of fuel explosions. Heat fiber reinforced resin metal composite internal electric motor can be driven, or at the same time forced air cooling whole heat radiated fiber reinforced resin metal composite internal combustion engine angular momentum at the rear of jet turbine-shaped heat fiber reinforced resin metal composite electric motor as hybrid type Adjustable spring wheel torque converter clutch forced air cooling whole heat radiating fiber reinforced resin metal composite generator motor output power generation integrated power transmission and transmission integrated hybrid device to integrate the output, power generation and power transmission by internal combustion engine to manage the computer and share energy It becomes possible to control the power while obtaining thrust and power in the internal combustion engine. The above is a description of a bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor that can transmit power to the electric motor, can assist the battery power, and can charge the battery with surplus power From here, it is a description of a method using a turbine stack type electric motor for a personal aerial work flying object, a permanent magnet and an electric coil are arranged concentrically around the circumference of the blade, and the magnet The simplest method of the upper aircraft using a blade electric motor with alternating layers of electrical coils and an electric coil as a personal aerial work flying object is to use a blade with a permanent magnet fixed above and below a disk with an electric coil fixed to the upper blade. In this method, the lower blade is sandwiched so as to rotate in the reverse direction. FIG. 6 shows the simplest method in which a turbine blade laminated rotor permanent magnet stator electric coil electric motor is applied to an individual aerial work flying object. In the figure, the upper turbine blade blade has a permanent magnet at the center and an electric coil at the bottom. FIG. 5 is a diagram showing that the permanent magnets are radially installed in the blade blades along the concentric circles and the blades of the upper and lower turbines are reversely rotated to prevent the whole from rotating. FIG. 7 is a view of FIG. 6 looking down from the top. The disk to which the electric coil is fixed is a fiber reinforced resin having a thickness of 19.5 mm to 33 mm and a diameter of about 3300 mm, or a disk made of a combination of metal or metal and fiber reinforced resin, and concentrically along the circumference inside the circumference. Radial electric coils are arranged radially from double to triple concentric circles so that the direction of magnetic flux from N to S is on the surface of the disk, that is, the magnetic flux is perpendicular to the surface of the disk, that is, parallel to the rotation axis. The disk has a honeycomb structure through which wind passes (honeycomb through which unblocked wind passes) or a fiber-reinforced resin with a number of holes in consideration of mechanical distribution or a mesh shape that supports an electric coil, and the wind passes The road is for the passage of wind arranged diagonally according to the pitch angle of the blade. There is an axis at the center of the disk, and the axis flies from the center of the two faces of the stator disk. Two blade wind turbines with a hole through which the shaft passes in the center so as to sandwich the disk of the stator's electric coil is sandwiched from above and below on this shaft, and the blade of this blade wind turbine has permanent magnets such as neodymium magnets. An AC current is sent to the electrical coil that is positioned with the magnet facing the electrical coil with a gap of 0.19 mm to 0.33 mm in a phase in which the rotation directions of the upper and lower blades are opposite to each other. The blade windmill has a frame-shaped or net-shaped blade guard that prevents the entire aircraft from rotating due to the rotation direction being reversed and blowing the wind downward. An internal combustion engine generator motor that has a lower suspension attached to the lower part of the shaft of the stator electrical coil disk that protects the damage and constitutes a personal aerial work flying object. Brides device and personal aerial flying object in the lower portion of the upper flying object which can be combined with forced air across the heat dissipating fiber reinforced resin metal composite internal combustion engine equipped with a lower suspension member. FIG. 37 shows a hot air balloon, a gas balloon, a hot gas combined balloon, a hot gas balloon, and an external suspension cable that can be automatically carried out and stored by an envelope winder. FIG. FIG. 38 shows a hot air balloon, a gas balloon, a hot gas combined balloon, a hot gas balloon, and an external suspension cable that can be automatically taken out and stored by an envelope winder. It is the whole block diagram seen from the left side. FIG. 39 shows an overall configuration of the hot air balloon, gas balloon, hot gas combined use balloon, hot gas balloon, and external suspension cable that can automatically carry out and store the envelope (ball skin) as seen from the front of the back fan blow type personal aerial work flying object. In the figure, the envelope is stored in the envelope winder. 40 is a partial configuration diagram seen from the back side of a flying object of a personal air work air fan, a hot air balloon, a hot gas balloon, a hot gas balloon, and an external suspension cable that can automatically carry out and store the envelope (ball skin). is there. FIG. 41 shows a partial configuration of the hot air balloon, gas balloon, hot gas combined use balloon, hot gas balloon, external suspension cable back fan blower type personal aerial work flying object that can automatically carry out and store the envelope FIG. FIG. 42 shows a partial configuration of a hot air balloon, a gas balloon, a hot gas balloon, a hot gas balloon, and an external suspension cable that can automatically carry out and store the envelope (ball skin) as seen from the left side of the back fan blow type personal aerial work flying object. FIG. The method of using the balloon to obtain the ascending force of the upper flying object of the personal aerial work flying object is divided into the hot air balloon, gas balloon, hot air balloon and gas balloon combined heat and gas combined balloon method. An individual aerial work flight consists of an upper flying body and a lower suspension body. An upper flying body using a hot air balloon is made up of an envelope (ball skin) that contains hot air, a load tape, and a wire. The ball is made of nylon or polyester chemical fiber that is hermetically coated with polyurethane, and is a ball that is reinforced with road tape by vertically stitching Gore, which is the smallest unit of the envelope and stitched horizontally by vertically stitching the panels. Or the bag shape or cylindrical shape or the shape of tear drops upside down, the load receiving part is several nylon or The load tape that supports the load is sewed to the crown ring at the top of the emperope, and the lower end is connected to the following backpack with a suspension cable. The suspension cable is made of steel, stainless steel, carbon fiber reinforced resin wire, twisted wire, Kevlar fiber reinforced resin wire or twisted wire, and the load tape is used to prevent the envelope from tearing. A glass of a kerosene lamp below, which is used in the horizontal direction, and has an auxiliary cloth called a scoop with a triangular shape or a skirt shape to introduce hot air around the burner at the opening of the envelope. The squirt shape of There is a method to facilitate recovery of hot air cover the upper hemisphere of the sphere Hoya auxiliary fabric made with a net there is instead made this method of skirt or scoop, called skirt. FIG. 43 is a sectional view of the envelope winder, torch and burner. FIG. 44 is a diagram in which the left side figure shows the tip cylindrical root spherical kerosene lamp squirt type envelope combustion prevention net lowered when the envelope is stored, and the right side figure shows the tip cylindrical root spherical kerosene lamp squirt type envelope combustion prevention net when the burner burns. It is the figure which went up to the place. FIG. 45 is a partially enlarged view of the backpack and the backpack peripheral device as seen from the left side of the passenger. FIG. 46 is a partially enlarged view of the state in which the envelope winder winds the envelope halfway viewed from the left side of the passenger. The hot air balloon is also used as a gas balloon. The envelope is airtightly tied to the following torch with a belt, and the floating gas is ejected from the torch. This envelope is mainly sewn with a thread such as polyester and is heat resistant. The place where the nature is required is sewn with thread such as Nomex, and the solenoid valve made of carbon fiber reinforced resin that exhales hot air is opened and closed at the top or middle of the envelope, manually, wirelessly The opening and closing is controlled by automatic control. The envelope shape is a cylindrical shape with a diameter of about 195 to 9900 mm and a length of 1950 to 99000 mm. The lower suspension body has a size like a school bag used by elementary school students. This backpack and bag are about the size of a backpack that you carry when you climb Everest. The peripheral device of the pack consists of a peripheral device, and the belts that carry the backpack can be joined together using a buckle etc. at the position in front of the chest. A belt is hung on the seat part from the part of the backpack that is fixed to the lower suspension body and hits the back of the human back, and the human body can pass both legs through the two rings provided on the belt of the seat part The belt's central part of the back of the belt will extend further down and suspend a shock absorber under the human foot that carries the backpack. Propane gas cylinder and digestive liquid cylinder and battery or condenser or power supply controller or autopilot under the shock absorber The peripheral device of the backpack that suspends a video camera or the like and raises its center of gravity is a horizontal cylindrical envelope take-up device and a envelope (ball skin) with a horizontal length of about 1950 mm located at the top of the backpack. ) There is a guide to wind up the guide, the guide is in the form of a link through the envelope (ball skin) and the shape of the hopper with resin etc. The uppermost end of the envelope is connected to the winding device with a string or wire













It is like an unwinding and winding device that can wind up and wind a fishing boat net, and the envelope winding device can be moved by a motor in the backpack. The switch that winds up is on the right lever, and the right lever is structured to move up and down, left and right and back like the control stick of a zero-type ship fighter, and the method with multiple propellers is a device that changes the position of the flying object The propeller is linked to the back of the blade. The right lever is linked to the front / rear output and the vertical / left / right rudder of the rear of the blade. The left lever is roughly connected to the right lever, which is automatically connected by radio control and realizes automatic control by radio control, changing the position of the top and bottom, left and right and front and rear From the center of the upper part of the backpack that changes the vertical position, it is 19.5mm to 33mm in diameter and 195mm to 3300mm in length, and here is a pipe-shaped metal or resin or carbon fiber reinforced called torch. There is a cylinder that leads propane made of resin or glass fiber reinforced resin, and a small burner is installed at the top end of the cylinder of this torch, and an ignition device and a fire extinguishing nozzle are installed near the small burner The left lever is in a position that can be operated with the left hand on the left side from the person carrying the upper surface of the pack, and the amount of gas can be adjusted by turning the handle of the left lever, such as propane gas for hot air balloon and helium gas for rising These levers with ignition and fire extinguishing switches are on the left lever with the changeover switch. The control lever and the left lever are electrically connected to the autopilot, and the left lever shows the amount of propane inside the torch as viewed from the side of the backpack that is used for radio control and autopilot. A valve to be adjusted is installed, and an open / close button for the hot air or floating gas exhaust valve is installed on the valve. The valve for adjusting the amount of propane and the hot air exhaust solenoid valve are electrically connected to the autopilot. The lower end of the torch, which realizes manual, wireless and automatic maneuvering, is the combustion of a pipe that guides propane gas connected to a propane cylinder or a floating gas cylinder installed under the shock absorber at the foot of the man Around the area is a length 19 of 66 to 195 mm in diameter made of heat-resistant metal or fiber-reinforced resin called a combustion guard net. A 5 mm to 3300 mm net-shaped cylinder is installed around a small burner, and this net-shaped cylinder is structured to move up and down around the cylinder that sends propane. When using a burner when the cylinder that sends propane completely fits in the center of the net cylinder, this cylindrical net extends to the top of the small burner and prevents the envelope (ball skin) from burning with the heat of the burner. The burning guard net is swelled in a spherical shape with a diameter of 330mm to 990mm like a kerosene lamp glass squirt so that the envelope does not burn with the heat of the burner when the small burner is ignited. The method of extending the maximum cylindrical net upward is a small burner where the bottom of the cylindrical net protects the periphery of the burner A shaft that rotates the prober or the fan extends from the center of the back surface of the backpack where the digestion fluid is ejected when the envelope (ball skin) is burned by the heat of the burner. The diameter of the electric motor is about 19.5 mm to 33 mm and the length is about 19.5 mm to 66 mm. The electric motor is installed horizontally in the middle of the backpack. A fan guard similar in shape to the fan guard of a domestic fan with a propeller or fan fixed in the previous period has a cross-shaped rudder in the direction in which the air blows, and on the right side of the person riding on the side of the backpack The lever extends from the side of the backpack to the position of the right hand. The personal aerial work body moves up, down, left, and right by guiding the air blown back and forth from the rudder fixed to the fan guard to the top, bottom, left and right.This lever is electrically connected to the autopilot and is controlled by the radio control. The automatic operation of the left lever valve that adjusts the buoyancy of the hot air balloon by adjusting the burner power at the tip of the torch by adjusting the valve on the left hand lever of the passenger Balloon method is to adjust the amount of floating gas such as helium, rescue the rescuer by automatic control by radio control and take aerial shot with video camera, control by manual, wireless and automatic control, crew Is equipped with the shock absorbing human sleeping bag and shock absorbing air bag described above, and at the top of the envelope unwinding and winding device, the free fall is detected by the acceleration sensor and the human will Alternatively, a gas balloon method envelope equipped with a ballot chute that opens automatically is used. The base material of the balloon is 0.195 mm in diameter, using a mesh woven with fiber material and a cloth sealed with latex rubber or natural rubber. From 3.3 mm to 3.3 mm carbon fiber reinforced resin wire, the shape in which the mesh is braided from 330 mm to 1950 mm is the same size as the hot air balloon method. Latex rubber, natural rubber or urethane resin from the inside of a polyethylene terephthalate cloth bag in which a 0.195 mm to 3.3 mm thick cloth woven with polyethylene terephthalate cloth is bonded to the inside of the mesh The gas balloon is gas-tightened with a gas balloon. The tip of the hot-air balloon torch described above is introduced into the gas balloon to be airtight, and helium gas or hydrogen gas cylinder is installed instead of the propane gas cylinder, that is, the gas inside the balloon, that is, hot air is used. It can be used as a hot air balloon or a gas balloon by changing to hydrogen (explosion is prohibited because it explodes) or helium, the balloon opening is a hot air balloon method that spreads and collects heated air, and a gas balloon method The gas outlet tube is inside the envelope and the gas balloon method is like a flare skirt with a thin silicon rubber or rubber-based resin fiber sealed at the tip of the opening. This bundling method is tightly sealed and airtight so that gas does not leak as much as possible. Is to some extent since only needs to be obtained it is assumed that gas is leaking, personal aerial craft that combines an electric motor or an internal combustion engine and the balloon is divided into upper flight body and a lower suspension member. FIG. 47 shows from top to bottom of the truncated cone in order to describe how to form a kite that houses the cone shape envelope of the ice cream and the side of the truncated cone that forms the structure of the upper aircraft is a bowl. FIG. FIG. 48 is a view seen from above the side of the truncated cone in order to describe how to fold a bowl having a cone shaped side that houses the ice cream cone shaped envelope and forms the structure of the upper aircraft. It is. FIG. 49 shows a hot-air balloon, a gas balloon, a hot-gas balloon, a hot-gas balloon, and an ice cream cone-shaped suspension cable that has an envelope (bulb skin) housed in a cone-shaped bowl of ice cream. It is an overall configuration diagram of a personal aerial work flying object that can move up and down, front and back, left and right, with a propeller or fan that can project the beam at the four sides below the cage and change the direction of the electric motor with a spherical hinge at the beam tip . FIG. 50 shows a hot-air balloon, a gas balloon, a hot-gas balloon, a hot-gas balloon, and an ice cream cone-shaped with a suspension cable in which the envelope (ball skin) is housed in a cone-shaped basket of ice cream. It is a partial configuration view of a personal aerial work flying object that can be moved up and down, front and back, left and right, with a propeller or fan that can project the beam in the four directions below the cage and change the direction of the electric motor with a spherical hinge at the beam tip . FIG. 51 shows a hot-air balloon, a gas balloon, a hot-gas balloon, a hot-gas balloon, and an ice cream cone-shaped suspension cable in which the envelope (bulb skin) is housed in a cone-shaped bowl of ice cream. It is an overall configuration diagram of a personal aerial work flying object that can move up and down, front and back, left and right, with a propeller or fan that can project the electric motor with a spherical hinge at the beam tip and a spherical hinge at the beam tip It is a figure which shows the place which accommodated the envelope in the cone-shaped bowl of ice cream. FIG. 52 shows a hot-air balloon, a gas balloon, a hot-gas balloon, a hot-gas balloon, and an ice-cream cone shape in which an envelope (ball skin) is housed in a cone-shaped basket of ice cream. It is a partial configuration diagram of a personal aerial work flying object that can move up and down, front and back, left and right, with a propeller or fan that can project the beam in the four directions below the cage and change the direction of the electric motor with a spherical hinge at the beam tip . FIG. 53 shows a hot-air balloon, a gas balloon, a hot-gas balloon, a hot-gas balloon, and an ice cream cone-shaped with a suspension cable in which the envelope (ball skin) is housed in a cone-shaped bowl of ice cream. This is a cross-sectional view of the envelope of a personal aerial work flying object that can move up and down, front and back, left and right, with a propeller or fan that can project the electric motor with a spherical hinge at the end of the beam and a spherical hinge at the beam tip. It is a figure which shows that the suspension cable fixed to is wound up with the suspension cable winder under the cone-shaped bowl of ice cream. The upper flying object with the ice cream cup cone shaped saddle type envelope storage device is an arm that extends in the shape of a cantilever around the cup cone shaped ice cream and cup cone shaped ice cream that houses the envelope and envelope. An electric motor or an internal combustion engine is attached to the tip of the motor via a universal joint that can freely change the direction of the electric motor, and a propeller or fan is attached to the shaft of the electric motor or the internal combustion engine. The above-mentioned lower suspension body is attached to the tip of the lower part of the cup cone shape that moves the balloon in the up / down / front / back / left / right direction by changing the direction of the internal combustion engine, and the electric motor or the internal combustion engine and the hot air balloon or gas balloon on which a human can ride. Or heat and gas balloon How to make a cup cone-shaped bowl of ice cream that is automatically steered is as follows: The cup cone-shaped bowl of ice cream has a truncated cone shape with a circle with a small radius on the bottom and a circle with a large radius on the top From the circumference of the circle with a small radius at the bottom, from the three points divided by the pipe that the circumference is divided into three at the central angle of the lower link where the lower ring is made of metal or fiber reinforced resin Since the branches forming the ridges are two from three places, which are two to the left and right at an angle of about 30 to 60 degrees with respect to the ring surface, there are six in total, each one at each angle The spiral ends forming the spirals are connected to the upper link at the outer peripheral point with a central angle of 60 degrees, the six spirals constitute a mesh, and the intersections of the meshes that are regularly knitted are fixed with epoxy resin or the like Of the lower The upper ring is divided into three parts, and the upper part is divided into six parts, and the three parts connected by a belt member knitted into a net cage is for description. Actually, the lower ring is divided into 12 parts. 12 divisions that will be divided into 24 times may be 36 divisions. The division of the lower link may be any number that is dynamically adapted, anyway, the upper part will be twice that number, this way A large trash-like object with a truncated cone that combines the envelope storage knitted into the shape of the side and the structure of the upper flying object is formed. The storage method is to store the inner point of the load tape divided into the inside of the balloon due to mechanical considerations, that is, when the balloon is compared to the earth, the balloon is reinforced with the load tape like meridians and parallels. of A flexible wire that also serves as a suspension cable made of metal, resin, or carbon fiber reinforced resin is suspended from the intersection. A plurality of flexible suspension cable wires inside this envelope are installed in the lower part of the cup cone-shaped cage. To the roller of the suspension cable winder













By rotating this fixed roller, the suspension cable can be wound and unwound so that the envelope can be stored inside the cup cone-shaped jar with the envelope opened upward or taken out from the cup cone-shaped jar. At the bottom of the cup-cone-shaped cup that can be heated, the burner is installed with a space between the envelope and the burner that takes heat into consideration so that the envelope does not melt with heat. Is provided inside the cup cone-shaped bowl and the tip of the burner that leads to the gas blow-out port that also serves as the gas outlet hole is guided inside the envelope, and the cup cone-shaped bowl carries out and stores the envelope so that the envelope does not burn Cup cone with a small burner surrounded by a combustion guard net at the bottom of the envelope As mentioned above, the ice cream cup cone type flying body is a mixture of propane gas and helium gas burned and sealed as a hot gas balloon enclosed and sealed. This technology can be applied to airships, and aerial vehicles are used in an orderly manner in accordance with the Aviation Law.

Personal aircraft for leisure or recreation, tools for simple altitude work that does not require scaffolding, and application to safe aircraft. Surface treatment of civil engineering structures. Powerful and lightweight internal combustion engine, electric motor and generator, jet engine that prevents air pollution with noise, bird strike damage prevention, improvement of aircraft fuel consumption, three-dimensional printer, rapid prototyping, cutting modeling method. Development of light and tough composite materials. Air safety and aircraft noise reduction.

The 101 upper flying object is a thing for obtaining the ascending thrust of the personal aerial work flying object.
The lower suspension body 102 is a thing for suspending a person who works in the air or a heavy object.
The 103 propeller or fan guard prevents contact damage with other objects of the propeller or fan.
104 A person who works in the air.
201 is an envelope (ball skin) for hot air balloon gas balloon hot gas balloon.
202 Ice cream cone-shaped bag made of metal or fiber reinforced resin, which also serves as an envelope storage place.
The horizontal member of the cantilever beam that supports the electric motor 203 is a hinge that supports the electric motor, and controls the attitude of the flying object for personal aerial work by changing the inclination of the electric motor.
204 propeller or fan.
205 electric motor.
206 A simple method with a suspended body that supports heavy objects is a wire or a rope.
207 A simple method of impact absorbing material upon landing or falling is something like a balance ball.
A heavy object such as a 208 battery or a gas cylinder lowers the center of gravity of the flying object for personal aerial work.
401 propeller or fan.
402 electric motor.
403 is a horizontal member of the upper flying object.
The vertical propeller or fan guard 404 prevents contact damage between the propeller or the fan and other objects.
405 is a cable or wire for controlling the attitude by moving the center of gravity by changing the inclination of the upper flying object.
406 is a vertical member of the upper flying object.
It is the one used to assemble the upper flying body into a cross-girder shape by winding a 407 stainless steel wire and covering with epoxy resin or fiber reinforced resin tape.
501 Center where four vertical members sandwich a horizontal member, form a cross-girder shape, wind a stainless steel wire, wrap with epoxy resin or fiber reinforced resin tape and tie up the upper flying object into a cross-girder shape It is a member.
The 502 horizontal propeller or fan guard prevents contact damage with other objects of the propeller or fan.
601 is an upper flying object vertical member.
The 602 horizontal propeller or fan guard prevents contact damage with other objects of the propeller or fan.
603 is the upper turbine blade.
A permanent magnet such as a 604 neodymium magnet.
A 605 vertical propeller or fan guard prevents contact damage with other objects of the propeller or fan.
A permanent magnet such as a 606 neodymium magnet.
607 is an electric coil.
608 A disk that serves as a horizontal member of the upper aircraft to fix the electric coil, and the air is blown by the net shape of the slanted hole in consideration of the wind tendency so as not to hinder the blow by the rotation of the upper blade or the rotation of the upper blade. The blade has a blade shape having a blade pitch considering the wind tendency.
609 Lower turbine blade blade.
This is a ball bearing for facilitating rotation of the blade blade of the 610 turbine around the axis of the vertical member.
611 is a ball bearing bearing along the outer periphery of the turbine blade blade for facilitating the rotation of the blade blade of the turbine around the axis of the vertical member. The ball bearing 611 can be omitted.
This is an 801 metal piston cylinder.
802 metal cylinder head.
It is an 803 metal piston.
It is a 804 metal connecting rod.
805 metal crankshaft.
806 is a rotation shaft of the internal combustion engine.
807 is an air cooling fin around a metal combustion chamber.
It is a thermal buffer layer that can contain air in which a steel wool layer, a rock wool layer, and a glass wool layer, which are compressed from the inside and provided as a thermal buffer layer on the outer side of an 808 metal radiation fin, are laminated.
The inner surface of the fiber reinforced resin in contact with the 809 heat buffer layer 808 from the outside is processed into a pleated shape like an engine heat radiating fin of an air-cooled motorcycle and is wrapped with a heat resistant carbon fiber reinforced resin.
A fin structure 810 of heat-resistant fiber reinforced resin is wrapped with a honeycomb structure such as fiber reinforced resin and fiber reinforced resin, and is in charge of a mechanical member related to the strength of the internal combustion engine. .Thousands of small holes of about 3 mm are open.
811 A cylinder head that receives the explosive force of the internal combustion chamber and a cylinder with a metal bar of about one chopsticks that are commercially available penetrate the steel wool layer, rock wool layer and glass wool layer, Like thorns, a plurality of radiating wires are transmitted radially to transmit the explosive force to the fiber reinforced resin layer, and the tip of the bar is supported by a support provided in the fiber reinforced resin layer.
812 is a support provided in the fiber reinforced resin layer provided to transmit the explosive force of the internal combustion chamber to the fiber reinforced resin layer and to support the tip of the bar 811.
813 An explosive force of the internal combustion chamber is transmitted to the fiber reinforced resin layer and is a support portion provided on a metal portion provided to support the tip of the bar 811. There is a method of screwing into the hole of the part as a bolt.
814. Fiber reinforced resin in charge of mechanical load and a two-dimensional or three-dimensional honeycomb structure wrapping the fiber reinforced resin with a total heat dissipation diameter of 0.195 mm to 3. Although not shown in the figure, which is an infinite number of small holes of about 3 mm, dedicated pipes for blowing air directly onto the fins around the combustion chamber are arranged around each cylinder.
815 is a fan for forced air cooling utilizing the rotation of the internal combustion engine, and the air for forced air cooling is blown directly through a dedicated pipe to the metal fan around each combustion chamber, and the air cooling fan is a turbo that uses exhaust There is also a method that can be rotated by the power of the charger.
It is a guard that protects the 816 air cooling fan.
817 is a ball bearing that supports the rotating shaft of the internal combustion engine.
An oil pan covering the 818 crank chamber.
819 is a cooling fin around the oil pan.
820 engine oil.
821 is a combustion chamber of an internal combustion engine.
A 901 disk type rotor is a permanent magnet arranged radially and fixed along a concentric circle, and the direction of magnetic flux is orthogonal to the surface of the disk.
The direction of the magnetic flux is perpendicular to the surface of the disk in a fixed electric coil radially arranged along a concentric circle on a 902 disk type stator.
903 is a disk-shaped rotor fixed to the shaft of the electric motor.
904 is a stator with a hole through which a shaft fixed to the casing of the electric motor is passed.
The air opened for forced air cooling becomes a kind of air blower by rotating a hole that is inclined at an angle of 19.5 to 33 degrees with respect to the rotation surface with respect to the rotation direction of the 905 disk. It is a hole in the rotor that is opened with an inclination to feed backward.
Opened for forced air cooling that becomes a kind of blower by rotating the rotor so that air passes through a hole that is inclined at an angle of 19.5 to 33 degrees with respect to the surface of the 906 disc It is a hole in the stator that is opened with an inclination to send the generated air backward.
It is an infinite number of small holes with a diameter of 0.195 mm to 3.3 mm for overall heat dissipation, which are opened in the casing of the 907 electric motor.
908 is a guard for a forced air cooling fan.
This is a forced air cooling fan fixed to the shaft of a 909 electric motor.
It is a support that supports the ball bearing of the 910 bearing.
It is a ball bearing of 911 bearing.
It is a rotating shaft of a 912 electric motor.
It is a ball bearing of 913 bearings.
This is a casing of an electric motor made of metal or fiber reinforced resin with innumerable small holes having a diameter of 0.195 millimeters to 3.3 millimeters for heat radiation.
1101 is a hole through which the electric motor shaft of a disk-shaped stator fixed to the casing of the electric motor passes.
1201 Bird strike prevention device Fiber reinforced resin metal composite turbine laminated electric motor rotating shaft.
1202 Bird strike prevention device This is a ball bearing that supports the rotating shaft of the fiber-reinforced resin-metal composite turbine laminated electric motor.
1203 Bird Strike Prevention Device Fiber Reinforced Resin Metal Composite Turbine Laminated Type Electric Motor Concentric with the shaft, an electric coil is embedded in the blade and the blade has a hole with a hole through which the shaft of the electric motor passes. Blade type stator fixed to the casing of the electric motor, the tip of the wind-off part where the wind hits is processed into a blade shape with steel or aluminum alloy steel so that the meat pieces are crushed into minced state during bird strike It has become.
1204 Bird Strike Prevention Device Fiber Reinforced Resin Metal Metal Composite Turbine Laminated Type Electric Motor Blade Type Rotor with Blade Fixed to Shaft of Electric Motor Fixed with Permanent Magnet Embedded and Fixed Along Concentric Circle A permanent magnet such as a neodymium magnet in which the magnetic flux embedded in the blade is parallel to the axis of the electric motor.
1205 Bird Strike Prevention Device Fiber Reinforced Resin Metal Metal Composite Turbine Laminated Type Electric Motor Blade Type Rotor with Blade Fixed to Shaft of Electric Motor Fixed with Permanent Magnet Embedded in Blade The tip of the wind-off portion where the wind of the rotor blade hits is processed into a blade shape with steel or aluminum alloy steel, and the piece of meat is crushed into a minced state during a bird strike.
1206 Bird Strike Prevention Device Fiber Reinforced Plastic Metal Composite Turbine Stacked Electric Motor Concentric with the shaft of the electric coil embedded in the blade, and a blade with a hole through which the electric motor shaft passes is fixed at the center of the blade The magnetic flux embedded in the blade type stator fixed to the casing of the electric motor is an electric coil parallel to the rotation axis.
1207 Bird Strike Prevention Device Fiber Reinforced Resin Metal Metal Composite Turbine Stacked Electric Motor Casing of Electric Motor with Embedded Stator Blades Fixed to Electric Motor Casing, Not Shown in Figure, but Sensitive to Bird Strike A bird's minced meat piece crushed by detecting a bird strike with a vessel has a small window that automatically opens and closes with the detector when it collides with the casing due to centrifugal force and removes the piece of meat with the wind inside the electric motor outside the electric motor It is a mechanism to do.
1208 is a beam that supports a bearing provided at the air inlet.
1209 is a guide for gathering winds provided at the wind inlet.
It is a guide for restricting the wind provided at a 1210 wind outlet.
It is a beam that supports a bearing provided at a 1211-style jet nozzle.
1701 is a vertical member of a propeller or fan guard.
1801 is a detachable horizontal member that penetrates a rigid horizontal member.
1802 This is a product obtained by abutting a horizontal member for detachment from the left and right at the center of the horizontal member for rigid connection.
1803 A rigid horizontal member is inserted from one side, and the removable horizontal member is a cantilever.
1804 is a vertical member.
1805 is a rigid horizontal member extending on both sides.
1806 A rigid horizontal member extending to one side.
3301 is a lightweight, flexible and strong belt-like member in which a hemispherical metal and a fiber reinforced resin film on the upper part of 3301 are laminated and knitted into a bamboo basket shape. The crossing point of the belt is bonded and fixed with an epoxy resin or the like, so that the bag has a restoring force even if it is slightly deformed.
Speaking of the earth supporting the hemispherical ridges at the top of 3302, it is a ring made of a lightweight, flexible and tough belt-like member in which a metal corresponding to the position of the equator and a film of fiber reinforced resin are laminated.
This is a blade of a 3303 blade laminated electric motor. There is a method of forming an electric motor in which a permanent magnet or an electric coil is disposed on the blade. Alternatively, there is a method in which a permanent magnet is fixed to the tip of the blade and an electric coil is arranged on the outer ring.
This is a shaft of a 3304 blade type electric motor.
There is a method in which an electric coil is arranged on a ring on the outer periphery of a 3305 blade. It also prevents damage to the blade.
Speaking of the earth that supports the hemispherical ridges at the bottom of 3306, it is a ring made of a lightweight, flexible and strong belt-like member in which a film corresponding to the position of the equator and a film of fiber reinforced resin are laminated.
3307 is a material knitted in a bamboo basket shape with a lightweight flexible tough belt-like member in which a hemispherical metal and a fiber reinforced resin film are laminated at the bottom. The crossing point of the belt is bonded and fixed with an epoxy resin or the like, so that the bag has a restoring force even if it is slightly deformed.
It is a honeycomb sandwich structure plate with 3401 propeller or fan holes.
3402 is a vertical member for laminating a honeycomb sandwich structure plate having a propeller or fan hole.
It is a honeycomb sandwich structure plate with holes of 3501 propeller or fan.
A hole drilled in a honeycomb sandwich plate for a 3502 propeller or fan and electric motor.
3503 is a vertical member for laminating a honeycomb sandwich structure plate having a propeller or fan hole.
3701 is an exhaust port for discharging hot air, gas, and hot gas. The hot air balloon method is a lip panel, the gas balloon method is an open / close electromagnetic valve, and the open / close electromagnetic valve in the center of the lip panel is attached together by airtightly pressing or bonding the lip panel with a tape that can be hermetically bonded.
Panel member of 3702 envelope. It has a square, rectangular or trapezoidal shape.
3703 There is a method of using a fiber reinforced resin film material for the load tape bearing the stress in the vertical direction.
There is a method of using a film material of fiber reinforced resin for 3704, which bears a horizontal stress called a tape.
3705 Envelope panels are sewn horizontally and connected vertically, which is called Gore.
A flexible and strong Kepler fiber reinforced resin wire connecting the envelope, the load tape and the backpack with a suspension cable outside the 3706 envelope is used.
3707 An envelope around the net to prevent the envelope from being damaged when the burner burns in a net of kerosene lamps with a cylindrical shape at the top and a spherical shape at the bottom, is a heat-resistant material called Menox. This flyer-shaped net, in which the material is used, can move up and down along the torch. The combustion burner is located at the bottom of the spherical surface of the hoya-shaped net during flight and the burner is located at the upper part of the cylinder of the hoya when stored in the envelope.
When using as a hot air balloon at the opening on the lower surface of the 3708 envelope, it is open, and the method of using it as a gas balloon is that the member called the skirt from the envelope is pulled down to the lower part of a net like a sea bream and belted on an airtight torch It has a structure that prevents the binding gas from leaking and that the gas for rising or hot gas is ejected from the burner at the top of the torch.
A burner at the tip of a 3709 torch can burn propane with a hot air balloon, blow out a levitation gas with a gas balloon, or burn a helium propane mixed gas with a hot gas balloon to obtain a rising force.
A pipe for injecting a fire extinguishing liquid when a combustion gas such as propane called 3710 torch (torch), a gas such as helium for ascending, a propane helium mixed gas, etc. burns is provided.
A cable for guiding the winding from the top of the envelope with a hopper for winding the 3711 envelope passes through the hopper and is fixed to the rotating shaft of the envelope winding machine.
A hopper for winding the envelope with the 3712 envelope winder is located behind the winder, and a cable for guiding the winding from the top of the envelope passes through the hopper and is fixed to the rotating shaft of the winder. At the end of the envelope winding, the suspension cable can be wound together with the envelope. In the method of carrying out the envelope, the envelope winder is carried out by rotating the envelope winder in the reverse direction. Pull out the envelope with sufficient margin, and then manually or automatically ignite the burner to pull out the envelope to the end. A parachute is built in the center of the rear of the winder, and it can be opened manually or automatically.
Like the school bag belt used by 3713 elementary school students, the passenger passes his arms through the left and right belts to fix the body and backpack. The left and right belts can be fixed using buckles at the chest.
Like the school bag used by 3714 elementary school students, the passenger can pass the arm through the left and right belts to fix the body and backpack. The left and right belts can be fixed using buckles at the chest. It is a belt and a buckle that fix the chest.
3715 The belt and buckle that can be fastened to the left and right sides of the backpack from the left and right sides of the backpack to secure the abdomen of the occupant by using a buckle etc. It is.
3716 This is the left handle, the left handle controls the general vertical movement of the flying object, and the left handle extends from the left side of the backpack so that it can be operated with the left hand as seen by the person carrying it. There is a left lever on the left lever, and the amount of gas can be adjusted by turning the hand of the left lever. The gas has a changeover switch such as propane gas for hot air balloon and helium gas for rising or propane helium mixed gas. These switches with the ignition device and fire extinguishing device switches and the left lever are electrically connected to the autopilot device, and it is viewed from the backpack who carries the radio control and autopilot. The left lever has a valve that adjusts the amount of propane in the torch. Valve and the hot air exhaust solenoid valve for adjusting the amount of propane closing button of the exhaust valve is provided manually are contacted autopilot and electrically wired, wireless, are realized autopilot.
3717 This is the right lever, and the right lever extends from the right side of the backpack as seen from the passenger, and the switch that unwinds and winds the envelope is attached to the right lever, and the right lever is a zero-type warship battle It is structured to move up and down, left and right and back and forth like the control stick of the aircraft, and the movement of the flying object of the individual aerial works in conjunction with the movement of up and down, left and right and back and forth, so the method with multiple propellers or fans changes the position of the flying object The propeller or fan that is linked to the device has one back, and the movement of the right lever back and forth is linked to the propeller or fan output in the front-rear direction and linked to the vertical and horizontal rudder behind the fan guard. The position of the object can be manipulated, and it is also electrically connected to the autopilot device to realize autopilot by radio control. Left lever to change the minor up, down, left and right of the front and rear position in the right lever has a structure to change the position of the rough up and down.
The belt extends downward from the back of the 3718 backpack, and two belts that allow both feet to pass through the belt are fixed to the belt. can do.
A belt extends further down from the portion where the back of the 3719 backpack hits beyond the wheel through which both feet pass, and an impact absorbing material is fixed to the end of the belt, rope material or bar material.
3720 is an impact absorbing material such as a balance ball for landing and crashing methods.
It is a heavy object such as a 3721 battery, a propane gas or a helium gas cylinder, or a power supply control device, and functions to lower the center of gravity of the flying object for personal aerial work.
A backpack of the size of a backpack used by 3801 elementary school students, which is about the size of a rucksack that can be carried when climbing to Everest. At the top is an envelope winder on the back, with a propeller or fan and fan guard, and at the bottom and right and left rudder The belt, wire, rope or bar is stretched and the shock absorber and heavy load are suspended. The front part of the backpack is the shoulder belt, the chest belt, the abdomen belt, and the bilateral belt. The left handle right handle extends from the left and right sides of the fixed backpack, and the right handle controls the detailed movements of the front, back, left, right, up and down, and the left handle controls the movement of the flying object roughly in the air. is there.
A propeller or fan on the back of the 3802 backpack.
The propeller or fan guard on the back of the 3803 backpack.
3804 A vertical rudder on the back of the fan guard.
3805 Left and right rudder on the back of the fan guard.
3901 waterproof and airtight zipper with waterproof zipper is waterproof and airtight, and the purpose is to prevent the fabric from getting into the zipper. Each of the zippers on the sides of the zipper prevents the cloth from biting into the zipper when the zippers are sewn into the zipper's seams one by one with a width slightly exceeding the width of the zipper, and the zipper is pulled up The area where the fin and the fin that cover the zipper overlap with the silicone resin or rubber resin exactly seals the back and front of the zipper so that it is waterproof and airtight. The zipper can be pulled up and down easily without any damage, and at the same time the inside of the zipper is airtight and waterproof Is a zipper that does not catch airtight.
4001 is a fan guard rear vertical rudder.
4002 is a fan guard rear left / right rudder.
4003 A flexible and strong cable for winding and unwinding envelopes.
4301 burner gas outlet.
4302 is an envelope winder winding shaft.
4303 is an electric motor that rotates a rear propeller or fan.
4304 burner oxygen inlet.
The 4401 tip cylindrical root kerosene lamp squirt type envelope combustion prevention net is lowered to the envelope winding device when the envelope is stored.
4402 tip cylindrical root kerosene lamp squirt type envelope combustion prevention net is raised to the burner at the time of burner combustion.
The envelope pulled by the 4601 envelope take-up cable 4003 is gathered and enters the hopper of the envelope take-up machine.
The envelope winding cable and a part of the envelope are wound around the winding shaft of the 4602 envelope winding machine and are wound into the yarn winding state.
A side surface of the 4701 truncated cone is an upper ring of a bowl-shaped bowl.
The side surface of the 4702 truncated cone is a lower ring of a bowl-shaped bowl.
This is a bifurcation point of the diagonal material extending in a spiral manner in two directions from the divided points of the 4703 lower ring.
It is one diagonal of two diagonal materials that stretch while weaving diagonal materials diagonally at 33 to 66 degrees in one direction from the 4704 branch point. The intersection of the diagonal material and the diagonal material is epoxy It is fixed with resin.
It is one diagonal of the two diagonals that are stretched while weaving diagonals diagonally at about 33 to 66 degrees in the other direction from the 4705 branch point. The intersection of the diagonal and diagonal is It is fixed with epoxy resin.
4706 is an equally divided point of the lower ring.
The number of equally divided points in the 4707 upper ring is twice the number of equally divided points in the lower ring.
4901 is an exhaust port for discharging hot air, gas, and hot gas. The hot air balloon method is a lip panel, the gas balloon method is an open / close electromagnetic valve, and the open / close electromagnetic valve in the center of the lip panel is attached together by airtightly pressing or bonding the lip panel with a tape that can be hermetically bonded.
A 4903705 envelope panel is stitched horizontally and vertically connected, and is called a gore. In this method, a flexible and strong suspension cable such as a Kevlar fiber reinforced resin wire is disposed inside a load tape envelope.
It is a truncated cone shaped like a cone of 4903 ice cream. It becomes the structure of the upper flying body and winds up the suspension cable, so that the envelope can be stored inside the cone-shaped cone of ice cream.
A cantilever of a horizontal member for fixing an electric motor extending in all directions from the lower part of a cone-shaped truncated cone of 4904 ice cream.
4905 ice cream cone-shaped truncated cone can be freely changed the tilt of the electric motor with a spherical hinge attached to the tip of the cantilever of the horizontal member that fixes the electric motor extending from the bottom of the truncated cone It can be a spherical hinge.
5001 is a backpack that can be moved back and forth, left and right and up and down with an electric motor with an ice cream cone shaped truncated cone attached to the top of the backpack.
5101 is an envelope housed inside the cone-shaped bowl of cone shape of 5101 ice cream.
5303 is an exhaust port for discharging hot air, gas, and hot gas. The hot air balloon method is a lip panel, the gas balloon method is an open / close electromagnetic valve, and an open / close electromagnetic valve in the center of the lip panel is attached by airtightly crimping or bonding the lip panel with tape that can be airtightly bonded. It is an open / close electromagnetic valve at the center of the lip panel connected to the backpack.
A 5401 honeycomb structure is shown.
The 5402OX structure is shown.
A 5403 flex structure is shown.
5404 shows a bisecting structure.
5405 shows a feather structure.
It is a groove cut on the surface of 5501 resin or fiber reinforced resin.
This is a product obtained by cutting a raised portion of the square of the 5502 grid by laser processing.
The raised portion of the square of the 5503 grid is cut by laser processing and shaped like a sea urchin spine.
5504 is a resin or a fiber reinforced resin which becomes a base of weather resistant resin.
This is a weather-resistant substance that is deposited in a thickness necessary for weather resistance between grooves and spines formed by cutting a square that has been cut and raised in the grid of 5505 laser processing.
In order to resist the 5601 pulling force, there are a method in which steel wires are bundled in parallel and a method in which the steel wires are knitted like a hand-knitted sweater to form a belt. This should be used according to the application.
Assuming when muscle fibers are torn in 5602 muscles, the wire that shares the tensile force is put in the rheological body, and the method of bundling and binding the wires that suppress the progression of metal fatigue is also like a hand-knitted sweater The method of weaving the wire also puts the wire in the rheological body, but in the method of securing the strength, there is a method of putting the wire in the fiber reinforced resin in the rheological body, the method shown in the figure uses the rheological body Is the method.
It is a resin-made mantle for enclosing the 5603 rheological body.
The honeycomb structure in charge of 5604 compressive force simulates the structure of a turtle shell, and the section of the honeycomb structure in this portion shows a rigid honeycomb structure such as metal.
This belt member can be made gentle by the soft honeycomb structure made of resin around the section of the rigid honeycomb structure such as a honeycomb structure of 5605 metal, and the like.
5606 is a fiber reinforced resin base material that connects a wire in charge of 5606 and a honeycomb structure in charge of compressive force. The wire and the honeycomb structure are firmly bonded with an adhesive such as an epoxy resin.
In the cross section of the fuselage of the 5701 aircraft, it is an exoskeleton like a bamboo basket made by knitting bamboo using a belt member.
The cross section of the wing of the 5702 aircraft has an exoskeleton like a bamboo fence made by knitting bamboo using a belt member.
It is a cross-sectional view that supports the floor in the form of a wall with an object that supports the 5703 floor, and has a skeleton like a bamboo basket made by knitting bamboo using a belt member.
In the cross-sectional view of the 5704 floor, it is a plane skeleton like a bamboo basket made by knitting bamboo using a belt member.
In a cross-sectional view of the 5705 ceiling, it has a planar skeleton like a bamboo basket made by knitting bamboo using a belt member.
The 5706 both wings have a plane skeleton like a bamboo fence made of woven bamboo using a belt member in a sectional view divided into three sections to store fuel.
This is a stiffening part of the connection between the fuselage and both wings by the 5707 belt member.
It is a wall which suspends the ceiling by a 5708 belt member.
The body is a 5801 belt member.
It is a wing by a 5802 belt member.
This is a vertical tail with a 5803 belt member.
It is a horizontal tail with a 5804 belt member.
This is a stiffening braided joint between the fuselage and the wing by the 5805 belt member.
This is a joint portion in which a body and a tail are knitted in a stiffening manner by a 5806 belt member.
A 5901 piano wire or prestressed concrete steel wire is assembled and bundled in parallel to cope with the tensile load.
A rheological body in which 5902 piano wires or prestressed concrete steel wires are gathered and bundled in parallel to prevent the progress of fatigue failure between the wires. There is a method of using a fiber reinforced resin instead of a rheological body.
It is a section of a rigid honeycomb structure such as 5903 metal.
A rigid honeycomb structure such as 5904 resin surrounds a rigid section. Thanks to this flexible honeycomb structure, the belt member can be knitted.
5905 is an impact absorbing material having a shock absorbing material made of 5905 industrial gel material, Hanenite (registered trademark), urethane foam or resin ball, chemical fiber cotton and air, and hardened with epoxy resin or the like. The figure shows a resin ball.
5906 is an impact-absorbing material made of an industrial gel material, Hanenite (registered trademark), foamed urethane or resin ball, chemical fiber cotton and air, which is hardened with epoxy resin or the like. The figure shows a chemical fiber cotton and an adhesive for bonding resin balls.
5907 is a skin of fiber reinforced resin.
It is a net of piano wire or prestressed concrete steel wire that prevents the outer skin from being shredded when the 5908 body crashes. The pre-tension, that is, the pre-tensioning force and the expansion force that are applied in advance, are balanced so that the aircraft can be prevented from expanding in the sky. It is also a lightning prevention net for aircraft.
It is a fiber reinforced resin of 5909 endothelium.
The space inside the 5910 aircraft.
It is a mantle of resin encapsulating 5911 steel wire and rheology.
This is a fiber reinforced resin base material for fixing a 5912 steel wire and a honeycomb structure with an epoxy resin or the like.
6501 is a hopper portion of a movable vacuum hopper vapor deposition laser sintering laminated spraying apparatus.
6502 is a spraying device that sprays a weather-resistant substance mixed with an adhesive. The sprayed material is electrostatically transported to the work surface.
In a small silo in which the 6503 weathering substance is powdered metal, the metal fine powder is electrostatically transported, and the adhered metal fine powder adhering to the weathering processed surface is sintered by a laser device.
The vacuum pump that evacuates the 6504 hopper is seen from the outside.
This is a crucible having a 6505 gimbal structure and is an electric furnace crucible capable of vacuum deposition in any direction of 360 degrees.
It is a sucker made of silicon rubber or rubber that sucks the weather-resistant processed surface like a 6506 octopus sucker and evacuates the hopper.
6507 is an object to be weathered. Metal, concrete or wood.
This is a device that allows a 6508 hopper to rotate 360 degrees.
This is a truss-type arm that can move the 6509 hopper up, down, left and right.
6601 is a spherical hinge that changes the angle of the laser device.
6602 is a laser device that moves like an electron scanning line of an electron gun of a cathode ray tube for cutting, welding, or sintering a surface to be weatherproofed.
6603 is an openable / closable shutter that protects the laser device during vacuum deposition.
6604 is a silo containing fine powder of a substance to be weather-resistant processed.
6605 A shutter that can be opened and closed to protect a silo containing a fine powder of a substance to be weatherproofed during vacuum deposition.
It is a gimbal structure that keeps the crucible horizontal like a 6606 compass.
6607 is a crucible and electric furnace used in vacuum deposition.
6608 is a device that raises and lowers the position of the crucible.
6609 A shutter that can be opened and closed when the crucible is lowered and stored when the crucible is not used.
6610 is a shutter that can be opened and closed to protect the inside when spraying a material to be weatherproofed together with an adhesive liquid.
6611 is a vacuum pump that enables vacuum deposition.
The shutter can be opened and closed to protect the 6612 vacuum pump.
6613 is a potential that enables electrostatic transport.
6614 is an air inlet of a vacuum pump.
6701 A resin that has been pressed into a conduit or phloem to harden wood and hardened.
6702 resin is wood that has been hardened by press-fitting into a conduit or phloem.
6703 resin is a wood reinforced with a resin like a honeycomb structure in which a large number of holes are opened like a honeycomb structure in order to reduce the weight of the hardened and reinforced wood which is press-fitted into a conduit or a teacher's tube.
In order to reduce the weight of the hardened and reinforced wood that 6704 resin is press-fitted into the conduit or pedestal, the surface of the wood reinforced with resin like a honeycomb structure with many holes like a honeycomb structure is fiber reinforced. It is a fiber reinforced resin reinforced by coating with resin.
6801 plywood or laminated wood or the above-mentioned solid wood is reinforced with a resin and numerous holes are formed to make a honeycomb structure.
6802 It is made of resin such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 3.3 millimeters encapsulated with compressed air or gas of 1 to 3 atmospheres. A sphere is a small crushed egg grain shape with multiple numbers of children.
6803 A plurality of spherical or polyhedral resin spheres such as polyethylene terephthalate is an adhesive that is cured by containing air together with a plurality of small crushed egg grains.
6804 plywood or laminated timber or the above-mentioned solid wood is reinforced with resin and innumerable holes are formed, and compressed into 1 to 3 atm in the adhesive between wood and wood like a honeycomb structure. Spherical or polyhedral resin spheres such as polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and a diameter of 0.195 millimeters to 3.3 millimeters encapsulated in air or gas are small crushed egg grains The outer surface of the product cured by sandwiching the material reduced in weight by mixing and adhering the material of the material with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin is 3.3 mm to 195 mm thick It is a fiber reinforced resin that has been hardened by coating reinforcement.
It is sectional drawing of the thing which laminated | stacked papers, such as 6901 cardboard, was made to contain air, and was hardened with the adhesive agent.
A sheet of paper such as 6902 corrugated cardboard is laminated with air and hardened with an adhesive. A structure like a honeycomb structure, that is, a hexagonal or round hole like a hexagonal hole in a honeycomb structure is used for corrugated cardboard. To reduce the weight by making a plurality of small holes such as hexagons or circles with one side of a hexagon or a circle diameter of about 1.95 to 33 mm in order to make a plurality of holes spaced from millimeters to 33 millimeters It is a small hole. In other methods, 6902 indicates a small hole.
A paper structure such as 6903 corrugated cardboard, which is laminated with air and hardened with an adhesive, has a structure like a honeycomb structure, that is, a hexagonal or round hole like a hexagonal hole in a honeycomb structure is 19.5 on corrugated cardboard. To reduce the weight by making a plurality of small holes such as hexagons or circles with one side of a hexagon or a circle diameter of about 1.95 to 33 mm in order to make a plurality of holes spaced from millimeters to 33 millimeters This is a foamed resin whose surface is reinforced with a foamed resin such as urethane foam. In other methods, 6903 indicates a foamed resin.
A sheet of paper such as 6904 cardboard is laminated and air is contained and hardened with an adhesive. A structure like a honeycomb structure, that is, a hexagonal hole or a round hole like a hexagonal hole in a honeycomb structure is used for corrugated cardboard. To reduce the weight by making a plurality of small holes such as hexagons or circles with one side of a hexagon or a circle diameter of about 1.95 to 33 mm in order to make a plurality of holes spaced from millimeters to 33 millimeters A material whose surface is reinforced with foaming resin such as urethane foam, or a honeycomb structure in which a plurality of small holes of paper are provided with a plurality of holes spaced from 19.5 mm to 33 mm, that is, a hexagonal hole in the honeycomb structure This is a honeycomb structure in which the outer surface of the foamed resin reinforced with a material replaced by a circular hole is sandwiched with a metal or paper honeycomb structure. In other methods, 6904 shows a honeycomb structure.
A sheet of paper such as 6905 corrugated cardboard, which is laminated with air and hardened with an adhesive, has a structure like a honeycomb structure, that is, a hexagonal or round hole like a hexagonal hole in the honeycomb structure is 19.5 on the cardboard. To reduce the weight by making a plurality of small holes such as hexagons or circles with one side of a hexagon or a circle diameter of about 1.95 to 33 mm in order to make a plurality of holes spaced from millimeters to 33 millimeters A material whose surface is reinforced with foaming resin such as urethane foam, or a honeycomb structure in which a plurality of small holes of paper are provided with a plurality of holes spaced from 19.5 mm to 33 mm, that is, a hexagonal hole in the honeycomb structure Is a carbon fiber reinforced resin after the outer surface of the foamed resin is reinforced with a metal or paper honeycomb structure. Is a fiber-reinforced resins of what hardened coated reinforced at 195 millimeters thick 3.3 mm in fiber reinforced resin such as glass fiber reinforced resin. In other methods, 6905 indicates fiber reinforced resins.
7001 Thick paper with a thickness of about 0.195 to 3.3 mm is chopped with a corn flake shape of food with a square or rectangular side of about 1.95 to 33 mm or shredder used in office work The paper is mixed with air and stirred to make the paper wrinkled or wrap around the air, and it is half soft and fluffy. A fluffy paper fiber loosened object is mixed with air with an adhesive such as epoxy resin, stirred and compressed appropriately and molded into a member of the required strength. The required strength can be obtained by adjusting the amount of the agent.
Pressure gas made of resin such as spherical or polyhedral polyethylene terephthalate having a diameter of 1.95 mm to 33 mm and a thickness of 0.195 mm to 330 mm enclosed with compressed air or gas of 7101 atm to 3 atm is enclosed. The object is a thing like the shape of a small crushed egg with a number of children, or a spherical or polyhedral shape with a size of about a tennis ball to a volleyball.
7102 The diameter of the fiber shape is between 0.195 microns and 3.3 millimeters in size. Chemical fiber or natural fiber like cotton is mixed with an appropriate amount of an adhesive such as epoxy resin, and air is blown. It is a product in which a gap between a product in which a pressure gas made of resin is encapsulated and filled is hardened by filling an appropriate air with an adhesive such as a cotton-like fiber and a resin.
7103 paper or fiber tape or fiber reinforced resin or other film material tape wrapped between the tape and rolled tape while winding the material between the tapes like a laver rolled sushi roll Pressure gas made of resin such as spherical or polyhedral polyethylene terephthalate having a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 330 millimeters enclosed with compressed air or gas of 1 to 3 atmospheres is enclosed. The object is like a small crushed egg particle shape with a number of children, or a spherical or polyhedral and fiber shape with a diameter of about 0.195 microns to 3.3 millimeters. Make the chemical fiber or natural fiber with tensile force like cotton Mix together the appropriate amount of adhesive such as epoxy resin, soak in the air, stir and paste the pressure gas made of resin into the gap between the cotton-like fiber and resin Is a tape-like material used for a fiber-reinforced membrane material tape or a commercially available tape packed between air and filled with air.
7401 is a manufacturing base on which a molten metal laminate forging fixing technique is performed, and lamination is performed thereon. In another lamination method, this number means a laminated production base.
7402 is a first-stage laminated metal.
This is a main body of a ceramic mold having a 7403 hopper and capable of maintaining a high temperature below the melting point by electricity.
7404 is a ceramic mold hopper.
This is a pressure chamber for extruding 7405 layers of molten metal with an inert gas.
7406 is a second layer metal.
7407 is a hole made of ceramic-molded mold that has a mesh shape for three-dimensional lamination.
A chute for dropping 7501 layers of molten metal and an apparatus for injecting one more layer by increasing the pressure of the inert gas by closely contacting the chute and lowering the chute.
7502 is a machine-driven computer-controlled hammer adjusted to a hitting degree so that the mesh shape becomes slightly thick before the metal such as the mesh-shaped steel that is laminated is cooled and hardened.
7601 is a sheet of metal such as first-stage steel to be laminated.
7602 is a sheet of metal such as second-stage steel to be laminated.
It is a laser device that moves like a three-dimensional printer that welds sheets according to the shape of 7603 laminated sheets.
7604 is a machine-driven computer-controlled hammer that is adjusted so that the mesh shape is slightly thickened before the laminated sheet of net-like steel or the like is cooled and hardened.
The 7605 sheet is a portion that is welded and fixed by a laser technique so that the sheet does not peel off.
7701 is a lamination target figure using a wire or conductive ink to be a lamination target.
7702 is an electrode for charging the vapor deposition material. Although it is the lower part in the figure, there is a method of inserting a rod-shaped electrode into the melting surface.
7703 is an electrode at the bottom of the crucible. Although it is the lower part in the figure, there is a method of inserting a rod-shaped electrode into the melting surface.
7704 A crucible for storing molten metal.
7705 A crane-neck-shaped lid that prevents evaporation and diffusion of molten metal.
7706 is a crane neck portion of the lid of the crucible for diffusive electrostatic transport of molten metal vapor.
7707 is a molten metal vapor that is intensively and selectively adsorbed to the target lamination pattern from the opening of the 7707 crane neck.
7708 Molten metal inside the crucible.
7709 molten metal vapor.
7710 is a hermetic contact point between the lower crucible for accumulating molten metal and the crucible at the bottom of the crucible lid with the crucible-shaped tube at the top of the crucible preventing the entire diffusion of molten metal vapor.
7711 is a molten metal vapor that is selectively and intensively adsorbed onto a target graphic.
7712 is an airtight contact between a crucible at the bottom of the crucible lid and a crucible-shaped tube at the top of the crucible that prevents the entire diffusion of molten metal vapor. Although they are essentially the same, different numbers are added in this figure.
7801 is a wall for fixing a stack of stacked paper.
7802 is a bundle of stacked paper.
7803 Ink containing metal powder to be laminated
It is a three-dimensional figure made of fine metal powder that has penetrated and become familiar with paper.
7804 paper is a column that bonds paper and protects the three-dimensional structure and facilitates transport of a bundle of paper.
7805 Oily or water-soluble air contact curable curing agent and the figure to be laminated on the paper or resin fiber nonwoven paper placed on the production base using ink containing a mixture of fine metal powder to be laminated It is a device that draws and stacks like a three-dimensional printer.
7901 Silicone rubber sucker layer Shock absorbing layer Honeycomb structure layer Fiber resin layer Interlocking part This is a palate bone inside a human gum with a metal ceramic composite laminated denture.
7902 Silicone rubber sucker layer Shock absorbing layer Honeycomb structure layer Fiber resin layer Interlocking portion This is meat around the periphery of a human gum fitted with a metal ceramic composite laminated denture.
7903 is a shock absorbing material such as urethane foam for medical use.
A honeycomb structure such as 7904 fiber reinforced resin.
7905 is a fiber-reinforced resin that is safe for medical use.
7906 A medical safe metal layer.
7907 is a device for fixing a metal layer safe for medical use to a resin.
7908 is a surface of a fiber-reinforced resin that is safe for medical use.
7909 It is a sucker such as silicon rubber that is safe for medical treatment. The dentures as a whole are suckers, and the gums remove the air inside the dentures so that they are snugly adsorbed, making it difficult for fragments of rice crackers to enter between the dentures and gums.
8001 Silicone rubber sucker layer Shock absorbing layer Honeycomb structure layer Fiber resin layer Interlocking part Metal ceramic composite Laminate metal that gently stabilizes the upper and lower dentures and is covered with impact absorbing material on the surface of the temporomandibular joint so that the temporomandibular joint is free It is a shape memory alloy in which the shape is memorized at a temperature close to body temperature or a movable steel spring.
It is used for multiple purposes in the spherical space of the fuselage of the 8201 flying object.
It is relatively wide and versatile in the wing space of the 8202 flying object.
The wide space inside the 8301 sphere is used for multiple purposes, and it is possible to form a plurality of floors by supporting the honeycomb structure floor with the ridge-shaped walls and floors. Because it is possible, it is a spherical exoskeleton used for multiple purposes.
Application of 8501 sandwich belt member Thick flying squirrel Simulates the total lift The flying object is a flying object simulating a thick flying fish with a skeleton-shaped exoskeleton. According to the theorem, the entire flying object has a structure like a cross section of a wing, and the wing portion of this flying object that has lifted by generating a pressure difference between the upper and lower parts is cut in the direction in which the flying object travels.
8601 stubby and thick wings.
The connecting portion between the 8602 wing and the fuselage is reinforced by braiding with a sandwich belt member.
8701 Bird strike prevention device Fiber reinforced resin metal composite turbine laminated electric motor where wind is sent backward.
8702 Forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine is used to obtain rotational power by using a forced air-cooled whole heat-dissipating fiber-reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor as a generator Device.
8703 Bird Strike Prevention Device Fiber Reinforced Resin / Metal Composite Turbine Laminated Electric Motor Inlet.
9101 sphere center disc outer periphery plural duct fan disc outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging dropable flying object is a spherical part knitted with sandwich band member of flying object.
9102 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigating parachute installation fuel generator ballast hanging bird strike prevention device to obtain the traveling force of fallable flying object fiber reinforced resin metal composite turbine laminated electric motor It is a motor.
9103 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging vertical wall inside the wing of the disk part of the dropable flying object.
9104 Flying object exoskeleton is braided with sandwich belt members, and the duct engine has a structure in which the duct engine is blown and floated to the bottom by a plurality of duct engines in the middle of the cylindrical height A cross-shaped beam is provided, and two rotary engines or a twin-type horizontal piston forced air-cooling whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine is fixed above and below the center of the cross. This is a cylindrical duct fan for obtaining a levitation force by a plurality of duct fans around the outer periphery of the disk which is a rotating duct fan.
9105 sphere center disk outer periphery plural duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging horizontal wall inside wing of disk part of dropable flying object.
The bottom end of the 9106 sphere has a structure that allows heavy loads such as generator fuel to be hung at the bottom like a ballast tank. When the airflow is bad, the heavy portion of the ballast generator or fuel is suspended below. This ballast part that lowers the center of gravity and prevents the entire disk from rotating to the top and bottom can be separated and separated from the spherical disk body in a safe position in order to reduce the weight when falling It is a ballast part.
9107 sphere center disk outer periphery plural duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging vertical wall of the spherical part of the dropable flying object.
9108 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installed fuel generator ballast hanging horizontal floor base that supports the honeycomb structure floor of the spherical part of the dropable flying object.
9109 sphere center disk outer periphery plural duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installed fuel generator ballast suspended part of the wing shape of the disk around the sphere of the fallable flying object.
9110 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installed fuel generator ballast suspended horizontal falling floor base of honeycomb structure etc.
9111 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installed fuel generator ballast suspended horizontal drop base for supporting the honeycomb structure floor of the spherical part of the flying object.
9201 is a cross-sectional view of a wing-shaped portion of a disk around a spherical shape of a flying object capable of hanging and dropping a fuel generator ballast suspended by a parachute installed fuel generator ballast;
9301 sphere center disk outer periphery plural duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast suspended vertical falling wall woven vertical wall sandwiched belt member
9401 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast suspended fallable flying object disk outer periphery part duct fan is installed between duct fans This parachute is opened at the time of falling, and the opening of the upper part of the parachute is opened with a wire at the time of falling to induce the fall of the spherical disk, so that it falls down like a fluttering leaf and a leaf flies and relaxes the collision with the ground It is. This contains a float that spreads like an air bag when it touches the sea.
9501 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast suspended fallable flying object disk outer periphery part duct fan multiple installations between duct fans This parachute is opened when it is dropped, and a plurality of parachutes are opened when it is dropped. In the figure, the number of parachutes is four, but in reality, only the number of duct fans is necessary, and the number and weight of parachutes are considered to be important numbers and weights compared to human life. The method of transporting about 900 people in the air must give priority to human life.
9502 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall falling mitigation parachute installation fuel generator ballast hanging dropable flying object disk outer peripheral part duct fan multiple installations between duct fans This parachute is a trajectory that opens when it falls and opens the mouth of the upper part of the parachute with a wire when it falls to induce the fall of the spherical disk, and flutter and leaves flutter.
The bottom end of the 9601 sphere has a structure that allows heavy loads such as generator fuel to be hung at the bottom like a ballast tank. When the airflow is bad, the heavy parts such as the generator and fuel of the ballast are suspended below. This ballast part that lowers the center of gravity and prevents the entire disk from rotating to the top and bottom can be separated and separated from the spherical disk body in a safe position in order to reduce the weight when falling The lowermost part of this suspendable sphere is suspended from the vertical wall of the sphere part to the lower part and can be raised and lowered by the lifting device and dropped to a safe position in an emergency.
The bottom end of the 9602 sphere has a structure that allows heavy loads such as generator fuel to be hung in the lower part like a ballast tank, and when the air current is bad, the heavy parts such as the ballast generator and fuel are suspended below This ballast part that lowers the center of gravity and prevents the entire disk from rotating to the top and bottom can be separated and separated from the spherical disk body in a safe position in order to reduce the weight when falling The bottom part of this suspendable sphere is suspended from the vertical wall of the sphere part and suspended from the vertical wall of the sphere part to the lower part of the sphere part which can be raised and lowered by the lifting device and dropped to a safe position in an emergency. This is a suspended member.
9701 sphere center disk outer periphery multiple duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast hanging dropable flight object spherical disk outer periphery is processed into wing shape and both left and right wings are elongated It is a thing.
9901 propeller or fan.
This is a forced air-cooling air suction port of a 9902 rotary engine or a forced-air-cooling whole heat-dissipating fiber-reinforced resin-metal composite internal combustion engine of a twin-engine horizontal piston.
This is a 9903 rotary engine or a forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite internal combustion engine of a twin-engine horizontal piston.
A duct engine having a structure in which a plurality of duct engines are blown down and floated on the outer peripheral portion of the 9904 disk portion is a cross-shaped beam in the middle of a cylindrical height.
9905 sphere center disk outer periphery plural duct fan disk outer periphery part wing shape tree leaf fall fall mitigation parachute installation fuel generator ballast suspended fallable flying object disk outer periphery part duct duct cylindrical duct.
Although it is a 9906 bird strike prevention net, it may not be.
This is a base cloth for sewing 10301 zippers.
10302 This is the portion of the fabric that is zipped together.
10303 is the place where the zipper joint bites the zipper cloth.
10304 is a resin fin that prevents biting of the base fabric into the zipper at the upper left of FIG.
10305 is a resin fin that prevents biting of the base fabric into the zipper at the upper right of FIG.
10306 is a resin fin that prevents biting of the base fabric into the zipper at the lower left of FIG. 10306.
10307 is a resin fin that prevents biting of the base fabric into the zipper at the lower right of FIG. 10307.
10308 is where the zipper joint fitting is engaged on the left and right.
A silicone rubber is in contact with the upper portion of the 10309 zipper to achieve waterproof and airtightness at the portion where the fins and fins made of resin overlap.
In the lower part of the 10310 zipper, a silicone rubber is in contact with the part where the fin and the fin made of resin overlap each other in order to realize waterproofing and airtightness.
The base to which the 10311 zipper is attached, the cloth portion of the zipper and the fin made of resin are sewn together with a thread or the like and joined together.
10401 ray simulated flying object four bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable bouncer torque converter clutch forced air cooling whole heat radiating fiber reinforced resin A metal composite rotor permanent magnet stator electric coil disk stacking type generator motor output power transmission and transmission integrated hybrid device is used to obtain propulsive force.
The duct engine of the 10402 ray simulated flying object has a cross-shaped beam in the middle of the cylindrical height, and two rotary engines or two zero-type warships on the top and bottom of the center of the cross Engine twin-engine horizontal piston simulated forced air cooling Whole heat radiating fiber reinforced resin metal composite internal combustion engine fixed up and down at the center of the cross beam Two upper and lower propellers or fans fixed on the shaft of each internal combustion engine rotate inside the cylindrical shape The exhaust of the engine that is the duct fan is taken into the silencer in the disk and purified through a ceramic filter and exhausted from the lower surface of the disk between the upper and lower internal combustion engines in the cylindrical duct of the disk. There is a method of obtaining electric power simultaneously with buoyancy by installing a composite rotor permanent magnet stator electric coil disk stacked generator Forced air-cooled whole heat-dissipating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable adjustable push-wheel torque converter clutch forced air-cooling whole heat-dissipating fiber reinforced resin metal The composite rotor permanent magnet stator electric coil disk stacked generator motor output power transmission and transmission integrated hybrid device is combined to obtain buoyancy.
This is a fuselage in which a sandwich band member of a 10403 ray simulated flying object is knitted into a hook shape.
10404 ray is a wing obtained by knitting a sandwich band member of a simulated flying object into a hook shape.
A vertical wall of a wing obtained by knitting a sandwich band member of a 10405 ray simulated flying object into a hook shape.
10406 ray is a vertical tail wing obtained by knitting a sandwich band member of a simulated flying object into a hook shape.
This is the base of the center floor that is obtained by knitting a sandwich band member of a 10407 ray simulated flying object into a bowl shape.
This is a central wall obtained by knitting a sandwich band member of a 10408 ray simulated flying object into a hook shape.
This is a wing tip part obtained by knitting a sandwich band member of a 10409 ray simulated flying object into a hook shape.
This is a wall that cuts the body of a 10501 ray simulated flying object sandwich band member knitted into a bowl shape.
10502 ray is a tail part obtained by knitting a sandwich band member of a flying object in a hook shape.
This is a tail end of a 10503 ray simulated flying object sandwich band member knitted into a hook shape.
10601 is a sightseeing observation window for a simulated flying object.
10602 ray simulated flying object bird strike prevention device Fiber reinforced resin metal composite turbine laminated electric motor inlet.
10603 ray simulated flying object bird strike prevention device Fiber reinforced resin metal composite turbine laminated electric motor exhaust port.
10701 The ray simulated flying object, which is a storage place for a plurality of parachutes, has a structure in which a leaf flies in the air in the event of a crash and softens a collision with the ground.
The 10801 ray simulated flying object is structured such that when it crashes on the sea, it floats like an air bag and does not sink into the sea.
The 1002 ray simulated flying object has a structure in which heavy objects such as a fuel tank and a generator can be taken in and out while hanging under the air current. The ray simulated flying object has a structure in which the center of gravity is below and does not rotate in the vertical direction. A simulated flying object has a structure that can drop a heavy ballast under a heavy object such as a fuel tank or a generator to a safe place in the event of a crash, like an auxiliary fuel tank of a Type-0 ship fighter. In the event of a crash, the area around the lower ballast is made of a shock absorber to soften the crash shock and the air bag-like float swells to ease the impact.

Claims (2)

The personal aerial work flying object has a structure simulating the seeds of dandelions flying in the sky. From here, the material of the material of the personal aerial work flying object, which is a description of the light and strong material of the personal aerial work flying object As a form of protein, a basic structure such as a metal or a resin corresponding to an amino acid, a fiber reinforced resin, or the like, which has a structure simulating a chemical structural bond model of protein, is bonded with multiple branches such as peptide bonds. Conformation domain (conformation) motif (super secondary structure) fold protein (folder structure) of the primary, secondary, quaternary, and quaternary binding side chains of proteins that make up a three-dimensional structure. 3D structure considering tension member and compression member so as to meet mechanical needs by mechanical structural mechanics analysis by computer so as to constitute There is a method that uses a cutting three-dimensional modeling technique or a three-dimensional three-dimensional lamination technique to determine and manufacture. The term “honeycomb” used in this claim means a broad-sense honeycomb structure such as a weir-ferran structure, and a hexagonal honeycomb structure Or the term fiber reinforced resin, which includes OX structure, flex structure, bisecting structure, or feathered structure, is defined as a term that refers to carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin, etc. In order to realize a personal aerial working flying object, the present invention claims that a lightweight and toughened laminated composite material is invented by using a large amount of honeycomb structure and fiber reinforced resin. The term is defined as an object flying in the air, and various fighters or passenger planes Or there are methods that use waterproof paint or weather resistant resin on the outer surface of the flying object, including methods that apply techniques and materials of personal aerial work flying objects in helicopters, airships, spacecrafts, artificial satellites, space stations, etc. A simple method of weathering a personal aerial work flying object according to the present invention is the method described in the claims of the present invention on the surface of steel and has a diameter of about 3.3 nanometers to about 1.95 millimeters and a height of 3 The weather resistant resin, which is a method of processing a plurality of sea urchins at intervals of about 3.3 nanometers to about 1.95 millimeters at intervals of about 3.3 nanometers to about 1.95 millimeters and vacuum-depositing titanium, aluminum, or glass on the surface, Using a laser technique on the surface of epoxy resin, etc., cut multiple grooves with a thickness and depth of about 3.3 nanometers to about 1.95 millimeters. A square surface with a side of about 3.3 nanometers to about 1.95 millimeters is cut by laser technology and cut to a diameter of about 3.3 nanometers to about 1.95 millimeters with a height of 3.3 nanometers. 1 to 1.95 millimeters from 3.3 nano to 1.95 millimeters at intervals of a plurality of sea urchin strips, such as titanium or aluminum, or layers of metal or glass are layered alternately. Or by laminating a single material to form a film, laminating a vacuum-deposited film, and burying the portion cut out by laser technology as much as necessary for weather resistance, and laminating amorphous oxidation and UV protection This is a product that has improved the weather resistance of resins by creating a film, and the manufacturing method of this weather resistant resin is to make a resin body as a fiber reinforced resin. It can be used for weathering surface treatment of civil engineering structures such as steel, tools, machinery, automobiles, reinforced concrete, etc. The surface treatment of flying objects is a surface by a movable vacuum hopper vapor deposition sintered lamination spraying device instead of painting. The movable vacuum hopper vapor deposition laser-sintered laminating spray equipment that can be processed is constructed by replacing the baking part of electrostatic coating with laser technology by applying vacuum vapor deposition and electrostatic coating in combination. The problem of peeling between layers in the laminated method is solved by cutting technology such as sea urchin spines. There is a method in which the mixture is mixed with the liquid and fixed on the sprayed surface from the nozzle to the processed surface and baked by the method described in the claims. Or, the crucible of a normal vacuum deposition apparatus has a gimbal structure and the vacuum deposition direction can be 360 degrees, and the movable vacuum hopper atom molecule implantation spray deposition powder electrostatic transport laser welding sintering laser cutting spine processing lamination method surface In the weathering method, a square or conical funnel-shaped hopper having a bottom surface with a bottom of about 195 mm to 3300 mm, which creates a vacuum in the hopper, is used, and a bottom surface of the silicon-based resin or along the bottom surface of the hopper A sucker-shaped object made of a rubber-based resin that is kept airtight, so that the octopus's sucker sticks to anywhere. Like a cathode-ray tube electron gun from the top of the square or cone toward the bottom surface after vacuuming In addition, weathering fine particles are sprayed from the nozzle at high pressure for weathering processing on the surface processing site using laser technology, and the charged atoms, molecules or fine particles necessary for weathering are electrically electrostatically transported for weathering. Transporting to the processing surface to secure the properties or electrically charging atoms, molecules or fine particles by moving like an electron gun and accelerating using an electric field, and laser processing is the electron gun's cathode ray tube Scanning lines on the scanning surface move like electrons, and a weather-resistant substance is welded and fixed on the processing surface, or electrostatic transport is required to be processed by laser technology like scanning line electron movements. Powder electrostatic transport that welds or sinters the surface or evaporates the weathering substance with a gimbal crucible and electrostatically transports and deposits it to fix the weathering substance to the work surface. There is also a method of laser welding and sintering. Ultrasonic waves are applied to fine particles that are in a charged state and diffused by electrostatic transport. There is also a method of bonding to a weather resistant processed surface by vacuum evaporation. The surface of the resin layer or metal layer is melted by laser technology by electrostatically transporting it to the processing surface while diffusing with fine powder ultrasonic vibration of about 3.3 nanometers to 0.195 millimeters in size of the resin or metal. Then, a resin layer or a metal layer that is welded or bonded by sintering and bonding is formed, and a charged fine fiber fragment having a size of about 3.3 nanometers to about 0.195 millimeter is electrostatically applied to the processed surface. A resin layer or a metal layer is formed on the surface of the resin or metal that has been transported to form a fiber layer by the method described in this claim. Cut a plurality of grooves from 3.3 nanometers to 0.195 millimeters, and the square side with a square of 3.3 nanometers to 1.95 millimeters on one side of the grid is cut by laser technology and cut into diameters. Is an object such as a sea urchin elongated spine having a height of about 3.3 nanometers to 1.95 millimeters and a height of about 3.3 nanometers to about 1.95 millimeters. A square surface is processed, and a quantity of titanium or aluminum metal or glass necessary for weather resistance is melted on a plurality of spines with a gimbal crucible. The crucible is heated in an electric furnace to evaporate the weather-resistant material and process the surface. Vacuum-deposited and vapor-deposited on these weather-resistant materials to create a vacuum space. In addition, this method includes a method of performing weathering processing on a metal surface by directly applying laser-processed spines to the base of the structure, and then depositing the weathering material, which is applied not only to flying objects but also to existing structures. The above-described series of processes that can be applied to can be automated robot construction, and the above is a description of the light and tough material of the flying object for personal aerial work. The application of laminated honeycomb structure fiber reinforced resin composite technology for flying objects is applicable to denture manufacturing method applying beam theory on elastic floor, from here silicon rubber sucker layer shock absorption layer honeycomb structure layer fiber resin layer meshing Silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part metal ceramic composite laminated denture manufacturing method, which is a description of part metal ceramic composite laminated denture manufacturing method Place the gypsum male mold on the gypsum male mold base around the gums in the oral cavity of the human mouth where you want to put the denture, and then spray the gypsum gum male mold with a medically safe release material layer The method of laminating from a soft resin that is safe for medical use to a hard resin is a method of laminating a computer using the theory of beams on an elastic floor so that when the force is applied to the denture, the force is applied to the entire gum. The first layer in which the dentures come into contact with the gums is a medically safe silicone rubber sucker layer on which a honeycomb structure as an intermediate layer on top of a stress buffer layer that is a stress buffer layer such as foamed urethane This is a denture surface layer made of a fiber-reinforced resin that is relatively thin and made of fiber-reinforced resin on a honeycomb structure and is made of a fiber-reinforced resin that is safe for medical use and has a thickness of about 1.95 mm to 3.3 mm. The resin is a fiber reinforced resin in the tooth portion, and only the meshing portion at the top end of the tooth is 0.195 mm to 3.3 mm in thickness, which is safe for medical use, sintered metal, or metal ceramic. Or porcelain or ceramic, or a composite of these metals and ceramics, and the dentures as a whole are 0.195 mm to 0. When the denture is pressed by a denture that is soft enough to move about 33 millimeters and the engaging part is hard and at the same time the resin part can be deformed, the shock absorber transmits the force to the fiber reinforced resin through the honeycomb structure. It is a denture with a stress buffer layer made of shock absorbing material that can distribute the force to the entire gum The inner surface of the denture is made of medical silicone rubber and has good adhesion, and the gum removes the air inside the denture so that it sticks to the gum exactly like a sucker, and a piece of rice cracker is between the gum and denture It is a structure that does not hurt when it enters, and the metal or ceramic or metal-ceramic composite that forms the complete tooth shape of the meshing part by laser cutting technology is only the meshing part and the resin of the meshing part is booked The sea urchin spine described in the claims is processed on a medically safe resin, and the necessary amount of medically safe titanium is deposited or coated with an adhesive on the meshing part and titanium powder is applied. The surface of the denture is sintered by laser technology, or the meshing part is made of titanium in a thin horseshoe shape with a fiber reinforced resin with a return at the center of the teeth Shape memory memorized with a spring or body temperature that is safe for medical use and covered with resin so that the upper and lower dentures can be moved softly at the end of the dentition, which may be fixed using an adhesive in place A steel material with a shock absorber attached to the back of the alloy or a spring material, or a shape memory alloy wire material or a metal material with a shape memorized at body temperature, or a metal material coated with a resin or shock absorber material is embedded in the denture. The force of sticking the teeth to the palate with the viscosity of saliva is gently supplemented with the restoring force of the metal, and the teeth are stabilized in the palate, and the substances in the denture resin have medically safe medical effect substances, for example regularly under the guidance of a doctor Functional dentures infiltrated with anti-diabetic drugs or other substances that relieve the mood are included in this method, and they are strong, light, and strong, comfortable to wear and not painful It is possible to manufacture comfortable dentures that do not hurt anything and feel comfortable. Silicone rubber sucker layer Shock absorption layer Honeycomb structure layer Fiber resin layer Interlocking metal ceramic layer Metal and resin and impact that stabilize dentures above and below A manufacturing method in which an absorbent material and a silicone rubber sucker layer are separately manufactured and assembled using a medical adhesive such as an epoxy resin is also included in the scope of the present invention. Fiber resin layer meshing part Metal ceramic composite laminated denture manufacturing method description, from here on the description of the material reinforced and reinforced with a fiber reinforced resin on the surface of the honeycomb structure made of wood, paper, resin and foam resin, etc. As a structure of the flying body, solid wood conduits and mentor pipes are stuffed with curable resin to strengthen the wood, and then the hexagonal shape such as honeycomb structure A hexagonal shape with a side of about 1.95 millimeters to 33 millimeters or a circle with a diameter of about 1.95 millimeters to 33 millimeters with a plurality of small holes at intervals of about 1.95 millimeters to 33 millimeters. Generate multiple small holes on the surface











Foam such as foam urethane

The outer surface is filled with a fiber reinforced resin such as a carbon fiber reinforced resin or a glass fiber reinforced resin instead of a material reinforced with a resin and reinforced to a thickness of about 1.95 to 33 mm or a foamed resin such as urethane. What is hardened by covering and reinforcing 95 to 33 millimeters, or plywood or laminated timber or solid wood described in the scope of claims, is reinforced with resin and has a side of about 1.95 to 33 millimeters. In the adhesive between wood and wood of hexagonal shape or a circle with a diameter of about 1.95 to 33 millimeters and drilling a plurality of holes at intervals of 19.5 to 33 millimeters like a honeycomb structure From 1.95 mm in diameter, which is filled with compressed air or gas at 1 to 3 atm. Resin spheres such as polyethylene terephthalate, such as spherical or polyhedral polyethylene terephthalate, with a thickness of 33 millimeters from 0.195 millimeters to 3.3 millimeters are mixed with a small crushed egg grain shape of multiple children and bonded with epoxy resin etc. The outer surface of the object that has been hardened by sandwiching a weight-reduced object and containing air is coated and reinforced with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin at a thickness of 3.3 to 195 mm. A structure like a honeycomb structure, that is, a hexagonal hole or a round hole like a hexagonal hole in a honeycomb structure on a thing that has been hardened or laminated with paper such as corrugated cardboard and soaked with air and adhesive In order to make a plurality of cardboards with a space of 19.5 mm to 33 mm spaced apart from one side or circle of a hexagon. The surface of an object whose weight has been reduced by drilling a plurality of small holes such as hexagons or circles of about 1.95 mm to 33 mm or the like is reinforced with a foaming resin such as urethane foam or a plurality of small holes of paper. Metal or paper honeycomb structure with a foamed resin outer surface reinforced with a honeycomb structure with a plurality of holes spaced from 5 mm to 33 mm, that is, a hexagonal hole in the honeycomb structure replaced with a circular hole And then reinforced with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm, or a thickness of 0.195 to 3.3 mm. A paper cone with a square or rectangular side of about 1.95mm to 33mm. Paper that has been cut into a flake shape or shredded with shredders used in office work is mixed with air and stirred to wrap the crumpled air. The paper is soft and fluffy. After the fiber is loosened, about half this soft and fluffy paper fiber loosen object together with an adhesive such as epoxy resin is stirred and compressed appropriately and hardened to the required strength The material molded into this member is light and has a cavity inside, and the required strength can be obtained by adjusting the amount of adhesive. This paper is cut into a cone flake shape and mixed with air and agitated paper and adhesive. In order to reduce the weight after forming the compressed member into a mold, the side of the circle or hexagon has a side of about 1.95 to 33 millimeters. A plurality of holes are formed at intervals of 19.5 mm to 33 mm to make a thing similar to a honeycomb structure, that is, a hexagonal hole in the honeycomb structure is replaced with a circular hole. The honeycomb structure of resin, fiber reinforced resin, paper or metal is attached and wrapped, and then the surface is coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm. There is a method of using the hardened material as a member of the flying body, or a tape of film material such as paper or fiber or fiber reinforced resin is sandwiched between the tapes so that the seaweed roll sushi rolls in a cylindrical shape 1 to 3 atmospheres of pressure were compressed between the tape wound while being wound and the tape to be wound. Gas or gas encapsulated resin encapsulated pressure gas such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 to 33 mm and a thickness of 0.195 to 330 mm is a small crushed egg of several children Or a spherical or polyhedron of a size similar to that of a tennis ball or a volleyball and a chemical fiber or a natural fiber having a tensile force of a fiber shape diameter of about 0.195 microns to 3.3 millimeters Put together a cotton-like object, mix an appropriate amount of adhesive such as epoxy resin, soak in air and stir the gap between the resin-filled pressure gas and the cotton-like fibers. Use a fiber reinforced membrane tape or a commercially available product filled with an appropriate air-containing resin or other adhesive. A honeycomb structure layer made of paper, resin or metal is bonded to the outer surface of the object that is packed between the tape and tape and hardened with air, and is formed by adhering with an adhesive such as epoxy resin. Is used with a thickness of 3.3 to 195 mm coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin, or the structure of the flying object is paper, non-combustible paper, aramid paper or A honeycomb structure of resin or metal was formed into a required shape, and the outer surface of the honeycomb structure was coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm. There is a method of using an object as a member, or a compressed air or gas of 1 to 3 atm is filled with a diameter of 1.95 mm Resin spheres such as spherical or polyhedral polyethylene terephthalate with a thickness of 0.195 mm to 3.3 mm from rimeter are small crushed egg-like particles such as a number child, and the fiber shape has a diameter of 0.195. Resin by mixing chemical fiber or natural fiber with a pulling force of micron to 3.3 millimeters in size like cotton and mixing with an appropriate amount of adhesive such as epoxy resin and mixing with air. The gap between the products filled with the pressure gas made of cotton-like fibers and the resin or other adhesive material that contains moderately air is formed into the shape of the member, and the adhesive contains moderate air As a result of the consolidation, the adhesive has a shape like an elongated lump of the number of children littered with a white thin film that is an aggregate of the number of eggs. Before curing, it is put into a mold and formed into the shape of the required member, and the outer surface of the cured object containing air is wrapped in a honeycomb structure, and then the surface is 3.3 mm to 195 mm in thickness with a carbon fiber reinforced resin Alternatively, there is a method of using a material reinforced and coated with fiber reinforced resins such as glass fiber reinforced resin as a member, or a central member of a flying object is formed of foamed resins such as foamed polystyrene or foamed urethane, and paper is placed around the foamed resins. Alternatively, a honeycomb structure layer made of resin or metal is formed by bonding with an adhesive such as epoxy resin, and the outer surface of the honeycomb structure has a thickness of 3.3 mm to 195 mm and is made of carbon fiber reinforced resin or glass fiber reinforced resin. Material reinforced with fiber reinforced resins such as compressed air or gas compressed at 1 to 3 atmospheres Encapsulated resin spheres such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 330 millimeters can be as small as a small crushed egg or a tennis ball. Adhesion of a moderate amount of a sphere or polyhedron with a size of about volleyball and a cotton-like material made of chemical fibers or natural fibers with a strong tensile force of 0.195 microns to 3.3 millimeters in diameter. This outer surface is a mixture of agents mixed with air and stirred in a spherical or polyhedron gap filled with chemical fiber cotton and adhesive, which is then stirred in with air. A honeycomb structured layer made of paper, resin or metal is bonded around with an adhesive such as epoxy resin. The outer surface of the honeycomb structure is 3.3 mm to 195 mm in thickness and coated with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin, or a honeycomb structure made of paper, resin or metal alone. There is a method to use as a member of the flying body, the above is a description of a material in which the surface of a honeycomb structure made of wood, paper, resin, foam resin, etc. is reinforced with fiber reinforced resin, the above is a light and tough composite material From here on, there is a method of using the above-mentioned composite material as a member of a flying object, which is a description of the safety and structural strengthening of the flying object or aircraft. To prevent lightning strikes, a wire of piano wire with a diameter of 1.95 to 33 mm or steel wire for prestressed concrete is buried. After pre-tensioning, the fiber resin is cured, and the stress is controlled with a computer using a strain gauge or the like on a steel wire for piano wire or prestressed concrete. This method suppresses the aircraft from expanding in the sky by competing with the force that suppresses the pretension bulge that is the pre-tensioning force of the ano wire or prestressed concrete steel wire rod. Or the aircraft structure crashes into the ground and the aircraft's fuselage breaks apart, preventing the piano wire or the steel wire mesh for prestressed concrete from breaking, ensuring a passenger's living space in the event of a crash. Or steel, aluminum, stainless steel, or titanium Or, there is a method using a member made by rolling forging or extrusion of metals such as ultra-lightweight high-performance general-purpose magnesium alloy or using a member manufactured by molten metal lamination forging fixation technology. There is a method using a framework structure of a three-dimensional honeycomb structure such as a wire-ferran structure with a metal such as steel using a molten metal laminate forging fixation technique, which is a description of As in the laminating technology of the above, using a ceramic formwork, the molten metal to be laminated with a mesh shape of about 0.195 mm to 33 mm in height for each layer, etc. The molten metal into which the molten metal to be poured can be extruded and melted by electricity The bottom surface of the ceramic mold that can maintain a high temperature below the point is a mesh with a cross-section of the honeycomb structure that is cut horizontally A chute that drops a layer of molten metal onto the production base horizontally using a ceramic mold with a hopper-shaped ceramic mold with a nozzle-shaped mold. A small amount of metal such as molten steel is poured into the ceramic mold by increasing the pressure of the inert gas and injecting a single layer of the molten metal. The metal, such as drawn molten steel, cools and hardens and adjusts to the degree of striking that the mesh shape is a little thicker for the layered mesh-shaped steel drawn on the production base according to the mesh shape of the ceramic mold The machine-driven computer controlled hammer is forged while maintaining the three-dimensional shape of the mesh to be laminated, but the thickness of the laminate is forged. Assuming that the thickness is corrected to be slightly thicker, a plurality of grooves having a thickness and depth of about 3.3 nanometers to 0.195 millimeters are formed on the upper surface of the forged metal using laser technology. The square side of the cut-off board is 3.3 nanometers to 1.95 millimeters, and the surface of the sea urchin has a diameter of 3.3 nanometers to 1.95 millimeters. 3.3 to 1.95 millimeters from 3.3 nanometers to 1.95 millimeters at intervals of 3.3 nanometers to 1.95 millimeters, and then the laser-processed and drawn ceramic molds give high frequency vibrations. After cleaning the remaining metal residue, the ceramic mold is lowered onto the forged mesh-shaped metal layer, a small amount of molten metal is poured, and press-in injection is performed with an inert gas. After forging by the above method, the tip of a plurality of elongate barbs laser-processed to the above dimensions is poured into the metal in the shape of a grid, and the next part of the barbs is melted by the heat of the molten metal. By biting into and adhering to one layer, a bond between the previous layer and the next layer is formed and fixed.













The upper layer is forged with a machine-driven computer-controlled hammer that adjusts the degree of striking, and the surface is forged with laser technology on the surface. Forged steel such as Weir Ferran structure made of metal such as steel forged by repeating this series of operations to improve the bite with the next molten metal and changing multiple ceramic molds A three-dimensional honeycomb structure made of metal can be obtained, and the conventional lamination technology eliminates the problem that the laminated part peels off like bamboo fiber, eliminating the biting, sticking and forging by sea urchin spines on the laminated surface The method of replacing multiple ceramic molds according to the type of each layer to be laminated in a three-dimensional honeycomb structure is to laminate one unit of the basic structure shape of the honeycomb structure. A plurality of ceramic molds as many as the number of cut planes horizontally cut are connected continuously horizontally to form a strip, and the ceramic molds are moved vertically, front, back, left, right, left and right, and ceramic. After the mold is moved, the molten metal to be laminated is poured onto the substrate, the ceramic mold is lifted, the ceramic mold is cleaned by the vibration of the ceramic mold, and the laminated metal surface is forged. Laser cutting spine processing can be used to automate a series of flow processes by shifting the molding form up, down, front, back, left, and right, or the steel sheet laminating laser melt forging laminating technology can be used for steel meshes like 3D printers. This is a method in which forged formation is performed after laminating the laminated surface using laser technology after laminating metal sheets to be laminated, such as shapes, and so on. The ideal 3D honeycomb structure to be formed is placed virtually, and the virtual 3D honeycomb structure is cut by a horizontal plane in the first stage. A virtual three-dimensional honeycomb structure in the horizontal plane of the second stage is cut horizontally on the first stage, where a sheet of metal such as steel having a thickness of .95 microns to 33 mm is placed on the production base. This is the second stage in which a sheet of metal such as steel having a mesh shape is formed by punching and shearing a sheet of metal such as steel with a thickness of about 1.95 microns to 33 mm in a cross-sectional shape with a punching shear. Along with the mesh shape of the second sheet, the center of the mesh is melted by laser technology and the upper and lower sheets are melted and fixed, and then cooled to an appropriate temperature. It is assumed that the laminated sheet to be forged while hitting with a machine-driven computer-controlled hammer with an appropriate hitting state on a metal sheet such as steel, which has been struck, has been corrected to be thicker on the assumption that it will be forged. On this second stage, punching shears are used to punch a metal sheet, such as steel, with a thickness of about 1.95 microns to 33 millimeters in the shape of a cross section obtained by horizontally cutting a virtual three-dimensional honeycomb structure on the horizontal plane of the third stage. The upper and lower sheets are melted at the center of the mesh by laser technology along the shape of the mesh of this third stage sheet, which is a third stage by placing a sheet of steel or other metal that has been punched and sheared. 3D shape is maintained by hitting the mesh of a metal sheet such as steel that has been melted and fixed and then cooled to an appropriate temperature with a machine-driven computer controlled hammer with an appropriate level of striking. By repeating this forging operation, a series of flow operations that can replace a metal sheet layer while forging a virtual three-dimensional structure can be automated. Three-dimensional honeycomb structures such as Weir Ferran structure, forged with various metals, can be applied to aircraft or large passenger aircraft frame members, etc. This is a description of aircraft design methods and aircraft technology As a design philosophy of an aircraft, the inner skeleton of a passenger aircraft etc. has a lot of cavities inside like a bird skeleton, and the outer shell of the passenger aircraft must be strong to some extent lightweight The passenger aircraft that must be strong crashed with the ground When a skeleton of a three-dimensional honeycomb structure such as a wire-ferran structure in which a metal such as steel that has been laminated and forged inside is forged, is deformed. The framework of the three-dimensional honeycomb structure such as Weir Ferran structure that absorbs and absorbs some energy is processed into a sandwich belt member, and heat insulating materials and fiber reinforced resins are placed outside the framework like an aircraft cage and toward the inside of the framework The belt where the skeleton of the aircraft forming the outer wall of the aircraft while being laminated is knitted The intersection of the belt and belt is cured and fixed using epoxy resin etc. when the aircraft is completed At the time of first knitting into the shape of an aircraft, it is an industrial gel material or honeynite (registered trademark) or foam on the outside of the skeleton of an aircraft-like belt member that is entirely made of straw. Diameter of 1.95 in which compressed air or gas of 1 to 3 atmospheres is sealed with urethane or a resin ball that can withstand changes in atmospheric pressure above and above the ground. A product filled with pressure gas made of resin such as spherical or polyhedral polyethylene terephthalate with a thickness of 0.195 mm to 330 mm is about the size of a small crushed egg or a tennis ball. A ball or polyhedron with a size of from about volleyball to a polyhedron and a cotton or other chemical fiber or natural fiber with a pulling force of about 0.195 microns to 3.3 millimeters in diameter. Mix an appropriate amount of an adhesive such as epoxy resin, mix it with air, and stir it. The gap between the resin-filled pressure gas will be filled with cotton-like fibers and an adhesive such as resin containing appropriate air. When a resin ball that uses a material filled with shock absorber as a shock absorber crashes due to a collision with the ground, it may break A shock-absorbing material that absorbs more energy is attached to the outside, and the outer wall of the fiber-resin is the outer wall of the shock-absorbing material. This skeleton belt that protects the safety of passengers is a collective steel manufactured by a method in which metal wires such as piano wires or prestressed concrete steel wires are bundled in parallel like the muscle fibers of the outside There is a method of knitting like a hand-knitted sweater with wire rod or wire rod, and the inside of the metal honeycomb structure and the fiber reinforced resin honeycomb structure that are used separately according to the application are like the hard part and the soft part of the turtle shell A stretch of belt that is a bamboo-like skeleton that weaves a strong and strong belt member arranged in a balanced manner. There is a method in which the wires are bundled in parallel, and there is a method in which the wire is knitted like a hand-knitted sweater. There is a method of wrapping the wire so that the rheology body does not leak with the mantle film.There is a method of replacing the fatigue fracture of the wire with a fiber reinforced resin, that is, a wire such as steel bundled in a bundle This is a method in which a wire knitted like a hand-knitted sweater is housed in a fiber reinforced resin. The honeycomb structure in which the honeycomb material is used for the inner part of the belt that receives compressive force with the braided wire rod surrounds the section of the metal honeycomb structure The honeycomb structure of the resin surrounds the turtle shell, and I want to see the turtle shell here.A soft growth layer surrounds the hard hexagonal shell around the turtle-shaped hard hexagon shell and the honeycomb structure The combination of this rigid and flexible honeycomb structure allows the belt member to bend slightly but flexibly and, like an H-shaped steel, the mantle can withstand alternating stresses of compression and tension Inside, the rheology body and steel wire material, then the fiber reinforced resin base material, then the rigid and soft honeycomb structure, then the fiber reinforced resin base material, then the steel wire material and rheology body are encased in the mantle. The belt member becomes a more mechanically advantageous and easy-to-use material by the method in which the honeycomb structure is sandwiched with a wire material such as steel from both sides. The rheological body of a sandwich belt member, which will be referred to as a Dutch belt member, has a method of replacing it with a fiber reinforced resin. When describing a belt member in the claims, it mainly refers to a sandwich belt member. The skeleton of an aircraft made of bamboo fences is created Inside the fence is a wide cavity, especially the fuselage, both wings and tail are all like mechanical aircraft made of bamboo fences as a mechanical structure The stiffening knitting method that connects the fuselage, both main wings, fuselage, and tail wings is woven so that the stress is distributed in a distributed manner and the fatigue of repeated loads is withstood, as if looking at a delicate bamboo craft. This method, which is designed to balance the entire aircraft, is like paper on a bamboo skeleton like a Nebuta Festival float A special fiber reinforced resin is encased in the outermost fiber reinforced resin, and a piano wire or prestressed steel wire is pre-tensioned (a technology that pre-tensions the steel wire and then hardens the fiber reinforced resin). The outermost skin is made of fiber reinforced resin with a mesh of piano wire or prestressed steel wire in the center so that it does not break into fine dust at the end of a crash. As described for safety, the fiber reinforced resin sandwich structure with the shock absorber sandwiched around the heel skeleton, so the energy of the collision is the order of the fiber reinforced resin outer wall shock absorber 籠 shape skeleton shock absorber fiber reinforced resin inner wall However, the conventional aircraft has a rigid skeleton and a brittle outer skin to reduce the weight of the aircraft. The method of the present invention is a design method that goes from the center to the outside, but the design method of the conventional aircraft that wraps passengers from the outside in terms of structural dynamics from the outside to the inside absolutely respects human life rather than the economy As an application of the sandwich belt member, the sandwich belt member 籠 exoskeleton spherical flying object is composed of a spherical passenger part with a head part, both wings and tail part, and is about the size of a jumbo jet (registered trademark) The wide space inside the spherical shape is used for multiple purposes, and it is possible to construct a plurality of floors by supporting the honeycomb structure floor with the ridge-shaped walls and floors. As an application of a sandwich belt member that is used for multiple purposes, a flying object that simulates a thick flying fish simulates a large flying fish with a skeleton-like exoskeleton. The flying object has a rounded body like a goldfish and the thick wings are structured like the cross section of the wing according to Bernoulli's theorem, and the upper and lower air pressure difference creates lift In the tail of this squadron, the forced air-cooled whole heat radiating fiber reinforced resin metal composite internal combustion engine is used to obtain the rotational force to generate the forced air cooled whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor Forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite rotor permanent magnet stator Electric coil disk laminating generator is used to obtain power, and then the bird strike prevention device fiber-reinforced resin metal composite turbine laminating electric motor A flying object simulating a thick flying fish can be moved forward by sending the wind backward with a forced air cooling whole heat radiation fiber reinforced resin metal composite Combined internal combustion engine angular momentum adjustable flywheel torque converter clutch forced air cooling overall heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacked generator motor output power transmission integrated hybrid device A large internal space that can be managed by a computer is partitioned by a wall-shaped wall, floor, or honeycomb structure knitted with a sandwich belt member and can be used for multiple purposes. Bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor attached to both wing tip, horizontal tail tip and fuselage tail of flying object is an application of sandwich belt member that can obtain strong driving force. The center of the sphere is a sphere and the outer periphery of the sphere is a disk shape. Tophan internal-combustor generator combined disk outer periphery part wing shape Koba Sora dance fall fall mitigation parachute installation fuel generator ballast hanging dropable flight object is the outer periphery of the disk part where the exoskeleton of the flying object is knitted by the sandwich belt member The parts are blown down by multiple duct engines and floated













In order to obtain buoyancy, the disk part is expanded left and right, and multiple ducts and engines can be arranged radially on the concentric circles of the disk. The part where the wind hits the traveling direction of the disk is processed into a wing shape The engine has a cross-shaped beam in the middle of the cylindrical height, two rotary engines above and below the center of the cross, or two zero-type fighter aircraft Sakae engine twin-engine horizontal piston simulated forced air cooling overall heat dissipation Engine exhaust in which two propellers or fans fixed on the shaft of each internal combustion engine that fixes the fiber reinforced resin-metal composite internal combustion engine at the center of the cross beam are duct fans that rotate inside a cylindrical shape Between the upper and lower internal combustion engines in the cylindrical duct of the disk, which is taken into the silencer in the disk and purified through a ceramic filter and exhausted from the lower surface of the disk Air-cooled overall heat-dissipating fiber reinforced resin metal composite rotor permanent magnet stator Electric coil disk stacked generator is installed to obtain power at the same time as buoyancy There is a method of propelling in the traveling direction with that power Because of the levitation force, a long runway is not required, and four bird strike prevention devices fixed on the boundary between the spherical surface and the disk with respect to the direction of travel of the sphere. The left and right and up and down posture control is performed by the difference in the four outputs of the four motors in the forward direction that feed forward, and the rough vertical change is controlled by the difference in the output of the duct engine. There is also a method of extending both wings to the left and right, and it is possible to attach aileron to the wings and control the pitch This is like a big ray flying in the air Four bird strike prevention devices that obtain buoyancy with the duct engine described in the claims of the present invention Fiber reinforced resin metal composite turbine laminated electric motor with forced air cooling Whole heat radiating fiber reinforced resin metal composite internal combustion engine Adjustable angular momentum Spiral wheel torque converter clutch forced air cooling overall heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk laminated generator motor output power transmission transmission integrated hybrid device combined with a spherical center circumferential disk to obtain propulsion Four bird strike prevention device fiber reinforced resin metal that stabilizes flight by extending the tail sharply from the disk like ray, which also includes ray simulated flying object simulating deformed ray shape Obtain the buoyancy of the blades as the forward speed is obtained by sending the wind backward with the composite turbine stacked electric motor The vertical duct of the disk is configured to reduce the burden on the duct fan by forced air cooling overall heat radiation fiber reinforced resin metal composite Internal combustion engine angular momentum adjustable adjustable wheel torque converter clutch forced air cooling overall heat radiation fiber reinforced resin metal composite Rotor Permanent Magnet Stator Electric Coil Disc Stacked Generator Motor Output Power Transmission Transmission Integrated Hybrid Device The energy can be comprehensively managed by the computer. This parachute with multiple chutes is opened when it falls, and when it falls it pulls the mouth of the upper part of the parachute with a wire to induce the fall of the spherical disk, so that the ground and the leaves fall down in the air Ballast ballast with heavy objects such as generator fuel tank at the bottom of the spherical shape to ease the clash It has a structure that can be hung up and down like a tank and can be put in and out, and when the airflow is bad, hang down the heavy parts such as the generator and fuel of the ballast and lower the center of gravity to prevent the whole disk from rotating to the top This ballast part has a structure that can be dropped separately from the spherical disk body in a safe position to reduce the weight in the event of falling, and the bottom part around this suspendable ball is cut off The lower part of the sphere is provided with a shock absorbing layer, and the inside of the sphere, which reduces the impact when falling, is partitioned by a wall or floor made of sandwich belt members or a honeycomb structure plate. Fuel that is used for multiple purposes safely and comfortably, and has a structure that can transport about 900 people in a single flight without crashing the aircraft by crashing into the ground in the event of a crash Or, light oil or gasoline can be used, and exhaust gas passes through a muffler with built-in catalyst, so if it falls on the sea to mitigate calm air pollution, a float like an air bag will swell from the bottom of the disk part, but this spherical disk is originally Is a watertight and airtight structure that floats on the water, and in the event of a crash, it swells like an air bag and softens the impact of the crash. Above is the description of aircraft design method and aircraft technology, which is functionally the same as above. From now on, it is a description of lamination technology. Draw a figure using the fine wire of the metal and charge the metal thin wire as an electrode. The crucible lid in the shape of a crucible flask is brought into close contact with a stopped ordinary crucible to prevent the entire vapor deposition material from diffusing. The electrode for charging the vapor deposition material in the crucible is the melting surface inside the crucible or inside the crucible. The nozzle is formed into a target figure with a different potential so that vapor deposition does not occur in the nozzle having the same potential of the vapor deposition material through the conduit having the reverse potential of the vapor deposition material through the conduit having the reverse potential of the vapor deposition material. There is a method to drift the nozzle from the movable conduit by the diffusing force to evaporate and the electrostatic transport to reach the target electrode from the nozzle by moving the crucible flask shape crucible like a three-dimensional printer and the third shape of the crane neck flask shape Like the original printer, it is selectively and intensively lowered from the nozzle-shaped vapor deposition material outlet at the tip of the crane neck so that it does not scatter to other parts. Vapor deposition is controlled according to the shape of the electrode of the thin wire that is charged by concentrating and depositing the vapor deposition material, which is managed by a device such as a camera shutter, on the target fine wire at the top by electrostatic force The three-dimensional shape is formed by the vacuum deposition material or the method of using conductive ink instead of the target thin line is to draw the deposition target figure like a three-dimensional printer and charge the figure to the figure. By vacuum-depositing in a manner and drawing a figure to be laminated like a three-dimensional printer on the target figure so as to laminate further, charging the figure and intensively vacuum-depositing from the top on the top figure to repeat this process Laminated three-dimensional structures can be formed by vacuum-deposited materials, or the method using silver clay technology for three-dimensional lamination can be applied to paper or resin fiber nonwoven paper. Or use a water-soluble air contact curable curing agent and a fine powder of metal that you want to laminate with an ink that contains a mixture of fine powders, or a figure that you want to laminate on a non-woven paper that is placed on a production base. Like the original printer, draw another piece of paper on the figure you want to layer and draw like a three-dimensional printer. The curable ink containing fine metal powder penetrates between the fibers of the paper. Adjust the amount of ink to the extent that the ink on the upper paper and the lower paper are compatible, and draw a figure with a printer like a three-dimensional printer Curability containing metal fine powder you want to stack paper on this paper Drawing a figure with the ink of the above is repeated to obtain a paper or resin fiber non-woven paper which is laminated and cured to burn the paper or resin fiber non-woven paper in a sintering furnace to sinter bond the metal to form a three-dimensional structure Obtain paper or resin fiber The purpose of using non-woven paper is to shorten the lamination time, ensure the width of the ink, and smooth the surface of the method of three-dimensional lamination, and print multiple spot-like dots at fixed positions around the figure to be laminated When the paper bundle is cured, the point cloud is stacked and cured in a columnar shape until the laminated paper bundle is sintered and the shape is protected and the cured paper bundle is easily transported. Assuming that the three-dimensional structure shrinks, the size will be corrected and the laminated figure will be drawn. The above is the description of the new three-dimensional lamination technology, and here is the description of the structure of the flying object Certain aircraft structures are made of resin, carbon fiber reinforced resin, glass fiber reinforced resin, fiber reinforced resin such as Kevlar fiber reinforced resin, or a combination of these metals, resin or fiber reinforced resin materials. Or use Use a layer of metal and resin layers layered together with a layer of xy-resin, or use a combination of fiber materials such as aramid fibers, or use a fiber material in a belt shape. Use a braided material hardened with resin as a member for knitting the heel structure, or use a material that is extruded and sealed with metal or a resin that is press-fitted and sealed inside a material that gathers thin metal pipes Or use a honeycomb sandwich structure in which both sides of the honeycomb structure plate are sandwiched between plate materials such as fiber reinforced resin and bonded with an epoxy resin, or a honeycomb structure / plate material / honeycomb structure / plate material Carbon fiber reinforced resin or glass fiber reinforced resin is used for the outer surface of three-dimensionally machined products that are alternately stacked in layers using a milling machine. There is a method of using as a member a material reinforced by covering and reinforcing with a fiber reinforcing resin with a thickness of 3.3 to 195 mm, or a weir ferran structure that forms a weir ferran structure like a panel is a honeycomb structure There is a method to form a panel shape using a weir ferran structure which is a three-dimensional structure by bonding polygonal members that are the basic structural structure of epoxy resin, and using a fiber reinforced resin plate Thickness 3 on the outer surface of a sandwiched structure or an object obtained by three-dimensionally cutting a structure in which these layers are alternately laminated with a milling machine or the like with a fiber reinforced resin such as a carbon fiber reinforced resin or a glass fiber reinforced resin. There is a method of using a material which is hardened by covering and reinforcing at 3 to 195 mm as a member. Shaped members are assembled according to the flow of stress in the cross section and bundled together with an epoxy resin between the pipes to prevent stress concentration. A flexible and highly viscous mucous layer that absorbs the energy of possible fatigue rupture is provided with a rheological layer such as a muscle-tendon relationship. Stress by providing a rheological layer, such as a muscle-tendon relationship with flexible and highly viscous mucous properties, that absorbs the energy of fatigue breakage in the gap between the laminate and the non-compressed membrane assembly rather than the compression material A three-dimensional honeycomb structure that spreads the concentration in each part of the assembly to prevent the progress of fatigue fracture and has a mechanical balance, or a combination of these layered hierarchical structures and a three-dimensional aggregate structure. This composite structure can also be used for aircraft, using a composite structure or a layered structure object that is bonded with an epoxy resin using a three-dimensional aggregate structure object that prevents fatigue failure in the compression part. Passengers when a vehicle or aircraft crashes into the ground by providing a layer of rubber shock absorbers, or 195 to 330 millimeters in thickness, between 1.95 and 3.3 millimeters thick, between these composite structural walls. The shock absorbers sandwiched between the wall and the center of the wall that secure the passenger's living space by reducing the impact energy to the inside enclose air like a balance ball, rubber, resin, Kevlar fiber, silk, cotton fiber, chemical Shock absorbers are made using fibers or a combination of these. The above is a description of the structure of the aircraft. Or, the description of the aircraft safety and structural strengthening, the personal aerial work flying object is composed of the upper flying body and the lower suspension body, the upper part corresponding to the fluff (crown) part of the dandelion as its configuration form The flying object uses a method of using an electric motor, a method of using an internal combustion engine, a method of using a balloon, a balloon and an electric motor, or an internal combustion engine, or an electric motor, an internal combustion engine, a generator, and a balloon to obtain a lifting force. The description of the composite device divided into the composite device method is as follows. The balloon is divided into the hot air balloon, gas balloon or hot gas combined balloon method. This hot gas technology used in the following ice cream cone-type aircraft, including the method of enclosed sealed hot gas balloons that are used by heating The method of using an electric motor for the upper aircraft, which is also used for airships, is a gyro that stabilizes the upper aircraft, a parachute that can be used manually or automatically for emergency methods, and a blower to obtain lifting force in the upper aircraft. From here, the propeller or fan

The blower that is the description of the manufacturing method is a propeller or fan that is made by processing solid wood according to the description of the above composite material and cutting or pouring resin into the mold, titanium, aluminum, stainless steel, ultra-light, high-performance, general-purpose It consists of a metal such as magnesium alloy or carbon fiber reinforced resin or a material that is a combination of these materials. The method of compounding the materials here is propellers or fans that are perpendicular to the blade rotation direction, that is, from the shaft to the outer periphery. In the direction along the flow of the stress in the cross section in the radial direction, hollow pipe materials with a diameter of 0.195 mm to 3.3 mm are collectively arranged and the epoxy resin or the like is solidified by cutting such as a milling machine or laser technology , Scanning Electron Microscope Technology, Tunneling Effect and Atomic Implantation Using a molecular manipulator that combines a chipping technique, a molecular insulator and a molecular beam, or a nano-robot such as a ribosome that automatically transports and manufactures molecules, the molecules are assembled and arranged in three dimensions according to the molecular structure design method. The three-dimensional printer atomic layering technology at the level (can be used for room temperature superconducting material manufacturing, especially ceramics), using the technology to construct the molecule itself, a three-dimensionally formed in the shape of a propeller or fan blade, the inside of the pipe is hollow Another composite method that is tough because it is a collection of thin pipe materials with a light weight and at the same time a concordant (arrangement of suitable materials according to mechanical characteristics) along the flow of stress Laminate paper, resin, and metal honeycomb structures and use a milling machine or other cutting machine to stand in the shape of a propeller or fan blade. The outer surface is formed with a thickness of 3.3 to 195 mm and coated with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin, and another composite method is that the fiber material is subjected to stress in the radial direction. The propellant or fan shape is formed in the direction along the flow and then the resin is poured between the fibers and hardened. The lifting device of the upper flying body is strong against rotation. The above is the manufacturing method of the propeller or fan, which is composed of the motor, and here is the description of the light and powerful electric coil and the forced air blowing overall heat dissipation, there is a method that uses a commercially available electric motor, but a new fiber Reinforced resin electric motors use copper, gold, or room temperature superconducting materials such as conductive wire enamel, glass fiber reinforced resin, or conductive surfaces. A superconductor that prevents melting by heat through a wire coating material such as an Mick-processed method or a glass-finished product, or a pipe whose center is the shape of the wire, and the inside of the wire of the wire is forcibly air-cooled or water-cooled, or liquid helium or liquid nitrogen Conductive coils, steel, aluminum, titanium, ultra-light, high-performance, general-purpose magnesium alloy, or other metals, or carbon fiber reinforced resin, or combinations of these, the electromagnetic part of the electric motor can be made of metal and carbon fiber. The method of forced air cooling, in which a blade forcibly air-cooling with a small blade that forcibly blows air to the coil of a lightweight and strong electric motor in which the structural material is replaced with a fiber reinforced resin, is built directly into the electric motor and the coil is forcibly air-cooled. Method of forced air cooling from the inside of the pipe of the electrical lead The fiber reinforced resin that forms the structure of the electric motor has a plurality of small holes with a diameter of 0.195mm to 3.3mm, and heat radiation is released by releasing hot air from the entire electric motor. The upper flying object is arranged in a hierarchical manner with a plurality of brushes made of a composite material considered, or a plurality of brushless electric motors, or a plurality of electric motors combining these brushing motors and brushless motors. The above is a description of the lightweight and powerful electric coil and the forced ventilation overall heat dissipation. The upper air blower is a fan motor integrated type with a fan and motor integrated, or the air blowing direction of the air blower or air blower is upward And the exhaust also includes the method of the duct fan that is adjusted downward or the fan is in the duct, And the lower suspension body corresponding to the seed of dandelion is constructed so that humans can freely work in the air, such as carrying humans or hanging up and allowing them to work in the air. The upper flying body is divided into a method of stacking honeycomb structures such as a honeycomb sandwich panel or a weir-ferran structure panel, a method of collecting cocoon-shaped objects, or a method of combining pipe structures, honeycomb structures and cocoon structures. The method of using a pipe structure to form a framework as a structure is based on a method of assembling and fixing a pipe member and fixing with a fixture and fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin. There is a method that is integrally formed by autoclave formation, etc. that is baked under pressure in a large kiln at a factory. There is a method of forming the outer shape of the upper flying body by keeping the outer shape in the range of width and depth of about 195 to 3300 mm and height of about 195 to 3300 mm, and the inside with a hollow or a framework. The appearance shape of the upper flying object is a sphere or donut shape, that is, an annular surface, an annular body, a spheroid, a spheroid, a rotation quadratic curve, a rectangular parallelepiped, a cube, a polyhedron, a polygonal column or a cylinder of this size, or A shape in which a plurality of cylinders are connected horizontally, a cone shape, a method of using a truncated cone or a quadrangular pyramid alone, and a combination of these three-dimensional shapes, and a cone shape with the top apex of the cone shaped downward, Or on the upper and lower surfaces of a cylinder that looks like a sharp pencil A shape with a conical bottom connected, or a shape with a conical bottom connected to the lower surface of a cylinder shaped like the bottom end of a short pencil, or the larger bottom of a truncated cone like a large abacus ball A method of forming a solid with the shape of each other and using it alone, or a method of using this large abacus ball connected vertically, or connecting spheres vertically, or connecting a sphere or spheroid to a large grape bunch Or the shape of the aggregate using a combination of a cylinder and a conical solid and a sphere or spheroid, the upper aircraft is a method of assembling pipes, The framework of the horizontal member, the vertical member, the propeller or the fan guard member is a metal wire such as stainless steel wire or piano wire or The member is wound around the joint part from 3 to 33 times with a wire material of 0.195 mm to 3.3 mm in diameter, such as fat, chemical fiber, or carbon fiber reinforced resin, and is knotted from above the knotted wire. Fixtures that have a method of bonding with epoxy resin or bonding with epoxy resins, rigid bonding by welding between resins or metals, or fixing with aluminum screws or fixing tools are steel clips, resins or carbon fibers This is an assembled method combining reinforced resin and glass fiber reinforced resin. This is a method for aerial work or flight leisure by fixing a detachable member to a rigidly connected member with a detachable fixture that facilitates disassembly. The horizontal member of the upper flying object can be assembled quickly and easily and easily for personal aerial work flying objects on site. It is divided into a horizontal member, a horizontal member for attachment and detachment, and a horizontal member for propeller or fan guard, the vertical member is divided into a central vertical member and a peripheral vertical member, and the upper aircraft is detachable to fix the electric motor so that it can be assembled and disassembled The horizontal member is rigidly connected to the vertical member by passing the removable horizontal pipe through the pipe so that the central vertical member is in the middle of the horizontal member. Fixing the horizontal member and the detachable horizontal member and then fixing the electric motor to both ends of the detachable horizontal member, or fixing the electric motor first to one end of the detachable horizontal member and then fixing the electric motor Two detachable horizontal members which are inserted into the center of the central vertical member and fixed with a fixing tool inside the rigid horizontal member having an end different from the end of the detachable horizontal member rigidly connected to the vertical member. The There is a method of butting at the center of the center vertical member or a method of inserting a removable horizontal member with an electric motor fixed into the rigid horizontal member of the central vertical member like a cantilever, or for attaching and detaching to fix the electric motor The horizontal member is divided into two methods: a method using a pipe member alone, or a method for assembling a detachable horizontal member supporting an electric motor into an annular structure, that is, a method using a detachable horizontal member alone or an annular structure. The shape of the horizontal members stacked in multiple layers, as seen from above, is the cross shape of the same side, the star shape of David (hexagram), the pentagram or the ten-valve, the twelve-valve, the ten-valve. A polygon and a diagonal line with different shapes and sizes are combined inside a polygon that combines a triangle and a diagonal line inside a polygon such as a six-valve, thirty-two valve chrysanthemum pattern, or an octagon. There are methods that have the shape of eyes or squares, these shapes can be disassembled and assembled, and these various structures can be shifted by shifting the horizontal position or shifting the vertical position from aerodynamic considerations. Combined so that fans do not contact each other and stacked in layers so as to be stacked in the vertical direction, a horizontal member with the same side as a horizontal member, or a polygon that combines triangles and diagonal lines inside a polygon such as an octagon Due to the interference of winds aerodynamically blown horizontally and vertically so that multiple propellers or fans do not hit each other on a horizontal member with a combination of polygons and diagonal lines inside Considering the thrust of rising and the stability balance of the flying object, the flow is arranged while slightly shifting the position in the horizontal and vertical directions. The part flying body is structured to increase the thrust in the upward direction by laminating horizontal members of this equilateral cross shape or a combination of polygons and diagonal lines inside the polygon, the vertical member is the central vertical member And the peripheral vertical member and the fixture described in the claims, the central horizontal member is rigidly connected to the pipe of the horizontal member for rigid connection by screwing, welding, adhesion with epoxy resin, etc. The connecting part is reinforced by a plate member or rib member. The shape of the central vertical member is a prism or cylinder, or a three-dimensional girder structure that combines a horizontal member and a vertical member, or a rectangular pyramid that is elongated like a steel tower by combining a horizontal member and a vertical member. There is a method in which horizontal members of branches grow or a combination of these shapes in the circular structure of the ring, and the method in which the central vertical member is a prism is the cross section of the central member in the Kanji mouth or rice field Aluminum having a side of 33 to 66 millimeters in the vertical direction and having a length of about 195 to 3300 millimeters, carbon fiber reinforced resin, glass fiber reinforced resin, resins, foamed resins, or these materials There is a method of using an equilateral square pipe that is a single piece or a combination of materials, and the meaning of combining this material is to pour urethane foam or carbon fiber reinforced resin into the mouth of the Chinese character of the aluminum pipe or the hollow part of the cross section of the rice field The method of the central member of the cylinder, including the method of curing in the above, is a waterproof paper or paper tape having a diameter of 66 mm to 99 mm, a thickness of 1 mm to 6 mm, and a length of 195 mm to 3300 mm. Cylindrical shape The cylinder is made of a single material or a combination of a single material or a combination of a wound material, a composite material wound with the above membrane material, or aluminum, or a carbon fiber reinforced resin, a glass fiber reinforced resin, or a material made of the composite material. The meaning of combining vertically means to include a method of pouring foamed resin or carbon fiber reinforced resin into the hollow part of an aluminum cylindrical pipe and curing it, and drilling holes on the sides of these prisms or cylinders, vertical members Insert the pipes of the horizontal members for rigid connection into prisms or cylinders in order from the east, west, south, north, or eight directions so that the branch is perpendicular to the central member. A member made of wire with a diameter of 0.195 to 3.3 mm, such as metal, resin, chemical fiber or carbon fiber reinforced resin An upper flying object that is wound around the joint part 3 to 33 times around the joint part, and is rigidly joined with an epoxy resin from the top of the wire part, or screwed, welded or bonded with epoxy resins. From the top to the bottom of the tree
The shape of the character rack












Cylindrical center vertical material is a structure in which polygons and diagonal shapes combined in a polygon are stacked in multiple stages. The horizontal member and center vertical member for rigid connection are made of metal or resin. The material is wrapped with the wire material of 0.195mm to 3.3mm in diameter, such as chemical fiber and carbon fiber reinforced resin, around the joint part 3 to 33 times. The solid vertical girder center vertical member method is made of aluminum, which is rigidly fixed with a resin-solidified object or aluminum welded or epoxy resin or aluminum screw to rigidly fix the horizontal member and vertical member for rigid connection. Using carbon fiber reinforced resin, glass fiber reinforced resin, or a combination of these, a square cross section with a side of about 10 mm and a thickness of 1.5 mm. The center part of the horizontal member for rigid connection is sandwiched with four equilateral square pipes with a length of about 195mm to 3300mm in the vertical direction so that it has a cross-girder structure, and is rigidly connected with screws, welding, epoxy resin bonding, or fixtures. The vertical center member and the horizontal member are rigidly assembled and rigidly assembled so as to form a three-dimensional cross girder, and a horizontal member for detachment is inserted into the rigid horizontal member pipe and fixed with a fixture to constitute the upper flying body In order to facilitate the assembly and disassembly of the upper flying body, the horizontal member for rigid connection has a socket structure for inserting the horizontal member for fixing the electric motor. The method of inserting the horizontal member for use and the method of attaching the ends of the horizontal member for attachment / detachment at the center of the center vertical member and the end of the attachment / detachment horizontal member of the center vertical member as in the case of a cantilever It is divided into three methods that can be stopped by the heart. The method of the ring structure with a vertical center member that is elongated like a steel tower is stiffened at the center so that the compression member does not buckle like the steel ring structure. In order to obtain a propulsive force for ascending inside the upper aircraft, a plurality of propellers or fans of about 16 to 36 and a plurality of Electric motors are arranged in multiple stages. This arrangement method uses aluminum screws or the like to fix the electric motor base to the base of the detachable horizontal member. The electric motor and prober are targeted at each position of the horizontal member. The multiple propellers or fans inside the upper flying object are balanced by reversing the rotation direction of each propeller or fan at the target position, and the individual aerial work flying object is in the air The upper flying machine's horizontal members are 15mm to 30mm wide, 15 to 30mm high and 1.5mm thick From 3.3mm to 195mm to 3300mm in length, made of aluminum, carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin pipe, or a combination of these. The horizontal member and vertical member are rigidly connected while strengthening the necessary parts by welding the aluminum member, aluminum stiffening plate welding of the horizontal member and vertical member, and aluminum rib reinforcement welding. , Carbon fiber wire or netting, carbon fiber tape, carbon fiber reinforced A propeller or fan guard that is reinforced with a resin, glass fiber reinforced resin, or Kevlar fiber reinforced resin, and a detachable propeller or fan guard member is inserted into the tip of a detachable horizontal member to which an electric motor is fixed. The material of the member is resin or carbon fiber reinforced resin, glass fiber reinforced resin, chemical fiber, Tegs, stainless steel wire, wire or a combination of these, this propeller or fan guard member is a flying object for personal aerial work The propeller or fan guard member prevents the damage of the propeller or fan when it comes into contact with other objects. The pipe also includes a fan motor or blower method in which a duct fan and motor are integrated into a cylindrical duct. The structure of inserting a pipe into the A horizontal member, a vertical member, a propeller, a fan, or a fan motor or fan guard member in which a fan and a motor are integrated, which also serves as a body reinforcement, is subjected to buckling of the pipe in the pipe cavity. There is a method to reinforce the pipe by encapsulating and curing foamed resins for the purpose of preventing this, making the upper aircraft lightweight and robust, the pipe is made of the above composite material, the structure that assembled the pipe is the most Simplified method, width 15mm to 30mm, height 15 to 30mm, thickness 1.5mm length 195mm to 3300mm about non-equal or equilateral angle aluminum or carbon fiber reinforced resin, glass fiber reinforced Elongated ladder using resin pipes or a combination of these The shape of the shape of a birdcage or the frame of a jungle gym is an object included in the method of assembling by fixing a pipe with a fixture. The method using a honeycomb structure for the upper flying object is 1.95 mm in diameter made of resin or paper From 33mm to 0.195mm to 3.3mm thick cylindrical pipe is assembled and cured with resin to produce a honeycomb structure, and a honeycomb sandwich panel or via-ferran structure panel with a plate attached to both sides of the honeycomb structure. The honeycomb structure in this claim, which is divided into a method of stacking honeycomb structures, is a hexagonal honeycomb structure, an OX structure, a flex structure, a bisecting structure, a feather structure, or other various shapes, and adhesives and brazing Material or 3D lamination technology A laminated structure is created using three-dimensional cutting. The material of the honeycomb structure in this claim is paper, non-combustible paper, metal such as aluminum, titanium, stainless steel, aramid paper, carbon fiber reinforced resins, or glass fiber reinforced. Fiber reinforced resins such as resins, or a honeycomb structure panel such as a combination of these and honeycomb structure panels such as weir ferran structure panels, which have hollow holes with diameters of 330 mm to 990 mm for propellers or fans horizontally A honeycomb sandwich panel is a vertical member of a pipe made of aluminum, carbon fiber reinforced resin, or glass fiber reinforced resin, on which a honeycomb structure panel such as a honeycomb sandwich panel or a weir ferran structure panel is laminated. Or by stacking and connecting honeycomb structures such as weir ferran structure panels in multiple stages, such as honeycomb sandwich panels or weir ferran structure panels, like the internal structure of a honeycomb layered vertically in multiple layers The upper aircraft is composed of the shape of the upper aircraft combined with the shape of a rectangular parallelepiped, cylinder, disk, donut, etc. The upper aircraft is a honeycomb sandwich panel or via ferran when viewed from the top in the horizontal direction. In order to take in air from the periphery of honeycomb structures such as honeycomb sandwich panels or weir ferran structure panels, which are used in a direction that can withstand the load when rising and falling in the vertical direction, where hexagonal aggregates of honeycomb structures such as structural panels can be seen Product with spacing of millimeters to 330 millimeters A fan motor or blower in which holes having a diameter of about 330 mm to 990 mm are formed by closely laminating and stacking honeycomb structures such as a layered method or a honeycomb sandwich panel or a weir ferran structure panel, and a duct fan and a motor are integrated. In order to reinforce a honeycomb structure such as a honeycomb sandwich panel or a weir-ferran structure panel, a pipe made of aluminum, carbon fiber reinforced resin or glass fiber reinforced resin is used as a horizontal member or vertical member. The hexagonal column of the honeycomb sandwich panel made of a honeycomb structure material having a side of 19.5 mm to 330 mm and a thickness of 19.5 mm to 330 mm is used. An electric motor and propeller or fan or fan and motor are installed in a space where a hole of 330 mm to 990 mm in diameter is formed above and below the cave and a fan motor or a fan in which a duct fan and a motor are integrated. Including the method of laminating a honeycomb sandwich panel in which a fan motor or a blower in which the fan is integrated is laminated, and the word "belt member" is used for the upper flying body as a belt-like member, that is, a member for knitting a ridge in this patent claim. The method of assembling cocoon-shaped objects formed by weaving sandwich belt members, which means the sandwich belt member defined in the section, is assembled using a plurality of bamboo baskets formed by weaving bamboo belts. Aluminum and carbon fiber reinforced resins Weaving bamboo with a belt-shaped member made of a composite material that combines flexibility and toughness, like a bamboo material, which weaves bamboo bamboo using a sandwich belt member formed by combining glass fiber reinforced resins and resins. The belt member for knitting the heel used for the material is a metal such as aluminum or titanium having a thickness of 0.33 to 1.95 mm, a width of 3.3 to 19.5 mm, or a carbon fiber reinforced resin, a glass fiber reinforced resin or a resin. Thickness 0.33 to 1.95 mm width 3.3 to 19 centering on a film made of a laminated belt, and a carbon fiber wire knitted like a knitted yarn and belted with an epoxy resin. .Bamboo-like belt knitting bamboo baskets sandwiched between 5mm aluminum bands like sandwiches and bonded with epoxy resin There is also a method of using a composite object of shape as a material for knitting the cocoon. The cocoon is a combination of these cocoons that woven bamboo-shaped composite members of bamboo cocoons into various shapes to form a three-dimensional shape and knitting the cocoon The belt is bonded to the belt at the intersection of the belts with an epoxy resin. The entire collar is tough and supple, and the collar has a diameter of 1 so that it can be restored even if the collar structure is slightly deformed. It can be processed into various shapes like bamboo baskets reinforced with rods or pipe materials that are a combination of aluminum and carbon fiber reinforced resins, glass fiber reinforced resins and resins of millimeters to 5 millimeters. A sphere-shaped method that combines the shape of the colander and the shape of the colander, the earth's equivalent to the equator on the earth can be assembled and disassembled with a fixture, that is, a bamboo sphere hemisphere A semi-circular braid knitted in a hemispherical shape with a sandwich belt member in the shape of a half-shaped Shimazu clan's family crest in the middle and sandwiched up and down in a hemispherical shape, An electric motor and a prepeller or fan are installed in the center of the cross beam of the object shaped like the family crest of the Shimazu clan in the shape of the figure. The upper and lower hemispherical cicada members and the crest of the Shimadzu clan in the center circle Such a member is fixed with a fixture and can be easily assembled and disassembled like a spherical bamboo basket with an electric motor and a propeller or fan installed in the center. Like a wheel motor, there is a method in which the rotor is a disk-shaped wheel and the wheel becomes a propeller or a fan motor or fan that combines a fan and a motor with a motor. The manufacturing method of the fan motor or blower is four, eight, twelve, sixteen, or thirty-two pieces by cutting radially from a location 33 mm away from the center of the disk and bending it into a blade shape. The fan and motor are integrated into a fan motor or blower shape, or a ring-shaped member is welded to the outer periphery of the fan motor or fan shape in which the fan and motor are integrated. There is a method of using a disk-shaped electric motor in which a plurality of coils are arranged on the outer periphery of the ring so that a permanent magnet such as a neodymium magnet is fixed along the outer periphery and the permanent magnet is wrapped. The method of using multiple pieces to gather together like a bunch of kites is also included in the structure of the upper flying object. Including the method of laminating honeycomb structures such as honeycomb sandwich panels or weir ferran structure panels horizontally in multiple stages, this is exactly the shape of the internal structure of a natural round honeycomb. The kite becomes the structure of the entire flying object and protects people inside the kite













It is also possible to enter the inside of a spherical kite, and the kite allows the wind generated by the electric motor to pass downwards and both the propeller or fan guard and the upper flying body and the lower suspension body This kite can also be used as a boarding deck that can feel the structure of the airship and the wind, and the spherical kite can be easily assembled and disassembled by attaching and detaching the fixture. The method is structured by combining two hemispherical cocoons into a sphere, and a propeller or fan and electric motor are placed inside the sphere, and a cocoon-like sphere with a propeller or fan and electric motor is placed like a cocoon The electric motor and propeller or fan, which is a method of constructing the flying object by assembling with the fixtures, are on the shaft of a normal electric motor with a fist-sized rotor. A method of attaching a rocket or fan and fixing it to the center of the cross beam, and a horizontal plane passing through the center of the sphere is at the center of the disk motor and propeller or fan or fan motor or motor and cross beam. There is a method of installing a blower. As a motor, the rotor of a disk type motor is a three-blade prober shape, and a permanent magnet such as a neodymium magnet is fixed around the outer periphery of this disk-shaped propeller or fan. A disk-type electric motor that includes a method that combines a motor with a disk-type propeller or a fan in which a ring-shaped member is wrapped around a magnet on the outside of the child and a plurality of coils are arranged inside the ring is a pipe. Honeycomb such as honeycomb sandwich panel or weir ferran structure panel even with the combined method The lower suspension body in which the lower suspension body is provided at the center of the lower part of the upper floating body of the personal aerial work flying object can be used even in the method of laminating the mobile structure. The lower suspension body is a lobe of natural fibers or chemical fibers having a length of about 195 mm to 3300 mm. Or ropes, wires and wires made of steel wires or metals such as iron, steel, aluminum and titanium, resins, carbon fiber reinforced resins, glass fiber reinforced resins, Kevlar fiber reinforced resins or a combination of these materials The lower suspension body is composed of a lower suspension part made of steel, bar, or pipe material. The lower suspension body is connected to the center of the lower end of the upper aircraft with a freely movable connecting device such as a chain link or universal joint. Lower suspension rope that is flexibly connected so that the center of gravity of the body can be moved freely Alternatively, there is a method of sitting on a swing platform provided on a lower suspension body such as a rope or standing on a step fixed to the lower suspension body for a wire or bar material or pipe material in the air From here, it is a description of the safety measures for workers. Humans who work in the air are light helmets with air caps stiffened with styrofoam and small heels so that they do not damage the body even if they fall from about 33 meters above the ground. A waterproof cotton bag with a thickness of 19.5mm to 33mm, which is packed with air bags such as small air bags covered with rubber or silicon rubber inside a cloth or non-woven fabric of natural fiber size chemical fiber A waterproof and airtight zipper such as a lightweight waterproof cotton lining with a shape like clothes or a collection of fibers mainly containing air There is a method in which a human body protective bag such as a human-type sleeping bag or a human body protective clothing that humans can enter and exit is connected to the lower suspension body with a fixing tool or belt that can be attached to and detached from the lower suspension body, using Zic Tape (registered trademark) The waterproof and airtight zipper, which is a waterproof and airtight zipper description, is about 0.195mm to 3.3mm thicker than the two underlying fabrics for the purpose of waterproofing and airtightness and preventing the cloth from getting into the zipper. When looking at the zipper vertically, the width of the zipper is about the width of the seam on the left and right sides of the zipper, and the length of the resin zipper is about the length of the zipper. Prevents the cloth from biting into the zipper when the fins along the resin zipper are stitched one by one in the seam of the zipper, and the zipper is pulled up The zippers on both sides of the zippers are covered with a silicone resin or rubber-based resin so that the fins that cover the zippers and the fins overlap exactly with each other. Even if the fabric does not bite into the zipper, the zipper can be pulled up and down easily, and at the same time the inside of the zipper is airtight and waterproof, the above is a description of a zipper that is not waterproof and airtight, the protection of human side protection There is a method in which the shock-absorbing material and the seat are processed into a three-dimensional mesh like a scrap of plant yarn using a chemical fiber material wire, carbon fiber wire material or carbon fiber reinforced resin fiber material. The fiber shape of a thread spider that allows you to work in the air with your feet resting on the steps provided on your body -Like shock absorbers or human-type sleeping bag-type or clothes-type shock absorbers detect natural fall in parts that may collide with the ground, such as human-shaped heads, shoulders, spines, and buttocks The acceleration sensor that detects the natural fall of the human body and there is a method that the air bag instantly inflates with compressed air to protect the human body in a shape that wraps the human body before the human body collides with the ground, The method of working in the air is equipped with a parachute on the upper part of the gyro of the upper flying object, and it is structured to automatically open the parachute when a free fall is detected by human will or with an acceleration sensor, so that the worker lost consciousness As a simple emergency rescue method, the personal aerial work flying object is structured to safely descend with humans. The gyro is installed at the top of the upper flying body and works to stabilize the upper flying object in the air.The personal flying object is suspended by humans or robots, video cameras, and radio control devices. A shock absorber such as a balance ball with rubber or silicone rubber sealed inside at the lower end of a human or video camera and radio control device makes it possible to observe or save lives. The following capacitor (capacitor) or secondary battery (battery) is used on the lower surface of the shock absorber, which is a description of the capacitor (capacitor) or secondary battery (battery). Of capacitors and graphene using nanocapacitors between clusters in amorphous and crystalline alloys such as Ni-based and Si-based Single-crystal nanocube placement / arrangement / bonding / interface control technology single-crystal nanocube bottom-up from two to three-dimensional by single-crystal nanocube technology using stacked ceramic capacitors and dielectric ceramics Or, a nanostructured ceramic, metal, carbon, etc. structure that is precisely controlled at the atomic level, a storage device using a unique structure nanocrystal for an electricity storage device, a fuel cell / water electrolysis battery using an nano stacking method, an AGM deep cycle battery, Compact and lightweight fuel cells such as large-capacity ceramic capacitors and solid hydrogen source fuel cells, all-solid-state electricity storage devices of complex hydride-based fast ion conductors, oxide-based bulk all-solid lithium secondary batteries, or large-capacity laminated lithium I need a battery Lithium ion air battery, lithium ion battery, nickel / hydrogen rechargeable battery, magnesium storage battery, non-lithium battery using medium / low temperature ionic liquid, metal and air battery using high oxygen ion conductor nano thin film or anion exchange membrane Noble metal-free fuel cell or secondary metal filled with specific metals such as lithium and sodium only in the interior of a unique structure of tubular carbon nanofiber (CNF) that has multiple nanogates that can only enter and exit ions A lightweight, small, large-capacity battery or capacitor, such as a battery selectively prepared as a negative electrode material for a battery, as described above for a capacitor or secondary battery (battery), is placed under the shock absorber. , Lower the center of gravity of the flying object When the flying object of the personal aerial work is levitated when the mind is at the bottom, it prevents it from rotating in the top and bottom direction. A wire or rope or wire is hung at the lower end, and this wire, rope or wire in the front, back, left or right direction is equipped with a human or radio control device and a small computer with a built-in automatic posture control program. Or, by pulling the wire manually or mechanically, the center of gravity of the flying object for personal aerial work is moved back and forth and left and right to control the flight in the horizontal direction, and at the same time the motor current for levitation By adjusting and synchronizing with the adjustment device, flight control of hovering and movement in the vertical direction is performed to perform personal work flight. Radio control maneuvering device that enables forward, backward, ascending, descending, left and right movements as corps movements, transmitters (receivers), receivers, servos, motor amplifiers, speed controllers, wirings, wiring tools, etc. There is a method of automatically controlling while working with a device that combines a switchboard, switches, and computer. The personal aerial work flying object is controlled manually by a control switch provided at the hand of the passenger, by a radio control radio transmitter (propo) The rope or wire is hung from the lower end of the battery to the ground, the lower end is fixed to the ground, and the human being on the ground is hung from the personal aerial work flying object. To move the flying object of personal aerial work from the ground Yes, only for work, there is a method of transmitting electricity to the required height by placing a battery or power supply unit on the ground, instead of an electric motor for the upper flying body of a personal aerial work flying object to gain lifting force A method using an internal combustion engine is a method using a light-weight internal combustion engine made of a light metal such as titanium or aluminum instead of the electric motor of the above-mentioned flying object. Forced air-cooled whole heat-dissipating fiber reinforced resin metal composite internal combustion engine, which is a description of composite internal combustion engine, directly applies heat and explosion to the high temperature wear-resistant part covering the internal combustion part, ie cylinder head, cylinder, piston, piston ring, connecting rod, crankshaft The receiving part is a layer of lightweight metal such as titanium or aluminum and a steel woof around a layer of wear-resistant and heat-resistant metal. By applying a heat transfer layer of Lullock wool glass wool and a stress transmission rod that transmits explosive force to the fiber reinforced resin layer, stress is transmitted from the metal layer through the heat buffer layer to the fiber reinforced resin layer and directly to the metal part by forced air cooling. Cold air is blown and heat is released from a plurality of small holes opened in the entire casing, and the entire casing of the internal combustion engine such as an oil pan is configured to share a metal or fiber reinforced resin honeycomb structure. The outside of the titanium or aluminum layer is a radiating fin outside the engine of the air-cooled motorcycle. The height is 19.5 mm to 33 mm, the thickness is about 1.95 mm to 3.3 mm, and the range is 1.95 mm to 3.3 mm. Multiple processing is performed to wrap the surface of the metal layer at intervals of about millimeters, and a heat buffer layer is formed on the outside of the metal radiating fin. It is surrounded by a heat buffer layer in which a steel wool layer, a rock wool layer and a glass wool layer, which are compressed from the inside, are provided to form an air-containing layer and comes into contact with the heat buffer layer from the outside The inner surface of the fiber reinforced resin is 19.5mm to 33mm in height, 1.95mm to 3.3mm in thickness, and 1.95mm to 3.3mm in the interval of about 1.95mm to 3.3mm. A honeycomb structure made of metal or fiber reinforced resin is wrapped around the outside of the heat resistant fiber reinforced resin, which is wrapped in a layer of fiber reinforced resin such as heat resistant carbon fiber reinforced resin. The cylinder heads and cylinders that receive the explosive force of the internal combustion chamber, which is responsible for the mechanical structural members related to the strength of the internal combustion engine, are commercially available. The length of one split chopstick is from the support part of the metal layer to the support part of the heat-resistant fiber reinforced resin layer, and a plurality of metal rods having a diameter of 6 mm to 9 mm are provided at intervals of about 33 mm to 195 mm. Layers of wool and rock wool













A rod that penetrates through the layer of lath wool and spreads radially like sea urchin thorns to transmit the explosive force from the metal layer to the heat-resistant fiber reinforced resin layer and to the honeycomb structure layer made of metal or fiber reinforced resin. Both ends of the material are supported by a support part provided in a metal layer and a layer of heat-resistant fiber reinforced resin, the rod that transmits the explosive force is threaded, and the stress transmission rod is threaded into the screw hole cut in the groove of the support The steel wool layer, rock wool layer and glass wool layer are supported by the tips of the inner and outer radiating fins from the compressed inside, and are responsible for overall heat dissipation This heat-resistant heat-resistant fiber reinforced resin that bears the burden is covered with a two-dimensional or three-dimensional honeycomb structure made of metal or fiber reinforced resin, etc. Metal and fiber reinforced resin in which a plurality of small holes having a diameter of about 0.195 mm to 3.3 mm are opened at intervals of about 1.95 mm to 33 mm to achieve overall heat dissipation throughout the fiber reinforced resin and the honeycomb structure. This is an internal combustion engine that combines a honeycomb structure with a honeycomb structure, and the overall heat dissipation is like a dragonfly wing feather, with a thin trachea with a diameter of 0.195 to 3.3 millimeters for heat dissipation. It opens radially from the inside of the internal combustion engine to the outside at intervals of about 1.95 mm to 33 mm, and is opened at the front of the internal combustion engine by the power of the internal combustion engine rotating or by the power of the turbocharger using the exhaust exhaust of the engine. Rotating the blades of the opening, the air is blown and the air diameter is 19.5mm to 33mm There is a forced air cooling dedicated pipe that is distributed and branched so that air is directly blown to the metal fins of the cylinder using a forced air cooling dedicated pipe. Titanium is directly blown to the heat radiating fins of metal such as titanium or aluminum surrounding the internal combustion section to perform forced air cooling. Alternatively, the aluminum radiating fins dissipate heat, dissipate the entire air through the heat buffer layers in the order of steel wool rock wool glass wool, and the heat dissipated air has a honeycomb structure of heat-resistant fiber reinforced resin and metal or fiber reinforced resin. A plurality of diameters 0.195 mm to 3.95 mm inside the heat-resistant fiber reinforced resin layer and the honeycomb structure layer through a thin tube having a diameter of 0.195 mm to 3.3 mm, such as a feather of a dragonfly penetrating therethrough. There are tubules at intervals of about 1.95 mm to about 33 mm. This is to dissipate heat from the whole internal combustion engine through a small hole. This is to disperse the heat so that the resin does not melt with heat. The lower suspension body uses a battery and a fuel tank under the shock absorber. There is a method of installing a battery and a gasoline tank in the vehicle. Forced air-cooled whole heat-dissipating fiber reinforced resin metal composite internal combustion engine can be used as a gasoline engine or a diesel engine. Heavy electric control device, battery and gasoline There is a method of sending the fuel from the ground and sending the fuel to the air vehicle in the air with a pump through the oil supply pipe, and the piston engine type or rotary engine type internal combustion engine, generator and electric motor. Combined and integrated forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable flywheel Luke converter clutch forced air cooling Whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator Electric coil disk stacked generator motor output power transmission transmission integrated hybrid device is forced air cooling when the internal combustion engine is started by the motor and the output of the internal combustion engine increases Overall heat dissipation fiber reinforced resin metal composite internal combustion engine generator motor Torque of internal combustion engine by torque converter and clutch in hybrid device The inner disk is fiber reinforced resin and the outer periphery of the disk is metal fiber reinforced resin A metal wheel that can be increased and decreased while the metal is automatically rotated by computer control. Metal wheel on the outer periphery of this wheel is 360 degrees along the circumference like a shield segment. The equally divided segment is the relationship between the sectors and tracks in the cluster area of the floppy disk. The method of increasing the amount of metal on the outer periphery, which has a concentrically layered structure like the above, is that the metal segments are hooked on the rotating metal outer claws, and the claws form an arc like a claw The claw can be moved in and out by rotating the claw.When removing the metal segment, the claw is pulled in and the segment is separated from the spring wheel by centrifugal force and separated by a rotatable claw provided on the wall of the circumferential wheel. This mechanism can be used to adjust the rotational force of the rotating machine. This mechanism can be used to adjust the rotational force of the rotating machine. The momentum-adjustable flywheel adjusts the angular momentum in conjunction with the computer to ensure a stable angular momentum, and then sends a part of the output of the internal combustion engine to the motor / generator to generate power and output the power to the external compound. There is a method of transmitting power to the electric motor of this. To obtain electric power, the power of the internal combustion engine is obtained and then power generation is performed, and the fine adjustment of the output such as thrust is an advantage of the electric motor that obtains thrust if necessary. Is an internal combustion engine generator that can control the energy in total by using a computer and share the distribution of the motor and motor angular momentum adjustable spring wheel torque converter clutch computer integrated hybrid device, the above is forced air cooling overall heat dissipation fiber reinforced resin metal composite internal combustion engine The rotary engine method is a rotary engine and forced air-cooled whole heat radiation fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor forced air cooling whole heat radiation fiber reinforced resin metal composite rotor permanent magnet fixed This unit can be used as a sub-coil disk stack type electric motor / generator. Combined and laminated, forced air-cooled whole heat-dissipating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable spring wheel torque converter clutch forced air-cooling whole heat-dissipating fiber reinforced resin metal composite generator motor output power generation integrated power transmission hybrid device, here Is a description of forced air-cooled whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor, the disk stacking type electric motor has a rotor with a diameter of 19.5 mm to 330 mm in thickness 1. 95 to 33 mm metal or fiber reinforced plastic disc shape with a circular diameter of 1.95 to 33 mm inside 3 or 6 or 12 or 16 or 32 in a concentric radial position from the axis There are multiple holes that fit in the disc of A disk that fixes holes in a concentric circle radially from the shaft toward the electric motor shaft and is fixed with permanent magnets. Permanent magnets such as magnets are embedded and fixed, and the permanent magnet is fixed so that the magnetic flux is perpendicular to the disk surface. The disk of the electric coil is fixed to the rotating shaft of the electric motor. The magnetic flux of the electric coil is the disk. Is the same size as the disk of the magnet, but the shaft portion of the electric motor is a hole and passes through the shaft of the electric motor and is permanent with a gap of 0.195mm to 0.33mm At the position where the magnet and the electric coil face each other, an electric coil thicker than the permanent magnet is fixed at the position corresponding to the permanent magnet, and the copper enamel wire of the electric coil or room temperature The laminated ceramic type coil formation with nitrogen circulation glass amorphous or ceramic coating in the conductive pipe is not a coil but a three-dimensionally laminated coil and insulator to form a coil. There is a method in which a ceramic coil and an insulation coating ceramic are simultaneously formed by a three-dimensional solid atomic layering technique, or a high melting point glass or ceramic is used to make a female coil and a good conductive metal with a low melting temperature is made of glass or There is a method of manufacturing a heat-resistant coil made of glass or ceramic that is insulated by injecting with an inert gas gas while keeping the temperature in a female coil of a ceramic coil. Disks with holes in the central axis arranged radially on the circumference are fixed to the casing of the electric motor The disk that fixes the electric coil is made of metal or fiber reinforced resin. The permanent magnet disk and the electric coil disk are alternately laminated. The disk with the permanent magnet fixed is an electric coil from both sides. The electric coil that is sandwiched becomes a brushless motor that rotates the permanent magnet in phase with the rotation direction. This principle is based on fixing the disk that fixed the permanent magnet to the casing of the electric motor and fixed the disk that fixed the electric coil. The method of the brush motor fixed to the shaft of the electric motor may be the method of forced air cooling whole heat dissipation rotor permanent magnet stator electric coil disk laminated electric motor is metal and carbon fiber, the other part is fiber reinforced resin Forced air cooling is performed with blades fixed to the shaft of the electric motor, and the air passes through a plurality of holes formed obliquely at an angle of the blades with respect to the rotation direction of the disk. The air that has been cooled with air is passed backwards to cool the disk and dissipate heat. The hot air radiated from the entire casing has a diameter of 0.195 mm to 3.3 mm and is spaced at intervals of about 19.5 mm to 33 mm. The number of permanent magnets and electric coils is arranged for multiple shafts and casings compared to conventional electric motors that radiate heat from the whole electric motor through a small hole, eliminating the problem of heat dissipation and the rotation direction of the disk A plurality of holes with a diameter of about 0.195 mm to about 3.3 mm drilled at an interval of about 1.95 mm to 33 mm and inclined at an angle of about 19.5 to 33 degrees with respect to the rotating surface. Depending on the method that solves the problem of heat dissipation by becoming a kind of blower by rotating, the electric conductor is made into a pipe shape There is a method of cooling the inside by the above method.Also, the disks are all powerful electric coil disks, and the alternating current is generated in such a way that the disk with the opposite direction of the magnetic flux of each coil and the disk with its axis fixed rotates. This method, which may be given, will be all electric coil brush electric motor, the above is a description of forced air cooling whole heat radiation fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor, from here Bird Strike Prevention Device Fiber Reinforced Resin Metal Composite Turbine Stacked Electric Motor is a turbine stacked type electric motor. The disk of the disk stacked type electric motor is processed into a complete blade shape, and permanent magnets and electric coils are fixed to the blades. The blades are made by alternately laminating the permanent magnet layers and the electric coil layers so that they look like jet engine intake turbines. This is a description of the bird strike avoidance device, which is a description of the bird strike avoidance device. The blade for blade strike is made of steel, stainless steel or aluminum alloy steel with the tip of cutting the wind of the blade in order from the entire surface of the intake blade. When a bird strike occurs after processing like a sharp blade, the bird is cut with a multi-stage blade-shaped steel blade, and the meat pieces that are cut into pieces or minced meat pieces are removed from the sides of the engine or motor by centrifugal force. A flute that tends to splatter toward the blade is provided on the side of the casing to guide the meat piece to a position where the flesh of the electric motor or jet engine is likely to splatter by a sensor that detects the bird strike by guiding the blade to the position where the flesh is to fly. The engine or motor can be opened from a small window-shaped opening -The normal jet engine method that temporarily ejects and discharges with the internal wind is to prevent the bird's meat pieces from reaching the burning part of the jet engine and to minimize damage to the engine due to bird strike. The above is a description of the bird strike avoidance device, and a neodymium magnet at a position where the direction of magnetic flux is parallel to the blade rotation axis on the blades of the turbine blades having a pitch angle and obliquely arranged using this device. The electric motor in the shape of an intake turbine of a jet engine in which layers of permanent magnets and electric coils, such as alternating layers, are easily replaced, and the output can be controlled freely without the need for complicated mechanisms. Light turbine and noise-free jet turbine type by using fiber reinforced resin as the turbine that can solve the problem Aviation fuel that can be used in passenger aircraft and can be used in passenger aircraft to produce aircraft using a jet turbine-shaped electric motor for noise reduction by generating electricity with a lightweight internal combustion engine of gasoline or light oil or heavy oil Instead of a gasoline engine or heavy oil
Or diesel oil












It is possible to generate electricity with a diesel engine and to purify the exhaust gas through a soundproofing muffler and exhaust gas purification catalyst ceramic. At the same time, the aircraft attaches silicon-type solar cells or polymer organic thin-film solar cells to the whole or a part of the aircraft over the sea of clouds. It is useful for preventing air pollution or economically and safely for fuel explosions. Inside a jet turbine-shaped heat fiber reinforced resin-metal composite that generates power by a low fuel consumption internal combustion engine and obtains thrust of flight. Electric motor can be driven, or at the same time forced air cooling whole heat-dissipating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable bounce wheel torque converter clutch forced at the rear of jet turbine shaped heat fiber reinforced resin metal composite electric motor as hybrid type Air cooling whole heat radiation fiber reinforced resin metal composite generator By combining the power transmission integrated hybrid device, the output, power generation and power transmission by the internal combustion engine are integrated and computer management is performed, and it becomes possible to control the distribution of energy sharing, and the internal combustion engine obtains thrust and power while the power is converted into an electric motor. The above is a description of the bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor, which can transmit power and assist the battery power, and can charge the battery with surplus power. From here, it is a description of the method of using a turbine stack type electric motor for a personal aerial work flying object. Permanent magnets and electric coils are arranged concentrically around the circumference of the blade, and magnets and electric coils are arranged. The top of the upper aircraft using blade electric motors with alternating layers as the flying object for personal aerial work The pure method is a method in which the upper blade and the lower blade are sandwiched so that the upper blade and the lower blade are rotated in reverse directions with a blade having a permanent magnet fixed above and below a disk to which the electric coil is fixed. A magnetic flux from N to S is formed in a concentric circle along a circle inside the circumference of a disk made of fiber reinforced resin or a metal or a combination of metal and fiber reinforced resin with a diameter of about 3300 mm from 33 mm. The disk is arranged in a radial direction from double to triple concentric circles so that the direction of the magnetic flux is perpendicular to the disk surface, that is, the magnetic flux is perpendicular to the disk surface, that is, a honeycomb with no wind Honeycomb through which wind passes) The structure or fiber reinforced resin can be directly opened at intervals of about 1.95 mm to 33 mm in consideration of mechanical distribution. Wind that has a shape with a plurality of holes with a diameter of about 0.195 mm to 3.3 mm or a mesh shape that supports an electric coil, and the wind path is slanted according to the pitch angle of the blade. There is a shaft at the center of the disk that is for the passage of the shaft, and the shaft protrudes from the center of the two faces of the stator disk. This shaft has a hole through which the shaft passes through the center so as to sandwich the disk of the stator's electric coil Two blade windmills with a pinch are sandwiched from above and below. The blade of this blade windmill has a permanent magnet such as a neodymium magnet at a position facing the electric coil with a gap of 0.19 mm to 0.33 mm. The two blade wind turbines, in which the alternating current is sent to the electrical coils that are in opposite phases to each other, rotate in the opposite direction and blow the wind downward. The blade that prevents the entire aircraft from rotating by the frame shape or the net-shaped blade guard is protected from the damage of the blade. The internal combustion engine generator-motor hybrid device, which is attached to the body and constitutes a personal aerial work flying object, can be combined with forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine. The method of using the balloon to obtain the ascending force of the upper flying body of the personal aerial work flying object, which is attached to the body as a personal aerial work flying object, is a combination of hot air balloon, gas balloon, hot air balloon, and gas balloon. Individual air working flight using balloons is composed of upper flying body and lower suspended body, and upper flying body using hot air balloon Consists of an envelope (ball skin), a load tape, and a wire. The envelope material is made of nylon or polyester chemical fiber that is airtightly coated with polyurethane, and is the smallest unit of the envelope. A ball or bag shape or cylindrical shape reinforced with load tape by vertically stitching gores that are vertically sewn together horizontally and reinforced with load tape, or a number of parts receiving the load vertically. Load tape, which is reinforced with a nylon or polyester road tape or carbon fiber reinforced resin wire netting, is sewn on the crown ring at the top of the emperope, the lower end is a suspension cable and the following backpack Suspensions that are connected and share the load The cable is made of steel, stainless steel, carbon fiber reinforced resin wire, twisted wire, Kevlar fiber reinforced resin wire or twisted wire, and the load tape is horizontally oriented like a barrel tag to prevent the envelope from tearing. Also used in multiple, the peripheral part of the burner at the opening part of the envelope has a glass squirt shape of the following kerosene lamp with a supplementary cloth called a triangular scoop or skirt shaped skirt for introducing hot air There is a method in which the net replaces this skirt or scoop. There is a method in which an auxiliary fabric called a skirt covers the upper hemisphere of the squirt sphere made of net to facilitate the recovery of hot air. The part that receives heat is called Menox. The method of using a hot air balloon that uses materials as a gas balloon is airtight. The envelope is tied to the following torch with a belt and the floating gas is ejected from the torch.This envelope is mainly sewn with a thread such as polyester, and the place requiring heat resistance is sewn with a thread such as Nomex. A solenoid valve made of carbon fiber reinforced resin that exhales hot air is opened and closed at the top or middle of the envelope. It is controlled by manual, wireless, and automatic control. The lower suspension body is about 195mm to 9900mm in length and 1950mm to 99000mm in length, and the size of the lower suspension is about the size of a rucksack that you carry when climbing up Everest from the size of a school bag used by elementary school students. It consists of a backpack and a backpack peripheral device. The belts to be carried can be joined with the buckle at the position in front of the chest, the belt is wrapped from the backpack's back to the belly, the belt is wrapped around the front of the belly and the person is fixed to the lower suspension body with the buckle etc. A belt hangs down on the seat part from the contact part and the two rings provided on the belt of the seat part allow humans to pass both feet and stabilize the buttocks from the shoulder to the chest and around the belly and How to fix the occupant to the backpack that suspends the shock absorbing device under the human foot that carries the backpack and the back center part of this belt that is going to fix the heel part with a belt In detail, the backpack is like a school bag used by elementary school students, and the right and left belts that fix the body and backpack by passing the arms through the left and right belts The belt is stretched from the left and right sides of the backpack to fix the abdomen of the passenger, which can be fixed using a buckle at the chest. The belt extends downward from the backpack's back and can be fixed on the backpack, and the belt has two rings that allow both feet to pass through. A shock absorbing device in which a belt extends further beyond the wheel that passes both feet, and the shock absorbing material is fixed to the tip of the belt, rope material or bar material, which can fix the heel portion of the passenger The propane gas cylinder and the digestive gas cylinder below the battery and the battery, condenser, power supply controller, autopilot, video camera, etc. The peripheral device of the pack is a horizontal cylindrical envelope take-up device having a horizontal length of about 1950 mm located at the upper part of the backpack, and a guide for winding the envelope (ball skin). There is a method of forming a link shape that passes through the ball skin) and a hopper shape made of resin etc., and the uppermost end of the envelope is connected to the winding device with a string or wire, so that the fishing boat net can be unwound and rolled up As a detailed description of the winder, the envelope winder has a guide or hopper for winding the envelope behind the winder, and a cable that guides winding from the top of the envelope passes through the hopper. The envelope is fixed to the rotary shaft of the winder and The suspension cable can be taken up together with the envelope. The envelope take-up device, which has a mechanism that opens manually or automatically, can be moved by the motor in the backpack, and the right lever is viewed from the passenger. The right lever extends from the right side of the backpack, and the switch that unwinds and winds the envelope is attached to the right lever, and the right lever can be moved up and down, left and right and back and forth like the control stick of a zero-type ship fighter The movement of flying objects The method with multiple propellers or fans in order to interlock with the vertical and horizontal movements is a propeller or fan that is linked with the device that changes the position of the aircraft. It is linked with the front / rear direction output, and it is linked with the up / down / left / right direction rudder behind the fan guard, and the position of the personal aerial work flying object can be operated. The right lever that realizes autopilot changes the position of the top, bottom, left and right, and the left lever changes the position of the top and bottom. From the top center of the backpack, the diameter is 19.5mm to 33mm. 195mm to 3300mm pipe-shaped metal or resin here called torch Or there is a cylinder that leads propane made of carbon fiber reinforced resin or glass fiber reinforced resin, and a small burner is installed at the top end of the cylinder of this torch, and an ignition device and a fire extinguishing nozzle are near the small burner. The left handle attached controls the rough vertical movement of the flying object for personal aerial work, and the left handle extends from the left side of the backpack so that it can be operated with the left hand when viewed from the back. There is a lever and the amount of gas can be adjusted by turning the handle of the left lever. The gas has a changeover switch such as propane gas for hot air balloon and helium gas for rising or propane helium mixed gas. These switches with a fire extinguisher switch and the left lever are electrically connected to the autopilot and are A valve that adjusts the amount of propane inside the torch is installed on the left lever as viewed from the side of the backpack side that realizes maneuvering and automatic maneuvering, and hot air or floating gas exhaust valve is opened and closed on the valve A valve that adjusts the amount of propane and a hot air exhaust solenoid valve that are equipped with buttons are electrically connected to the autopilot device, realizing manual, wireless, and autopilot. A heat-resistant metal or fiber-reinforced resin called a combustion guard net around the vicinity of the combustion section of the pipe that guides propane gas connected to a propane cylinder or a floating gas cylinder installed under the shock absorber A net-shaped tube with a diameter of 66 to 195 mm and a length of 195 to 3300 mm surrounds the small burner. This net-shaped cylinder is structured so that it can move up and down around the cylinder that sends propane, and when storing the envelope, the cylinder that sends propane completely fits in the center of this net cylinder and the burner is When used, this cylindrical net extends to the top of the small burner.













The combustion guard net which prevents the envelope (ball skin) from burning with the heat of the burner is like a glass squirt of a kerosene lamp so that the envelope (ball skin) does not burn with the heat of the burner when the small burner is ignited The bottom of the mesh swells in a spherical shape with a diameter of 330 mm to 990 mm, and the method of extending the maximum cylindrical mesh upward is a small burner where the bottom of the cylindrical mesh protects the periphery of the burner. A shaft that rotates the prober or the fan extends from the center of the back surface of the backpack where the digestion fluid is ejected when the envelope (ball skin) is burned by the heat of the burner. The diameter of the backpack is about 19.5 mm to 33 mm and the length is about 19.5 mm to 66 mm. The electric motor described in the scope of claims of the present invention is installed horizontally in the middle of the interior of this electric motor. The fan guard and shape of the home electric fan, in which the propeller or fan of the previous period is fixed to the tip of the electric motor shaft The fan guard air that is similar has a cross-shaped rudder in the direction in which the air blows, and on the right side of the person riding on the side of the backpack, the lever extends from the backpack side to the right hand position and this right lever is By moving it up and down, left and right, the rudder fixed to the fan guard guides the air blown back and forth back and forth and left and right to move the individual aerial work body up and down and left and right.This lever is electrically connected to the autopilot. The control of the radio control and the automatic control are realized. Rise and fall are roughly adjusted by adjusting the valve on the left hand lever of the passenger. Adjusting the buoyancy of the hot air balloon by adjusting the fire power of the left lever valve adjusts the amount of floating gas such as helium etc., the gas balloon method rescues the rescuer by radio control automatic control and in the air with a video camera Capable of shooting, manual, wireless, automatic control is possible. The crew is equipped with the above-mentioned shock absorbing human sleeping bag and shock absorbing air bag and free fall on the upper part of the envelope unwinding and winding device This is a gas balloon method that is equipped with a ballot chute that is detected by a sensor and opened automatically by a person's will or automatically. The material is a carbon fiber reinforced resin wire having a diameter of 0.195 to 3.3 millimeters, and a grid of 330 to 1950 millimeters. The shape of the mesh knitted by the square mesh is 0.195 mm to 3.3 mm thick woven with a polyethylene terephthalate cloth inside the mesh of the carbon fiber reinforced resin wire having the same size as the hot air balloon method. This gas balloon is heat-treated and heat-treated from the inside of a polyethylene terephthalate cloth bag that adheres a 3 mm cloth to the inside of the mesh to make a gas balloon airtight with latex rubber, natural rubber or urethane resin. The tip of the hot-air balloon torch described above is introduced into the gas balloon and is air-tight, and helium gas or hydrogen gas cylinder is installed instead of the propane gas cylinder, that is, the gas inside the balloon, that is, hot air. As a hot air balloon or gas balloon by changing to hydrogen (explosion is prohibited because it explodes) or helium The balloon opening can be used for the hot air balloon method to collect the heated air and the gas balloon method has the gas outlet tube inside the envelope and the gas balloon method has the tip of the opening. This bundling method is like a flare skirt made of thin silicon rubber or rubber-based resin fibers in an airtight manner, and is tightly bound with a band to prevent gas leakage as much as possible. As long as the time or air floating time can be obtained, it is assumed that gas will leak to some extent. The personal air work flying object combining an electric motor or an internal combustion engine and a balloon is divided into an upper flying object and a lower suspension object. The ice-cream cup cone-shaped saddle type envelope storage device is a method for storing the envelope and envelope of the upper flying object. Motor motor or internal combustion engine through a universal joint that can freely change the direction of the electric motor to the tip of the arm that extends in the shape of a cantilever around the cup cone shape cup A propeller or fan is attached to the shaft of an electric motor or internal combustion engine, and the tip of the lower part of the cup cone shape that moves the balloon up and down, front and rear, left and right by changing the direction of the electric motor or internal combustion engine is described above. Electric motors or internal combustion engines and hot air balloons or gas balloons or heat and gas combined balloons that can be boarded by humans with a lower suspension body are manually, wirelessly, or automatically operated. The ice cream cup cone shaped bowl is a cone A circle with a small radius in the shape of a base, a circle with a large radius on the bottom surface is the top surface, and a circle with a small radius on the bottom has a lower ring made of metal or fiber reinforced resin. From the three points where the circumference is divided into three parts, the branches forming the ridges are from three places that extend from the ring surface to the left and right at an angle of about 30 to 60 degrees with respect to the ring surface. Since there are two each, there are a total of six, each one forming a helix according to each angle. The front end of the helix is connected to the upper link at a point at the outer periphery with a central angle of 60 degrees. The intersection of the mesh that is meshed and is knitted regularly is fixed with epoxy resin etc. The lower link is divided into three parts, the upper part is divided into six parts, and the three parts connected by the belt member knitted into the mesh ridge are described Because the lower ring is actually 1 The split method is that the upper ring will be divided into 24, which is twice the twelve. The twelve split may be 36, the lower link may be any number of dynamically adapted anyway, and the upper is double that anyway. In this way, an object like a large trash can is formed in the truncated cone with the bottom of the truncated cone that combines the envelope storage with the side of the truncated cone shaped like a bowl and the structure of the upper flying object. The storage method in which the envelope is stored in the cage with the frustum open upward is that the point inside the load tape divided inside the balloon due to mechanical considerations, that is, the balloon is the earth, and the balloon loads like meridians and parallels. This envelope in which a flexible wire that also serves as a suspension cable of metal, resin, or carbon fiber reinforced resin is hung from the intersection of the meridian and latitude that is reinforced with tape. Multiple flexible suspension cable wires inside the loop can be wound or unwound by rotating this roller, which is fixed to the roller of the suspension cable winder installed in the lower part of the cup cone shaped cage. The envelope is melted by heat at the bottom of the cup cone-shaped bowl, which can be stored inside the cup cone-shaped bowl opened up or removed from the cup cone-shaped bowl. The method of using heat and gas with a gap between the envelope and the burner that takes heat into consideration to a lesser extent is that the gas outlet is located inside the cup cone-shaped bowl and the gas outlet is the envelope Cup-cone bowl with the tip of the burner serving as a gas injection hole inside Is a cup cone-shaped kite with a small burner surrounded by a combustion guard net installed at the bottom of the envelope at a distance where the envelope is unburned and stored, and serves to transmit the lifting force of the balloon to the lower suspension body As described in the claims, the ice cream cup cone type flying body can be used as a sealed hot gas balloon by mixing and burning propane gas and helium gas. The method of manufacturing a personal aerial work flying object is a combination of the above.
The personal aerial work flying object has a structure simulating the seeds of dandelions flying in the sky. From here, the material of the material of the personal aerial work flying object, which is a description of the light and strong material of the personal aerial work flying object As a form of protein, a basic structure such as a metal or a resin corresponding to an amino acid, a fiber reinforced resin, or the like, which has a structure simulating a chemical structural bond model of protein, is bonded with multiple branches such as peptide bonds. Conformation domain (conformation) motif (super secondary structure) fold protein (folder structure) of the primary, secondary, quaternary, and quaternary binding side chains of proteins that make up a three-dimensional structure. 3D structure considering tension member and compression member so as to meet mechanical needs by mechanical structural mechanics analysis by computer so as to constitute There is a method that uses a cutting three-dimensional modeling technique or a three-dimensional three-dimensional lamination technique to determine and manufacture. The term “honeycomb” used in this claim means a broad-sense honeycomb structure such as a weir-ferran structure, and a hexagonal honeycomb structure Or the term fiber reinforced resin, which includes OX structure, flex structure, bisecting structure, or feathered structure, is defined as a term that refers to carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin, etc. In order to realize a personal aerial working flying object, the present invention claims that a lightweight and toughened laminated composite material is invented by using a large amount of honeycomb structure and fiber reinforced resin. The term is defined as an object flying in the air, and various fighters or passenger planes Or there are methods that use waterproof paint or weather resistant resin on the outer surface of the flying object, including methods that apply techniques and materials of personal aerial work flying objects in helicopters, airships, spacecrafts, artificial satellites, space stations, etc. A simple method of weathering a personal aerial work flying object according to the present invention is the method described in the claims of the present invention on the surface of steel and has a diameter of about 3.3 nanometers to about 1.95 millimeters and a height of 3 The weather resistant resin, which is a method of processing a plurality of sea urchins at intervals of about 3.3 nanometers to about 1.95 millimeters at intervals of about 3.3 nanometers to about 1.95 millimeters and vacuum-depositing titanium, aluminum, or glass on the surface, Using a laser technique on the surface of epoxy resin, etc., cut multiple grooves with a thickness and depth of about 3.3 nanometers to about 1.95 millimeters. A square surface with a side of about 3.3 nanometers to about 1.95 millimeters is cut by laser technology and cut to a diameter of about 3.3 nanometers to about 1.95 millimeters with a height of 3.3 nanometers. 1 to 1.95 millimeters from 3.3 nano to 1.95 millimeters at intervals of a plurality of sea urchin strips, such as titanium or aluminum, or layers of metal or glass are layered alternately. Or by laminating a single material to form a film, laminating a vacuum-deposited film, and burying the portion cut out by laser technology as much as necessary for weather resistance, and laminating amorphous oxidation and UV protection This is a product that has improved the weather resistance of resins by creating a film, and the manufacturing method of this weather resistant resin is to make a resin body as a fiber reinforced resin. It can be used for weathering surface treatment of civil engineering structures such as steel, tools, machinery, automobiles, reinforced concrete, etc. The surface treatment of flying objects is a surface by a movable vacuum hopper vapor deposition sintered lamination spraying device instead of painting. The movable vacuum hopper vapor deposition laser-sintered laminating spray equipment that can be processed is constructed by replacing the baking part of electrostatic coating with laser technology by applying vacuum vapor deposition and electrostatic coating in combination. The problem of peeling between layers in the laminated method is solved by cutting technology such as sea urchin spines. There is a method in which the mixture is mixed with the liquid and fixed on the sprayed surface from the nozzle to the processed surface and baked by the method described in the claims. Or, the crucible of a normal vacuum deposition apparatus has a gimbal structure and the vacuum deposition direction can be 360 degrees, and the movable vacuum hopper atom molecule implantation spray deposition powder electrostatic transport laser welding sintering laser cutting spine processing lamination method surface In the weathering method, a square or conical funnel-shaped hopper having a bottom surface with a bottom of about 195 mm to 3300 mm, which creates a vacuum in the hopper, is used, and a bottom surface of the silicon-based resin or along the bottom surface of the hopper A sucker-shaped object made of a rubber-based resin that is kept airtight, so that the octopus's sucker sticks to anywhere. Like a cathode-ray tube electron gun from the top of the square or cone toward the bottom surface after vacuuming In addition, weathering fine particles are sprayed from the nozzle at high pressure for weathering processing on the surface processing site using laser technology, and the charged atoms, molecules or fine particles necessary for weathering are electrically electrostatically transported for weathering. Transporting to the processing surface to secure the properties or electrically charging atoms, molecules or fine particles by moving like an electron gun and accelerating using an electric field, and laser processing is the electron gun's cathode ray tube Scanning lines on the scanning surface move like electrons, and a weather-resistant substance is welded and fixed on the processing surface, or electrostatic transport is required to be processed by laser technology like scanning line electron movements. Powder electrostatic transport that welds or sinters the surface or evaporates the weathering substance with a gimbal crucible and electrostatically transports and deposits it to fix the weathering substance to the work surface. There is also a method of laser welding and sintering. Ultrasonic waves are applied to fine particles that are in a charged state and diffused by electrostatic transport. There is also a method of bonding to a weather resistant processed surface by vacuum evaporation. The surface of the resin layer or metal layer is melted by laser technology by electrostatically transporting it to the processing surface while diffusing with fine powder ultrasonic vibration of about 3.3 nanometers to 0.195 millimeters in size of the resin or metal. Then, a resin layer or a metal layer that is welded or bonded by sintering and bonding is formed, and a charged fine fiber fragment having a size of about 3.3 nanometers to about 0.195 millimeter is electrostatically applied to the processed surface. A resin layer or a metal layer is formed on the surface of the resin or metal that has been transported to form a fiber layer by the method described in this claim. Cut a plurality of grooves from 3.3 nanometers to 0.195 millimeters, and the square side with a square of 3.3 nanometers to 1.95 millimeters on one side of the grid is cut by laser technology and cut into diameters. Is an object such as a sea urchin elongated spine having a height of about 3.3 nanometers to 1.95 millimeters and a height of about 3.3 nanometers to about 1.95 millimeters. A square surface is processed, and a quantity of titanium or aluminum metal or glass necessary for weather resistance is melted on a plurality of spines with a gimbal crucible. The crucible is heated in an electric furnace to evaporate the weather-resistant material and process the surface. Vacuum-deposited and vapor-deposited on these weather-resistant materials to create a vacuum space. In addition, this method includes a method of performing weathering processing on a metal surface by directly applying laser-processed spines to the base of the structure, and then depositing the weathering material, which is applied not only to flying objects but also to existing structures. The above-described series of processes that can be applied to can be automated robot construction, and the above is a description of the light and tough material of the flying object for personal aerial work. The application of laminated honeycomb structure fiber reinforced resin composite technology for flying objects is applicable to denture manufacturing method applying beam theory on elastic floor, from here silicon rubber sucker layer shock absorption layer honeycomb structure layer fiber resin layer meshing Silicon rubber sucker layer shock absorbing layer honeycomb structure layer fiber resin layer meshing part metal ceramic composite laminated denture manufacturing method, which is a description of part metal ceramic composite laminated denture manufacturing method Place the gypsum male mold on the gypsum male mold base around the gums in the oral cavity of the human mouth where you want to put the denture, and then spray the gypsum gum male mold with a medically safe release material layer The method of laminating from a soft resin that is safe for medical use to a hard resin is a method of laminating a computer using the theory of beams on an elastic floor so that when the force is applied to the denture, the force is applied to the entire gum. The first layer in which the dentures come into contact with the gums is a medically safe silicone rubber sucker layer on which a honeycomb structure as an intermediate layer on top of a stress buffer layer that is a stress buffer layer such as foamed urethane This is a denture surface layer made of a fiber-reinforced resin that is relatively thin and made of fiber-reinforced resin on a honeycomb structure and is made of a fiber-reinforced resin that is safe for medical use and has a thickness of about 1.95 mm to 3.3 mm. The resin is a fiber reinforced resin in the tooth portion, and only the meshing portion at the top end of the tooth is 0.195 mm to 3.3 mm in thickness, which is safe for medical use, sintered metal, or metal ceramic. Or porcelain or ceramic, or a composite of these metals and ceramics, and the dentures as a whole are 0.195 mm to 0. When the denture is pressed by a denture that is soft enough to move about 33 millimeters and the engaging part is hard and at the same time the resin part can be deformed, the shock absorber transmits the force to the fiber reinforced resin through the honeycomb structure. It is a denture with a stress buffer layer made of shock absorbing material that can distribute the force to the entire gum The inner surface of the denture is made of medical silicone rubber and has good adhesion, and the gum removes the air inside the denture so that it sticks to the gum exactly like a sucker, and a piece of rice cracker is between the gum and denture It is a structure that does not hurt when it enters, and the metal or ceramic or metal-ceramic composite that forms the complete tooth shape of the meshing part by laser cutting technology is only the meshing part and the resin of the meshing part is booked The sea urchin spine described in the claims is processed on a medically safe resin, and the necessary amount of medically safe titanium is deposited or coated with an adhesive on the meshing part and titanium powder is applied. The surface of the denture is sintered by laser technology, or the meshing part is made of titanium in a thin horseshoe shape with a fiber reinforced resin with a return at the center of the teeth Shape memory memorized with a spring or body temperature that is safe for medical use and covered with resin so that the upper and lower dentures can be moved softly at the end of the dentition, which may be fixed using an adhesive in place A steel material with a shock absorber attached to the back of the alloy or a spring material, or a shape memory alloy wire material or a metal material with a shape memorized at body temperature, or a metal material coated with a resin or shock absorber material is embedded in the denture. The force of sticking the teeth to the palate with the viscosity of saliva is gently supplemented with the restoring force of the metal, and the teeth are stabilized in the palate, and the substances in the denture resin have medically safe medical effect substances, for example regularly under the guidance of a doctor Functional dentures infiltrated with anti-diabetic drugs or other substances that relieve the mood are included in this method, and they are strong, light, and strong, comfortable to wear and not painful It is possible to manufacture comfortable dentures that do not hurt anything and feel comfortable. Silicone rubber sucker layer Shock absorption layer Honeycomb structure layer Fiber resin layer Interlocking metal ceramic layer Metal and resin and impact that stabilize dentures above and below A manufacturing method in which an absorbent material and a silicone rubber sucker layer are separately manufactured and assembled using a medical adhesive such as an epoxy resin is also included in the scope of the present invention. Fiber resin layer meshing part Metal ceramic composite laminated denture manufacturing method description, from here on the description of the material reinforced and reinforced with a fiber reinforced resin on the surface of the honeycomb structure made of wood, paper, resin and foam resin, etc. As a structure of the flying body, solid wood conduits and mentor pipes are stuffed with curable resin to strengthen the wood, and then the hexagonal shape such as honeycomb structure A hexagonal shape with a side of about 1.95 millimeters to 33 millimeters or a circle with a diameter of about 1.95 millimeters to 33 millimeters with a plurality of small holes at intervals of about 1.95 millimeters to 33 millimeters. Generate multiple small holes on the surface











Foam such as foam urethane

The outer surface is filled with a fiber reinforced resin such as a carbon fiber reinforced resin or a glass fiber reinforced resin instead of a material reinforced with a resin and reinforced to a thickness of about 1.95 to 33 mm or a foamed resin such as urethane. What is hardened by covering and reinforcing 95 to 33 millimeters, or plywood or laminated timber or solid wood described in the scope of claims, is reinforced with resin and has a side of about 1.95 to 33 millimeters. In the adhesive between wood and wood of hexagonal shape or a circle with a diameter of about 1.95 to 33 millimeters and drilling a plurality of holes at intervals of 19.5 to 33 millimeters like a honeycomb structure From 1.95 mm in diameter, which is filled with compressed air or gas at 1 to 3 atm. Resin spheres such as polyethylene terephthalate, such as spherical or polyhedral polyethylene terephthalate, with a thickness of 33 millimeters from 0.195 millimeters to 3.3 millimeters are mixed with a small crushed egg grain shape of multiple children and bonded with epoxy resin etc. The outer surface of the object that has been hardened by sandwiching a weight-reduced object and containing air is coated and reinforced with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin at a thickness of 3.3 to 195 mm. A structure like a honeycomb structure, that is, a hexagonal hole or a round hole like a hexagonal hole in a honeycomb structure on a thing that has been hardened or laminated with paper such as corrugated cardboard and soaked with air and adhesive In order to make a plurality of cardboards with a space of 19.5 mm to 33 mm spaced apart from one side or circle of a hexagon. The surface of an object whose weight has been reduced by drilling a plurality of small holes such as hexagons or circles of about 1.95 mm to 33 mm or the like is reinforced with a foaming resin such as urethane foam or a plurality of small holes of paper. Metal or paper honeycomb structure with a foamed resin outer surface reinforced with a honeycomb structure with a plurality of holes spaced from 5 mm to 33 mm, that is, a hexagonal hole in the honeycomb structure replaced with a circular hole And then reinforced with a fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm, or a thickness of 0.195 to 3.3 mm. A paper cone with a square or rectangular side of about 1.95mm to 33mm. Paper that has been cut into a flake shape or shredded with shredders used in office work is mixed with air and stirred to wrap the crumpled air. The paper is soft and fluffy. After the fiber is loosened, about half this soft and fluffy paper fiber loosen object together with an adhesive such as epoxy resin is stirred and compressed appropriately and hardened to the required strength The material molded into this member is light and has a cavity inside, and the required strength can be obtained by adjusting the amount of adhesive. This paper is cut into a cone flake shape and mixed with air and agitated paper and adhesive. In order to reduce the weight after forming the compressed member into a mold, the side of the circle or hexagon has a side of about 1.95 to 33 millimeters. A plurality of holes are formed at intervals of 19.5 mm to 33 mm to make a thing similar to a honeycomb structure, that is, a hexagonal hole in the honeycomb structure is replaced with a circular hole. The honeycomb structure of resin, fiber reinforced resin, paper or metal is attached and wrapped, and then the surface is coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm. There is a method of using the hardened material as a member of the flying body, or a tape of film material such as paper or fiber or fiber reinforced resin is sandwiched between the tapes so that the seaweed roll sushi rolls in a cylindrical shape 1 to 3 atmospheres of pressure were compressed between the tape wound while being wound and the tape to be wound. Gas or gas encapsulated resin encapsulated pressure gas such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 to 33 mm and a thickness of 0.195 to 330 mm is a small crushed egg of several children Or a spherical or polyhedron of a size similar to that of a tennis ball or a volleyball and a chemical fiber or a natural fiber having a tensile force of a fiber shape diameter of about 0.195 microns to 3.3 millimeters Put together a cotton-like object, mix an appropriate amount of adhesive such as epoxy resin, soak in air and stir the gap between the resin-filled pressure gas and the cotton-like fibers. Use a fiber reinforced membrane tape or a commercially available product filled with an appropriate air-containing resin or other adhesive. A honeycomb structure layer made of paper, resin or metal is bonded to the outer surface of the object that is packed between the tape and tape and hardened with air, and is formed by adhering with an adhesive such as epoxy resin. Is used with a thickness of 3.3 to 195 mm coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin, or the structure of the flying object is paper, non-combustible paper, aramid paper or A honeycomb structure of resin or metal was formed into a required shape, and the outer surface of the honeycomb structure was coated and reinforced with fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin to a thickness of 3.3 to 195 mm. There is a method of using an object as a member, or a compressed air or gas of 1 to 3 atm is filled with a diameter of 1.95 mm Resin spheres such as spherical or polyhedral polyethylene terephthalate with a thickness of 0.195 mm to 3.3 mm from rimeter are small crushed egg-like particles such as a number child, and the fiber shape has a diameter of 0.195. Resin by mixing chemical fiber or natural fiber with a pulling force of micron to 3.3 millimeters in size like cotton and mixing with an appropriate amount of adhesive such as epoxy resin and mixing with air. The gap between the products filled with the pressure gas made of cotton-like fibers and the resin or other adhesive material that contains moderately air is formed into the shape of the member, and the adhesive contains moderate air As a result of the consolidation, the adhesive has a shape like an elongated lump of the number of children littered with a white thin film that is an aggregate of the number of eggs. Before curing, it is put into a mold and formed into the shape of the required member, and the outer surface of the cured object containing air is wrapped in a honeycomb structure, and then the surface is 3.3 mm to 195 mm in thickness with a carbon fiber reinforced resin Alternatively, there is a method of using a material reinforced and coated with fiber reinforced resins such as glass fiber reinforced resin as a member, or a central member of a flying object is formed of foamed resins such as foamed polystyrene or foamed urethane, and paper is placed around the foamed resins. Alternatively, a honeycomb structure layer made of resin or metal is formed by bonding with an adhesive such as epoxy resin, and the outer surface of the honeycomb structure has a thickness of 3.3 mm to 195 mm and is made of carbon fiber reinforced resin or glass fiber reinforced resin. Material reinforced with fiber reinforced resins such as compressed air or gas compressed at 1 to 3 atmospheres Encapsulated resin spheres such as spherical or polyhedral polyethylene terephthalate with a diameter of 1.95 to 33 millimeters and a thickness of 0.195 to 330 millimeters can be as small as a small crushed egg or a tennis ball. Adhesion of a moderate amount of a sphere or polyhedron with a size of about volleyball and a cotton-like material made of chemical fibers or natural fibers with a strong tensile force of 0.195 microns to 3.3 millimeters in diameter. This outer surface is a mixture of agents mixed with air and stirred in a spherical or polyhedron gap filled with chemical fiber cotton and adhesive, which is then stirred in with air. A honeycomb structured layer made of paper, resin or metal is bonded around with an adhesive such as epoxy resin. The outer surface of the honeycomb structure is 3.3 mm to 195 mm in thickness and coated with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin, or a honeycomb structure made of paper, resin or metal alone. There is a method to use as a member of the flying body, the above is a description of a material in which the surface of a honeycomb structure made of wood, paper, resin, foam resin, etc. is reinforced with fiber reinforced resin, the above is a light and tough composite material From here on, there is a method of using the above-mentioned composite material as a member of a flying object, which is a description of the safety and structural strengthening of the flying object or aircraft. To prevent lightning strikes, a wire of piano wire with a diameter of 1.95 to 33 mm or steel wire for prestressed concrete is buried. After pre-tensioning, the fiber resin is cured, and the stress is controlled with a computer using a strain gauge or the like on a steel wire for piano wire or prestressed concrete. This method suppresses the aircraft from expanding in the sky by competing with the force that suppresses the pretension bulge that is the pre-tensioning force of the ano wire or prestressed concrete steel wire rod. Or the aircraft structure crashes into the ground and the aircraft's fuselage breaks apart, preventing the piano wire or the steel wire mesh for prestressed concrete from breaking, ensuring a passenger's living space in the event of a crash. Or steel, aluminum, stainless steel, or titanium Or, there is a method using a member made by rolling forging or extrusion of metals such as ultra-lightweight high-performance general-purpose magnesium alloy or using a member manufactured by molten metal lamination forging fixation technology. There is a method using a framework structure of a three-dimensional honeycomb structure such as a wire-ferran structure with a metal such as steel using a molten metal laminate forging fixation technique, which is a description of As in the laminating technology of the above, using a ceramic formwork, the molten metal to be laminated with a mesh shape of about 0.195 mm to 33 mm in height for each layer, etc. The molten metal into which the molten metal to be poured can be extruded and melted by electricity The bottom surface of the ceramic mold that can maintain a high temperature below the point is a mesh with a cross-section of the honeycomb structure that is cut horizontally A chute that drops a layer of molten metal onto the production base horizontally using a ceramic mold with a hopper-shaped ceramic mold with a nozzle-shaped mold. A small amount of metal such as molten steel is poured into the ceramic mold by increasing the pressure of the inert gas and injecting a single layer of the molten metal. The metal, such as drawn molten steel, cools and hardens and adjusts to the degree of striking that the mesh shape is a little thicker for the layered mesh-shaped steel drawn on the production base according to the mesh shape of the ceramic mold The machine-driven computer controlled hammer is forged while maintaining the three-dimensional shape of the mesh to be laminated, but the thickness of the laminate is forged. Assuming that the thickness is corrected to be slightly thicker, a plurality of grooves having a thickness and depth of about 3.3 nanometers to 0.195 millimeters are formed on the upper surface of the forged metal using laser technology. The square side of the cut-off board is 3.3 nanometers to 1.95 millimeters, and the surface of the sea urchin has a diameter of 3.3 nanometers to 1.95 millimeters. 3.3 to 1.95 millimeters from 3.3 nanometers to 1.95 millimeters at intervals of 3.3 nanometers to 1.95 millimeters, and then the laser-processed and drawn ceramic molds give high frequency vibrations. After cleaning the remaining metal residue, the ceramic mold is lowered onto the forged mesh-shaped metal layer, a small amount of molten metal is poured, and press-in injection is performed with an inert gas. After forging by the above method, the tip of a plurality of elongate barbs laser-processed to the above dimensions is poured into the metal in the shape of a grid, and the next part of the barbs is melted by the heat of the molten metal. By biting into and adhering to one layer, a bond between the previous layer and the next layer is formed and fixed.













The upper layer is forged with a machine-driven computer-controlled hammer that adjusts the degree of striking, and the surface is forged with laser technology on the surface. Forged steel such as Weir Ferran structure made of metal such as steel forged by repeating this series of operations to improve the bite with the next molten metal and changing multiple ceramic molds A three-dimensional honeycomb structure made of metal can be obtained, and the conventional lamination technology eliminates the problem that the laminated part peels off like bamboo fiber, eliminating the biting, sticking and forging by sea urchin spines on the laminated surface The method of replacing multiple ceramic molds according to the type of each layer to be laminated in a three-dimensional honeycomb structure is to laminate one unit of the basic structure shape of the honeycomb structure. A plurality of ceramic molds as many as the number of cut planes horizontally cut are connected continuously horizontally to form a strip, and the ceramic molds are moved vertically, front, back, left, right, left and right, and ceramic. After the mold is moved, the molten metal to be laminated is poured onto the substrate, the ceramic mold is lifted, the ceramic mold is cleaned by the vibration of the ceramic mold, and the laminated metal surface is forged. Laser cutting spine processing can be used to automate a series of flow processes by shifting the molding form up, down, front, back, left, and right, or the steel sheet laminating laser melt forging laminating technology can be used for steel meshes like 3D printers. This is a method in which forged formation is performed after laminating the laminated surface using laser technology after laminating metal sheets to be laminated, such as shapes, and so on. The ideal 3D honeycomb structure to be formed is placed virtually, and the virtual 3D honeycomb structure is cut by a horizontal plane in the first stage. A virtual three-dimensional honeycomb structure in the horizontal plane of the second stage is cut horizontally on the first stage, where a sheet of metal such as steel having a thickness of .95 microns to 33 mm is placed on the production base. This is the second stage in which a sheet of metal such as steel having a mesh shape is formed by punching and shearing a sheet of metal such as steel with a thickness of about 1.95 microns to 33 mm in a cross-sectional shape with a punching shear. Along with the mesh shape of the second sheet, the center of the mesh is melted by laser technology and the upper and lower sheets are melted and fixed, and then cooled to an appropriate temperature. It is assumed that the laminated sheet to be forged while hitting with a machine-driven computer-controlled hammer with an appropriate hitting state on a metal sheet such as steel, which has been struck, has been corrected to be thicker on the assumption that it will be forged. On this second stage, punching shears are used to punch a metal sheet, such as steel, with a thickness of about 1.95 microns to 33 millimeters in the shape of a cross section obtained by horizontally cutting a virtual three-dimensional honeycomb structure on the horizontal plane of the third stage. The upper and lower sheets are melted at the center of the mesh by laser technology along the shape of the mesh of this third stage sheet, which is a third stage by placing a sheet of steel or other metal that has been punched and sheared. 3D shape is maintained by hitting the mesh of a metal sheet such as steel that has been melted and fixed and then cooled to an appropriate temperature with a machine-driven computer controlled hammer with an appropriate level of striking. By repeating this forging operation, a series of flow operations that can replace a metal sheet layer while forging a virtual three-dimensional structure can be automated. Three-dimensional honeycomb structures such as Weir Ferran structure, forged with various metals, can be applied to aircraft or large passenger aircraft frame members, etc. This is a description of aircraft design methods and aircraft technology As a design philosophy of an aircraft, the inner skeleton of a passenger aircraft etc. has a lot of cavities inside like a bird skeleton, and the outer shell of the passenger aircraft must be strong to some extent lightweight The passenger aircraft that must be strong crashed with the ground When a skeleton of a three-dimensional honeycomb structure such as a wire-ferran structure in which a metal such as steel that has been laminated and forged inside is forged, is deformed. The framework of the three-dimensional honeycomb structure such as Weir Ferran structure that absorbs and absorbs some energy is processed into a sandwich belt member, and heat insulating materials and fiber reinforced resins are placed outside the framework like an aircraft cage and toward the inside of the framework The belt where the skeleton of the aircraft forming the outer wall of the aircraft while being laminated is knitted The intersection of the belt and belt is cured and fixed using epoxy resin etc. when the aircraft is completed At the time of first knitting into the shape of an aircraft, it is an industrial gel material or honeynite (registered trademark) or foam on the outside of the skeleton of an aircraft-like belt member that is entirely made of straw. Diameter of 1.95 in which compressed air or gas of 1 to 3 atmospheres is sealed with urethane or a resin ball that can withstand changes in atmospheric pressure above and above the ground. A product filled with pressure gas made of resin such as spherical or polyhedral polyethylene terephthalate with a thickness of 0.195 mm to 330 mm is about the size of a small crushed egg or a tennis ball. A ball or polyhedron with a size of from about volleyball to a polyhedron and a cotton or other chemical fiber or natural fiber with a pulling force of about 0.195 microns to 3.3 millimeters in diameter. Mix an appropriate amount of an adhesive such as epoxy resin, mix it with air, and stir it. The gap between the resin-filled pressure gas will be filled with cotton-like fibers and an adhesive such as resin containing appropriate air. When a resin ball that uses a material filled with shock absorber as a shock absorber crashes due to a collision with the ground, it may break A shock-absorbing material that absorbs more energy is attached to the outside, and the outer wall of the fiber-resin is the outer wall of the shock-absorbing material. This skeleton belt that protects the safety of passengers is a collective steel manufactured by a method in which metal wires such as piano wires or prestressed concrete steel wires are bundled in parallel like the muscle fibers of the outside There is a method of knitting like a hand-knitted sweater with wire rod or wire rod, and the inside of the metal honeycomb structure and the fiber reinforced resin honeycomb structure that are used separately according to the application are like the hard part and the soft part of the turtle shell A stretch of belt that is a bamboo-like skeleton that weaves a strong and strong belt member arranged in a balanced manner. There is a method in which the wires are bundled in parallel, and there is a method in which the wire is knitted like a hand-knitted sweater. There is a method of wrapping the wire so that the rheology body does not leak with the mantle film.There is a method of replacing the fatigue fracture of the wire with a fiber reinforced resin, that is, a wire such as steel bundled in a bundle This is a method in which a wire knitted like a hand-knitted sweater is housed in a fiber reinforced resin. The honeycomb structure in which the honeycomb material is used for the inner part of the belt that receives compressive force with the braided wire rod surrounds the section of the metal honeycomb structure The honeycomb structure of the resin surrounds the turtle shell, and I want to see the turtle shell here.A soft growth layer surrounds the hard hexagonal shell around the turtle-shaped hard hexagon shell and the honeycomb structure The combination of this rigid and flexible honeycomb structure allows the belt member to bend slightly but flexibly and, like an H-shaped steel, the mantle can withstand alternating stresses of compression and tension Inside, the rheology body and steel wire material, then the fiber reinforced resin base material, then the rigid and soft honeycomb structure, then the fiber reinforced resin base material, then the steel wire material and rheology body are encased in the mantle. The belt member becomes a more mechanically advantageous and easy-to-use material by the method in which the honeycomb structure is sandwiched with a wire material such as steel from both sides. The rheological body of a sandwich belt member, which will be referred to as a Dutch belt member, has a method of replacing it with a fiber reinforced resin. When describing a belt member in the claims, it mainly refers to a sandwich belt member. The skeleton of an aircraft made of bamboo fences is created Inside the fence is a wide cavity, especially the fuselage, both wings and tail are all like mechanical aircraft made of bamboo fences as a mechanical structure The stiffening knitting method that connects the fuselage, both main wings, fuselage, and tail wings is woven so that the stress is distributed in a distributed manner and the fatigue of repeated loads is withstood, as if looking at a delicate bamboo craft. This method, which is designed to balance the entire aircraft, is like paper on a bamboo skeleton like a Nebuta Festival float A special fiber reinforced resin is encased in the outermost fiber reinforced resin, and a piano wire or prestressed steel wire is pre-tensioned (a technology that pre-tensions the steel wire and then hardens the fiber reinforced resin). The outermost skin is made of fiber reinforced resin with a mesh of piano wire or prestressed steel wire in the center so that it does not break into fine dust at the end of a crash. As described for safety, the fiber reinforced resin sandwich structure with the shock absorber sandwiched around the heel skeleton, so the energy of the collision is the order of the fiber reinforced resin outer wall shock absorber 籠 shape skeleton shock absorber fiber reinforced resin inner wall However, the conventional aircraft has a rigid skeleton and a brittle outer skin to reduce the weight of the aircraft. The method of the present invention is a design method that goes from the center to the outside, but the design method of the conventional aircraft that wraps passengers from the outside in terms of structural dynamics from the outside to the inside absolutely respects human life rather than the economy As an application of the sandwich belt member, the sandwich belt member 籠 exoskeleton spherical flying object is composed of a spherical passenger part with a head part, both wings and tail part, and is about the size of a jumbo jet (registered trademark) The wide space inside the spherical shape is used for multiple purposes, and it is possible to construct a plurality of floors by supporting the honeycomb structure floor with the ridge-shaped walls and floors. As an application of a sandwich belt member that is used for multiple purposes, a flying object that simulates a thick flying fish simulates a large flying fish with a skeleton-like exoskeleton. The flying object has a rounded body like a goldfish and the thick wings are structured like the cross section of the wing according to Bernoulli's theorem, and the upper and lower air pressure difference creates lift In the tail of this squadron, the forced air-cooled whole heat radiating fiber reinforced resin metal composite internal combustion engine is used to obtain the rotational force to generate the forced air cooled whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor Forced air-cooled whole heat-dissipating fiber reinforced resin-metal composite rotor permanent magnet stator Electric coil disk laminating generator is used to obtain power, and then the bird strike prevention device fiber-reinforced resin metal composite turbine laminating electric motor A flying object simulating a thick flying fish can be moved forward by sending the wind backward with a forced air cooling whole heat radiation fiber reinforced resin metal composite Combined internal combustion engine angular momentum adjustable flywheel torque converter clutch forced air cooling overall heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacked generator motor output power transmission integrated hybrid device A large internal space that can be managed by a computer is partitioned by a wall-shaped wall, floor, or honeycomb structure knitted with a sandwich belt member and can be used for multiple purposes. Bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor attached to both wing tip, horizontal tail tip and fuselage tail of flying object is an application of sandwich belt member that can obtain strong driving force. The center of the sphere is a sphere and the outer periphery of the sphere is a disk shape. Tophan internal-combustor generator combined disk outer periphery part wing shape Koba Sora dance fall fall mitigation parachute installation fuel generator ballast hanging dropable flight object is the outer periphery of the disk part where the exoskeleton of the flying object is knitted by the sandwich belt member The parts are blown down by multiple duct engines and floated













In order to obtain buoyancy, the disk part is expanded left and right, and multiple ducts and engines can be arranged radially on the concentric circles of the disk. The part where the wind hits the traveling direction of the disk is processed into a wing shape The engine has a cross-shaped beam in the middle of the cylindrical height, two rotary engines above and below the center of the cross, or two zero-type fighter aircraft Sakae engine twin-engine horizontal piston simulated forced air cooling overall heat dissipation Engine exhaust in which two propellers or fans fixed on the shaft of each internal combustion engine that fixes the fiber reinforced resin-metal composite internal combustion engine at the center of the cross beam are duct fans that rotate inside a cylindrical shape Between the upper and lower internal combustion engines in the cylindrical duct of the disk, which is taken into the silencer in the disk and purified through a ceramic filter and exhausted from the lower surface of the disk Air-cooled overall heat-dissipating fiber reinforced resin metal composite rotor permanent magnet stator Electric coil disk stacked generator is installed to obtain power at the same time as buoyancy There is a method of propelling in the traveling direction with that power Because of the levitation force, a long runway is not required, and four bird strike prevention devices fixed on the boundary between the spherical surface and the disk with respect to the direction of travel of the sphere. The left and right and up and down posture control is performed by the difference in the four outputs of the four motors in the forward direction that feed forward, and the rough vertical change is controlled by the difference in the output of the duct engine. There is also a method of extending both wings to the left and right, and it is possible to attach aileron to the wings and control the pitch This is like a big ray flying in the air Four bird strike prevention devices that obtain buoyancy with the duct engine described in the claims of the present invention Fiber reinforced resin metal composite turbine laminated electric motor with forced air cooling Whole heat radiating fiber reinforced resin metal composite internal combustion engine Adjustable angular momentum Spiral wheel torque converter clutch forced air cooling overall heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk laminated generator motor output power transmission transmission integrated hybrid device combined with a spherical center circumferential disk to obtain propulsion Four bird strike prevention device fiber reinforced resin metal that stabilizes flight by extending the tail sharply from the disk like ray, which also includes ray simulated flying object simulating deformed ray shape Obtain the buoyancy of the blades as the forward speed is obtained by sending the wind backward with the composite turbine stacked electric motor The vertical duct of the disk is configured to reduce the burden on the duct fan by forced air cooling overall heat radiation fiber reinforced resin metal composite Internal combustion engine angular momentum adjustable adjustable wheel torque converter clutch forced air cooling overall heat radiation fiber reinforced resin metal composite Rotor Permanent Magnet Stator Electric Coil Disc Stacked Generator Motor Output Power Transmission Transmission Integrated Hybrid Device The energy can be comprehensively managed by the computer. This parachute with multiple chutes is opened when it falls, and when it falls it pulls the mouth of the upper part of the parachute with a wire to induce the fall of the spherical disk, so that the ground and the leaves fall down in the air Ballast ballast with heavy objects such as generator fuel tank at the bottom of the spherical shape to ease the clash It has a structure that can be hung up and down like a tank and can be put in and out, and when the airflow is bad, hang down the heavy parts such as the generator and fuel of the ballast and lower the center of gravity to prevent the whole disk from rotating to the top This ballast part has a structure that can be dropped separately from the spherical disk body in a safe position to reduce the weight in the event of falling, and the bottom part around this suspendable ball is cut off The lower part of the sphere is provided with a shock absorbing layer, and the inside of the sphere, which reduces the impact when falling, is partitioned by a wall or floor made of sandwich belt members or a honeycomb structure plate. Fuel that is used for multiple purposes safely and comfortably, and has a structure that can transport about 900 people in a single flight without crashing the aircraft by crashing into the ground in the event of a crash Or, light oil or gasoline can be used, and exhaust gas passes through a muffler with built-in catalyst, so if it falls on the sea to mitigate calm air pollution, a float like an air bag will swell from the bottom of the disk part, but this spherical disk is originally Is a watertight and airtight structure that floats on the water, and in the event of a crash, it swells like an air bag and softens the impact of the crash. Above is the description of aircraft design method and aircraft technology, which is functionally the same as above. From now on, it is a description of lamination technology. Draw a figure using the fine wire of the metal and charge the metal thin wire as an electrode. The crucible lid in the shape of a crucible flask is brought into close contact with a stopped ordinary crucible to prevent the entire vapor deposition material from diffusing. The electrode for charging the vapor deposition material in the crucible is the melting surface inside the crucible or inside the crucible. The nozzle is formed into a target figure with a different potential so that vapor deposition does not occur in the nozzle having the same potential of the vapor deposition material through the conduit having the reverse potential of the vapor deposition material through the conduit having the reverse potential of the vapor deposition material. There is a method to drift the nozzle from the movable conduit by the diffusing force to evaporate and the electrostatic transport to reach the target electrode from the nozzle by moving the crucible flask shape crucible like a three-dimensional printer and the third shape of the crane neck flask shape Like the original printer, it is selectively and intensively lowered from the nozzle-shaped vapor deposition material outlet at the tip of the crane neck so that it does not scatter to other parts. Vapor deposition is controlled according to the shape of the electrode of the thin wire that is charged by concentrating and depositing the vapor deposition material, which is managed by a device such as a camera shutter, on the target fine wire at the top by electrostatic force The three-dimensional shape is formed by the vacuum deposition material or the method of using conductive ink instead of the target thin line is to draw the deposition target figure like a three-dimensional printer and charge the figure to the figure. By vacuum-depositing in a manner and drawing a figure to be laminated like a three-dimensional printer on the target figure so as to laminate further, charging the figure and intensively vacuum-depositing from the top on the top figure to repeat this process Laminated three-dimensional structures can be formed by vacuum-deposited materials, or the method using silver clay technology for three-dimensional lamination can be applied to paper or resin fiber nonwoven paper. Or use a water-soluble air contact curable curing agent and a fine powder of metal that you want to laminate with an ink that contains a mixture of fine powders, or a figure that you want to laminate on a non-woven paper that is placed on a production base. Like the original printer, draw another piece of paper on the figure you want to layer and draw like a three-dimensional printer. The curable ink containing fine metal powder penetrates between the fibers of the paper. Adjust the amount of ink to the extent that the ink on the upper paper and the lower paper are compatible, and draw a figure with a printer like a three-dimensional printer Curability containing metal fine powder you want to stack paper on this paper Drawing a figure with the ink of the above is repeated to obtain a paper or resin fiber non-woven paper which is laminated and cured to burn the paper or resin fiber non-woven paper in a sintering furnace to sinter bond the metal to form a three-dimensional structure Obtain paper or resin fiber The purpose of using non-woven paper is to shorten the lamination time, ensure the width of the ink, and smooth the surface of the method of three-dimensional lamination, and print multiple spot-like dots at fixed positions around the figure to be laminated When the paper bundle is cured, the point cloud is stacked and cured in a columnar shape until the laminated paper bundle is sintered and the shape is protected and the cured paper bundle is easily transported. Assuming that the three-dimensional structure shrinks, the size will be corrected and the laminated figure will be drawn. The above is the description of the new three-dimensional lamination technology, and here is the description of the structure of the flying object Certain aircraft structures are made of resin, carbon fiber reinforced resin, glass fiber reinforced resin, fiber reinforced resin such as Kevlar fiber reinforced resin, or a combination of these metals, resin or fiber reinforced resin materials. Or use Use a layer of metal and resin layers layered together with a layer of xy-resin, or use a combination of fiber materials such as aramid fibers, or use a fiber material in a belt shape. Use a braided material hardened with resin as a member for knitting the heel structure, or use a material that is extruded and sealed with metal or a resin that is press-fitted and sealed inside a material that gathers thin metal pipes Or use a honeycomb sandwich structure in which both sides of the honeycomb structure plate are sandwiched between plate materials such as fiber reinforced resin and bonded with an epoxy resin, or a honeycomb structure / plate material / honeycomb structure / plate material Carbon fiber reinforced resin or glass fiber reinforced resin is used for the outer surface of three-dimensionally machined products that are alternately stacked in layers using a milling machine. There is a method of using as a member a material reinforced by covering and reinforcing with a fiber reinforcing resin with a thickness of 3.3 to 195 mm, or a weir ferran structure that forms a weir ferran structure like a panel is a honeycomb structure There is a method to form a panel shape using a weir ferran structure which is a three-dimensional structure by bonding polygonal members that are the basic structural structure of epoxy resin, and using a fiber reinforced resin plate Thickness 3 on the outer surface of a sandwiched structure or an object obtained by three-dimensionally cutting a structure in which these layers are alternately laminated with a milling machine or the like with a fiber reinforced resin such as a carbon fiber reinforced resin or a glass fiber reinforced resin. There is a method of using a material which is hardened by covering and reinforcing at 3 to 195 mm as a member. Shaped members are assembled according to the flow of stress in the cross section and bundled together with an epoxy resin between the pipes to prevent stress concentration. A flexible and highly viscous mucous layer that absorbs the energy of possible fatigue rupture is provided with a rheological layer such as a muscle-tendon relationship. Stress by providing a rheological layer, such as a muscle-tendon relationship with flexible and highly viscous mucous properties, that absorbs the energy of fatigue breakage in the gap between the laminate and the non-compressed membrane assembly rather than the compression material A three-dimensional honeycomb structure that spreads the concentration in each part of the assembly to prevent the progress of fatigue fracture and has a mechanical balance, or a combination of these layered hierarchical structures and a three-dimensional aggregate structure. This composite structure can also be used for aircraft, using a composite structure or a layered structure object that is bonded with an epoxy resin using a three-dimensional aggregate structure object that prevents fatigue failure in the compression part. Passengers when a vehicle or aircraft crashes into the ground by providing a layer of rubber shock absorbers, or 195 to 330 millimeters in thickness, between 1.95 and 3.3 millimeters thick, between these composite structural walls. The shock absorbers sandwiched between the wall and the center of the wall that secure the passenger's living space by reducing the impact energy to the inside enclose air like a balance ball, rubber, resin, Kevlar fiber, silk, cotton fiber, chemical Shock absorbers are made using fibers or a combination of these. The above is a description of the structure of the aircraft. Or, the description of the aircraft safety and structural strengthening, the personal aerial work flying object is composed of the upper flying body and the lower suspension body, the upper part corresponding to the fluff (crown) part of the dandelion as its configuration form The flying object uses a method of using an electric motor, a method of using an internal combustion engine, a method of using a balloon, a balloon and an electric motor, or an internal combustion engine, or an electric motor, an internal combustion engine, a generator, and a balloon to obtain a lifting force. The description of the composite device divided into the composite device method is as follows. The balloon is divided into the hot air balloon, gas balloon or hot gas combined balloon method. This hot gas technology used in the following ice cream cone-type aircraft, including the method of enclosed sealed hot gas balloons that are used by heating The method of using an electric motor for the upper aircraft, which is also used for airships, is a gyro that stabilizes the upper aircraft, a parachute that can be used manually or automatically for emergency methods, and a blower to obtain lifting force in the upper aircraft. From here, the propeller or fan

The blower that is the description of the manufacturing method is a propeller or fan that is made by processing solid wood according to the description of the above composite material and cutting or pouring resin into the mold, titanium, aluminum, stainless steel, ultra-light, high-performance, general-purpose It consists of a metal such as magnesium alloy or carbon fiber reinforced resin or a material that is a combination of these materials. The method of compounding the materials here is propellers or fans that are perpendicular to the blade rotation direction, that is, from the shaft to the outer periphery. In the direction along the flow of the stress in the cross section in the radial direction, hollow pipe materials with a diameter of 0.195 mm to 3.3 mm are collectively arranged and the epoxy resin or the like is solidified by cutting such as a milling machine or laser technology , Scanning Electron Microscope Technology, Tunneling Effect and Atomic Implantation Using a molecular manipulator that combines a chipping technique, a molecular insulator and a molecular beam, or a nano-robot such as a ribosome that automatically transports and manufactures molecules, the molecules are assembled and arranged in three dimensions according to the molecular structure design method. The three-dimensional printer atomic layering technology at the level (can be used for room temperature superconducting material manufacturing, especially ceramics), using the technology to construct the molecule itself, a three-dimensionally formed in the shape of a propeller or fan blade, the inside of the pipe is hollow Another composite method that is tough because it is a collection of thin pipe materials with a light weight and at the same time a concordant (arrangement of suitable materials according to mechanical characteristics) along the flow of stress Laminate paper, resin, and metal honeycomb structures and use a milling machine or other cutting machine to stand in the shape of a propeller or fan blade. The outer surface is formed with a thickness of 3.3 to 195 mm and coated with fiber reinforced resin such as carbon fiber reinforced resin or glass fiber reinforced resin, and another composite method is that the fiber material is subjected to stress in the radial direction. The propellant or fan shape is formed in the direction along the flow and then the resin is poured between the fibers and hardened. The lifting device of the upper flying body is strong against rotation. The above is the manufacturing method of the propeller or fan, which is composed of the motor, and here is the description of the light and powerful electric coil and the forced air blowing overall heat dissipation, there is a method that uses a commercially available electric motor, but a new fiber Reinforced resin electric motors use copper, gold, or room temperature superconducting materials such as conductive wire enamel, glass fiber reinforced resin, or conductive surfaces. A superconductor that prevents melting by heat through a wire coating material such as an Mick-processed method or a glass-finished product, or a pipe whose center is the shape of the wire, and the inside of the wire of the wire is forcibly air-cooled or water-cooled, or liquid helium or liquid nitrogen Conductive coils, steel, aluminum, titanium, ultra-light, high-performance, general-purpose magnesium alloy, or other metals, or carbon fiber reinforced resin, or combinations of these, the electromagnetic part of the electric motor can be made of metal and carbon fiber. The method of forced air cooling, in which a blade forcibly air-cooling with a small blade that forcibly blows air to the coil of a lightweight and strong electric motor in which the structural material is replaced with a fiber reinforced resin, is built directly into the electric motor and the coil is forcibly air-cooled. Method of forced air cooling from the inside of the pipe of the electrical lead The fiber reinforced resin that forms the structure of the electric motor has a plurality of small holes with a diameter of 0.195mm to 3.3mm, and heat radiation is released by releasing hot air from the entire electric motor. The upper flying object is arranged in a hierarchical manner with a plurality of brushes made of a composite material considered, or a plurality of brushless electric motors, or a plurality of electric motors combining these brushing motors and brushless motors. The above is a description of the lightweight and powerful electric coil and the forced ventilation overall heat dissipation. The upper air blower is a fan motor integrated type with a fan and motor integrated, or the air blowing direction of the air blower or air blower is upward And the exhaust also includes the method of the duct fan that is adjusted downward or the fan is in the duct, And the lower suspension body corresponding to the seed of dandelion is constructed so that humans can freely work in the air, such as carrying humans or hanging up and allowing them to work in the air. The upper flying body is divided into a method of stacking honeycomb structures such as a honeycomb sandwich panel or a weir-ferran structure panel, a method of collecting cocoon-shaped objects, or a method of combining pipe structures, honeycomb structures and cocoon structures. The method of using a pipe structure to form a framework as a structure is based on a method of assembling and fixing a pipe member and fixing with a fixture and fiber reinforced resins such as carbon fiber reinforced resin or glass fiber reinforced resin. There is a method that is integrally formed by autoclave formation, etc. that is baked under pressure in a large kiln at a factory. There is a method of forming the outer shape of the upper flying body by keeping the outer shape in the range of width and depth of about 195 to 3300 mm and height of about 195 to 3300 mm, and the inside with a hollow or a framework. The appearance shape of the upper flying object is a sphere or donut shape, that is, an annular surface, an annular body, a spheroid, a spheroid, a rotation quadratic curve, a rectangular parallelepiped, a cube, a polyhedron, a polygonal column or a cylinder of this size, or A shape in which a plurality of cylinders are connected horizontally, a cone shape, a method of using a truncated cone or a quadrangular pyramid alone, and a combination of these three-dimensional shapes, and a cone shape with the top apex of the cone shaped downward, Or on the upper and lower surfaces of a cylinder that looks like a sharp pencil A shape with a conical bottom connected, or a shape with a conical bottom connected to the lower surface of a cylinder shaped like the bottom end of a short pencil, or the larger bottom of a truncated cone like a large abacus ball A method of forming a solid with the shape of each other and using it alone, or a method of using this large abacus ball connected vertically, or connecting spheres vertically, or connecting a sphere or spheroid to a large grape bunch Or the shape of the aggregate using a combination of a cylinder and a conical solid and a sphere or spheroid, the upper aircraft is a method of assembling pipes, The framework of the horizontal member, the vertical member, the propeller or the fan guard member is a metal wire such as stainless steel wire or piano wire or The member is wound around the joint part from 3 to 33 times with a wire material of 0.195 mm to 3.3 mm in diameter, such as fat, chemical fiber, or carbon fiber reinforced resin, and is knotted from above the knotted wire. Fixtures that have a method of bonding with epoxy resin or bonding with epoxy resins, rigid bonding by welding between resins or metals, or fixing with aluminum screws or fixing tools are steel clips, resins or carbon fibers This is an assembled method combining reinforced resin and glass fiber reinforced resin. This is a method for aerial work or flight leisure by fixing a detachable member to a rigidly connected member with a detachable fixture that facilitates disassembly. The horizontal member of the upper flying object can be assembled quickly and easily and easily for personal aerial work flying objects on site. It is divided into a horizontal member, a horizontal member for attachment and detachment, and a horizontal member for propeller or fan guard, the vertical member is divided into a central vertical member and a peripheral vertical member, and the upper aircraft is detachable to fix the electric motor so that it can be assembled and disassembled The horizontal member is rigidly connected to the vertical member by passing the removable horizontal pipe through the pipe so that the central vertical member is in the middle of the horizontal member. Fixing the horizontal member and the detachable horizontal member and then fixing the electric motor to both ends of the detachable horizontal member, or fixing the electric motor first to one end of the detachable horizontal member and then fixing the electric motor Two detachable horizontal members which are inserted into the center of the central vertical member and fixed with a fixing tool inside the rigid horizontal member having an end different from the end of the detachable horizontal member rigidly connected to the vertical member. The There is a method of butting at the center of the center vertical member or a method of inserting a removable horizontal member with an electric motor fixed into the rigid horizontal member of the central vertical member like a cantilever, or for attaching and detaching to fix the electric motor The horizontal member is divided into two methods: a method using a pipe member alone, or a method for assembling a detachable horizontal member supporting an electric motor into an annular structure, that is, a method using a detachable horizontal member alone or an annular structure. The shape of the horizontal members stacked in multiple layers, as seen from above, is the cross shape of the same side, the star shape of David (hexagram), the pentagram or the ten-valve, the twelve-valve, the ten-valve. A polygon and a diagonal line with different shapes and sizes are combined inside a polygon that combines a triangle and a diagonal line inside a polygon such as a six-valve, thirty-two valve chrysanthemum pattern, or an octagon. There are methods that have the shape of eyes or squares, these shapes can be disassembled and assembled, and these various structures can be shifted by shifting the horizontal position or shifting the vertical position from aerodynamic considerations. Combined so that fans do not contact each other and stacked in layers so as to be stacked in the vertical direction, a horizontal member with the same side as a horizontal member, or a polygon that combines triangles and diagonal lines inside a polygon such as an octagon Due to the interference of winds aerodynamically blown horizontally and vertically so that multiple propellers or fans do not hit each other on a horizontal member with a combination of polygons and diagonal lines inside Considering the thrust of rising and the stability balance of the flying object, the flow is arranged while slightly shifting the position in the horizontal and vertical directions. The part flying body is structured to increase the thrust in the upward direction by laminating horizontal members of this equilateral cross shape or a combination of polygons and diagonal lines inside the polygon, the vertical member is the central vertical member And the peripheral vertical member and the fixture described in the claims, the central horizontal member is rigidly connected to the pipe of the horizontal member for rigid connection by screwing, welding, adhesion with epoxy resin, etc. The connecting part is reinforced by a plate member or rib member. The shape of the central vertical member is a prism or cylinder, or a three-dimensional girder structure that combines a horizontal member and a vertical member, or a rectangular pyramid that is elongated like a steel tower by combining a horizontal member and a vertical member. There is a method in which horizontal members of branches grow or a combination of these shapes in the circular structure of the ring, and the method in which the central vertical member is a prism is the cross section of the central member in the Kanji mouth or rice field Aluminum having a side of 33 to 66 millimeters in the vertical direction and having a length of about 195 to 3300 millimeters, carbon fiber reinforced resin, glass fiber reinforced resin, resins, foamed resins, or these materials There is a method of using an equilateral square pipe that is a single piece or a combination of materials, and the meaning of combining this material is to pour urethane foam or carbon fiber reinforced resin into the mouth of the Chinese character of the aluminum pipe or the hollow part of the cross section of the rice field The method of the central member of the cylinder, including the method of curing in the above, is a waterproof paper or paper tape having a diameter of 66 mm to 99 mm, a thickness of 1 mm to 6 mm, and a length of 195 mm to 3300 mm. Cylindrical shape The cylinder is made of a single material or a combination of a single material or a combination of a wound material, a composite material wound with the above membrane material, or aluminum, or a carbon fiber reinforced resin, a glass fiber reinforced resin, or a material made of the composite material. The meaning of combining vertically means to include a method of pouring foamed resin or carbon fiber reinforced resin into the hollow part of an aluminum cylindrical pipe and curing it, and drilling holes on the sides of these prisms or cylinders, vertical members Insert the pipes of the horizontal members for rigid connection into prisms or cylinders in order from the east, west, south, north, or eight directions so that the branch is perpendicular to the central member. A member made of wire with a diameter of 0.195 to 3.3 mm, such as metal, resin, chemical fiber or carbon fiber reinforced resin An upper flying object that is wound around the joint part 3 to 33 times around the joint part, and is rigidly joined with an epoxy resin from the top of the wire part, or screwed, welded or bonded with epoxy resins. From the top to the bottom of the tree
The shape of the character rack












Cylindrical center vertical material is a structure in which polygons and diagonal shapes combined in a polygon are stacked in multiple stages. The horizontal member and center vertical member for rigid connection are made of metal or resin. The material is wrapped with the wire material of 0.195mm to 3.3mm in diameter, such as chemical fiber and carbon fiber reinforced resin, around the joint part 3 to 33 times. The solid vertical girder center vertical member method is made of aluminum, which is rigidly fixed with a resin-solidified object or aluminum welded or epoxy resin or aluminum screw to rigidly fix the horizontal member and vertical member for rigid connection. Using carbon fiber reinforced resin, glass fiber reinforced resin, or a combination of these, a square cross section with a side of about 10 mm and a thickness of 1.5 mm. The center part of the horizontal member for rigid connection is sandwiched with four equilateral square pipes with a length of about 195mm to 3300mm in the vertical direction so that it has a cross-girder structure, and is rigidly connected with screws, welding, epoxy resin bonding, or fixtures. The vertical center member and the horizontal member are rigidly assembled and rigidly assembled so as to form a three-dimensional cross girder, and a horizontal member for detachment is inserted into the rigid horizontal member pipe and fixed with a fixture to constitute the upper flying body In order to facilitate the assembly and disassembly of the upper flying body, the horizontal member for rigid connection has a socket structure for inserting the horizontal member for fixing the electric motor. The method of inserting the horizontal member for use and the method of attaching the ends of the horizontal member for attachment / detachment at the center of the center vertical member and the end of the attachment / detachment horizontal member of the center vertical member as in the case of a cantilever It is divided into three methods that can be stopped by the heart. The method of the ring structure with a vertical center member that is elongated like a steel tower is stiffened at the center so that the compression member does not buckle like the steel ring structure. In order to obtain a propulsive force for ascending inside the upper aircraft, a plurality of propellers or fans of about 16 to 36 and a plurality of Electric motors are arranged in multiple stages. This arrangement method uses aluminum screws or the like to fix the electric motor base to the base of the detachable horizontal member. The electric motor and prober are targeted at each position of the horizontal member. The multiple propellers or fans inside the upper flying object are balanced by reversing the rotation direction of each propeller or fan at the target position, and the individual aerial work flying object is in the air The upper flying machine's horizontal members are 15mm to 30mm wide, 15 to 30mm high and 1.5mm thick From 3.3mm to 195mm to 3300mm in length, made of aluminum, carbon fiber reinforced resin, glass fiber reinforced resin, Kevlar fiber reinforced resin pipe, or a combination of these. The horizontal member and vertical member are rigidly connected while strengthening the necessary parts by welding the aluminum member, aluminum stiffening plate welding of the horizontal member and vertical member, and aluminum rib reinforcement welding. , Carbon fiber wire or netting, carbon fiber tape, carbon fiber reinforced A propeller or fan guard that is reinforced with a resin, glass fiber reinforced resin, or Kevlar fiber reinforced resin, and a detachable propeller or fan guard member is inserted into the tip of a detachable horizontal member to which an electric motor is fixed. The material of the member is resin or carbon fiber reinforced resin, glass fiber reinforced resin, chemical fiber, Tegs, stainless steel wire, wire or a combination of these, this propeller or fan guard member is a flying object for personal aerial work The propeller or fan guard member prevents the damage of the propeller or fan when it comes into contact with other objects. The pipe also includes a fan motor or blower method in which a duct fan and motor are integrated into a cylindrical duct. The structure of inserting a pipe into the A horizontal member, a vertical member, a propeller, a fan, or a fan motor or fan guard member in which a fan and a motor are integrated, which also serves as a body reinforcement, is subjected to buckling of the pipe in the pipe cavity. There is a method to reinforce the pipe by encapsulating and curing foamed resins for the purpose of preventing this, making the upper aircraft lightweight and robust, the pipe is made of the above composite material, the structure that assembled the pipe is the most Simplified method, width 15mm to 30mm, height 15 to 30mm, thickness 1.5mm length 195mm to 3300mm about non-equal or equilateral angle aluminum or carbon fiber reinforced resin, glass fiber reinforced Elongated ladder using resin pipes or a combination of these The shape of the shape of a birdcage or the frame of a jungle gym is an object included in the method of assembling by fixing a pipe with a fixture. The method using a honeycomb structure for the upper flying object is 1.95 mm in diameter made of resin or paper From 33mm to 0.195mm to 3.3mm thick cylindrical pipe is assembled and cured with resin to produce a honeycomb structure, and a honeycomb sandwich panel or via-ferran structure panel with a plate attached to both sides of the honeycomb structure. The honeycomb structure in this claim, which is divided into a method of stacking honeycomb structures, is a hexagonal honeycomb structure, an OX structure, a flex structure, a bisecting structure, a feather structure, or other various shapes, and adhesives and brazing Material or 3D lamination technology A laminated structure is created using three-dimensional cutting. The material of the honeycomb structure in this claim is paper, non-combustible paper, metal such as aluminum, titanium, stainless steel, aramid paper, carbon fiber reinforced resins, or glass fiber reinforced. Fiber reinforced resins such as resins, or a honeycomb structure panel such as a combination of these and honeycomb structure panels such as weir ferran structure panels, which have hollow holes with diameters of 330 mm to 990 mm for propellers or fans horizontally A honeycomb sandwich panel is a vertical member of a pipe made of aluminum, carbon fiber reinforced resin, or glass fiber reinforced resin, on which a honeycomb structure panel such as a honeycomb sandwich panel or a weir ferran structure panel is laminated. Or by stacking and connecting honeycomb structures such as weir ferran structure panels in multiple stages, such as honeycomb sandwich panels or weir ferran structure panels, like the internal structure of a honeycomb layered vertically in multiple layers The upper aircraft is composed of the shape of the upper aircraft combined with the shape of a rectangular parallelepiped, cylinder, disk, donut, etc. The upper aircraft is a honeycomb sandwich panel or via ferran when viewed from the top in the horizontal direction. In order to take in air from the periphery of honeycomb structures such as honeycomb sandwich panels or weir ferran structure panels, which are used in a direction that can withstand the load when rising and falling in the vertical direction, where hexagonal aggregates of honeycomb structures such as structural panels can be seen Product with spacing of millimeters to 330 millimeters A fan motor or blower in which holes having a diameter of about 330 mm to 990 mm are formed by closely laminating and stacking honeycomb structures such as a layered method or a honeycomb sandwich panel or a weir ferran structure panel, and a duct fan and a motor are integrated. In order to reinforce a honeycomb structure such as a honeycomb sandwich panel or a weir-ferran structure panel, a pipe made of aluminum, carbon fiber reinforced resin or glass fiber reinforced resin is used as a horizontal member or vertical member. The hexagonal column of the honeycomb sandwich panel made of a honeycomb structure material having a side of 19.5 mm to 330 mm and a thickness of 19.5 mm to 330 mm is used. An electric motor and propeller or fan or fan and motor are installed in a space where a hole of 330 mm to 990 mm in diameter is formed above and below the cave and a fan motor or a fan in which a duct fan and a motor are integrated. Including the method of laminating a honeycomb sandwich panel in which a fan motor or a blower in which the fan is integrated is laminated, and the word "belt member" is used for the upper flying body as a belt-like member, that is, a member for knitting a ridge in this patent claim. The method of assembling cocoon-shaped objects formed by weaving sandwich belt members, which means the sandwich belt member defined in the section, is assembled using a plurality of bamboo baskets formed by weaving bamboo belts. Aluminum and carbon fiber reinforced resins Weaving bamboo with a belt-shaped member made of a composite material that combines flexibility and toughness, like a bamboo material, which weaves bamboo bamboo using a sandwich belt member formed by combining glass fiber reinforced resins and resins. The belt member for knitting the heel used for the material is a metal such as aluminum or titanium having a thickness of 0.33 to 1.95 mm, a width of 3.3 to 19.5 mm, or a carbon fiber reinforced resin, a glass fiber reinforced resin or a resin. Thickness 0.33 to 1.95 mm width 3.3 to 19 centering on a film made of a laminated belt, and a carbon fiber wire knitted like a knitted yarn and belted with an epoxy resin. .Bamboo-like belt knitting bamboo baskets sandwiched between 5mm aluminum bands like sandwiches and bonded with epoxy resin There is also a method of using a composite object of shape as a material for knitting the cocoon. The cocoon is a combination of these cocoons that woven bamboo-shaped composite members of bamboo cocoons into various shapes to form a three-dimensional shape and knitting the cocoon The belt is bonded to the belt at the intersection of the belts with an epoxy resin. The entire collar is tough and supple, and the collar has a diameter of 1 so that it can be restored even if the collar structure is slightly deformed. It can be processed into various shapes like bamboo baskets reinforced with rods or pipe materials that are a combination of aluminum and carbon fiber reinforced resins, glass fiber reinforced resins and resins of millimeters to 5 millimeters. A sphere-shaped method that combines the shape of the colander and the shape of the colander, the earth's equivalent to the equator on the earth can be assembled and disassembled with a fixture, that is, a bamboo sphere hemisphere A semi-circular braid knitted in a hemispherical shape with a sandwich belt member in the shape of a half-shaped Shimazu clan's family crest in the middle and sandwiched up and down in a hemispherical shape, An electric motor and a prepeller or fan are installed in the center of the cross beam of the object shaped like the family crest of the Shimazu clan in the shape of the figure. The upper and lower hemispherical cicada members and the crest of the Shimadzu clan in the center circle Such a member is fixed with a fixture and can be easily assembled and disassembled like a spherical bamboo basket with an electric motor and a propeller or fan installed in the center. Like a wheel motor, there is a method in which the rotor is a disk-shaped wheel and the wheel becomes a propeller or a fan motor or fan that combines a fan and a motor with a motor. The manufacturing method of the fan motor or blower is four, eight, twelve, sixteen, or thirty-two pieces by cutting radially from a location 33 mm away from the center of the disk and bending it into a blade shape. The fan and motor are integrated into a fan motor or blower shape, or a ring-shaped member is welded to the outer periphery of the fan motor or fan shape in which the fan and motor are integrated. There is a method of using a disk-shaped electric motor in which a plurality of coils are arranged on the outer periphery of the ring so that a permanent magnet such as a neodymium magnet is fixed along the outer periphery and the permanent magnet is wrapped. The method of using multiple pieces to gather together like a bunch of kites is also included in the structure of the upper flying object. Including the method of laminating honeycomb structures such as honeycomb sandwich panels or weir ferran structure panels horizontally in multiple stages, this is exactly the shape of the internal structure of a natural round honeycomb. The kite becomes the structure of the entire flying object and protects people inside the kite













It is also possible to enter the inside of a spherical kite, and the kite allows the wind generated by the electric motor to pass downwards and both the propeller or fan guard and the upper flying body and the lower suspension body This kite can also be used as a boarding deck that can feel the structure of the airship and the wind, and the spherical kite can be easily assembled and disassembled by attaching and detaching the fixture. The method is structured by combining two hemispherical cocoons into a sphere, and a propeller or fan and electric motor are placed inside the sphere, and a cocoon-like sphere with a propeller or fan and electric motor is placed like a cocoon The electric motor and propeller or fan, which is a method of constructing the flying object by assembling with the fixtures, are on the shaft of a normal electric motor with a fist-sized rotor. A method of attaching a rocket or fan and fixing it to the center of the cross beam, and a horizontal plane passing through the center of the sphere is at the center of the disk motor and propeller or fan or fan motor or motor and cross beam. There is a method of installing a blower. As a motor, the rotor of a disk type motor is a three-blade prober shape, and a permanent magnet such as a neodymium magnet is fixed around the outer periphery of this disk-shaped propeller or fan. A disk-type electric motor that includes a method that combines a motor with a disk-type propeller or a fan in which a ring-shaped member is wrapped around a magnet on the outside of the child and a plurality of coils are arranged inside the ring is a pipe. Honeycomb such as honeycomb sandwich panel or weir ferran structure panel even with the combined method The lower suspension body in which the lower suspension body is provided at the center of the lower part of the upper floating body of the personal aerial work flying object can be used even in the method of laminating the mobile structure. The lower suspension body is a lobe of natural fibers or chemical fibers having a length of about 195 mm to 3300 mm. Or ropes, wires and wires made of steel wires or metals such as iron, steel, aluminum and titanium, resins, carbon fiber reinforced resins, glass fiber reinforced resins, Kevlar fiber reinforced resins or a combination of these materials The lower suspension body is composed of a lower suspension part made of steel, bar, or pipe material. The lower suspension body is connected to the center of the lower end of the upper aircraft with a freely movable connecting device such as a chain link or universal joint. Lower suspension rope that is flexibly connected so that the center of gravity of the body can be moved freely Alternatively, there is a method of sitting on a swing platform provided on a lower suspension body such as a rope or standing on a step fixed to the lower suspension body for a wire or bar material or pipe material in the air From here, it is a description of the safety measures for workers. Humans who work in the air are light helmets with air caps stiffened with styrofoam and small heels so that they do not damage the body even if they fall from about 33 meters above the ground. A waterproof cotton bag with a thickness of 19.5mm to 33mm, which is packed with air bags such as small air bags covered with rubber or silicon rubber inside a cloth or non-woven fabric of natural fiber size chemical fiber A waterproof and airtight zipper such as a lightweight waterproof cotton lining with a shape like clothes or a collection of fibers mainly containing air There is a method in which a human body protective bag such as a human-type sleeping bag or a human body protective clothing that humans can enter and exit is connected to the lower suspension body with a fixing tool or belt that can be attached to and detached from the lower suspension body, using Zic Tape (registered trademark) The waterproof and airtight zipper, which is a waterproof and airtight zipper description, is about 0.195mm to 3.3mm thicker than the two underlying fabrics for the purpose of waterproofing and airtightness and preventing the cloth from getting into the zipper. When looking at the zipper vertically, the width of the zipper is about the width of the seam on the left and right sides of the zipper, and the length of the resin zipper is about the length of the zipper. Prevents the cloth from biting into the zipper when the fins along the resin zipper are stitched one by one in the seam of the zipper, and the zipper is pulled up The zippers on both sides of the zippers are covered with a silicone resin or rubber-based resin so that the fins that cover the zippers and the fins overlap exactly with each other. Even if the fabric does not bite into the zipper, the zipper can be pulled up and down easily, and at the same time the inside of the zipper is airtight and waterproof, the above is a description of a zipper that is not waterproof and airtight, the protection of human side protection There is a method in which the shock-absorbing material and the seat are processed into a three-dimensional mesh like a scrap of plant yarn using a chemical fiber material wire, carbon fiber wire material or carbon fiber reinforced resin fiber material. The fiber shape of a thread spider that allows you to work in the air with your feet resting on the steps provided on your body -Like shock absorbers or human-type sleeping bag-type or clothes-type shock absorbers detect natural fall in parts that may collide with the ground, such as human-shaped heads, shoulders, spines, and buttocks The acceleration sensor that detects the natural fall of the human body and there is a method that the air bag instantly inflates with compressed air to protect the human body in a shape that wraps the human body before the human body collides with the ground, The method of working in the air is equipped with a parachute on the upper part of the gyro of the upper flying object, and it is structured to automatically open the parachute when a free fall is detected by human will or with an acceleration sensor, so that the worker lost consciousness As a simple emergency rescue method, the personal aerial work flying object is structured to safely descend with humans. The gyro is installed at the top of the upper flying body and works to stabilize the upper flying object in the air.The personal flying object is suspended by humans or robots, video cameras, and radio control devices. A shock absorber such as a balance ball with rubber or silicone rubber sealed inside at the lower end of a human or video camera and radio control device makes it possible to observe or save lives. The following capacitor (capacitor) or secondary battery (battery) is used on the lower surface of the shock absorber, which is a description of the capacitor (capacitor) or secondary battery (battery). Of capacitors and graphene using nanocapacitors between clusters in amorphous and crystalline alloys such as Ni-based and Si-based Single-crystal nanocube placement / arrangement / bonding / interface control technology single-crystal nanocube bottom-up from two to three-dimensional by single-crystal nanocube technology using stacked ceramic capacitors and dielectric ceramics Or, a nanostructured ceramic, metal, carbon, etc. structure that is precisely controlled at the atomic level, a storage device using a unique structure nanocrystal for an electricity storage device, a fuel cell / water electrolysis battery using an nano stacking method, an AGM deep cycle battery, Compact and lightweight fuel cells such as large-capacity ceramic capacitors and solid hydrogen source fuel cells, all-solid-state electricity storage devices of complex hydride-based fast ion conductors, oxide-based bulk all-solid lithium secondary batteries, or large-capacity laminated lithium I need a battery Lithium ion air battery, lithium ion battery, nickel / hydrogen rechargeable battery, magnesium storage battery, non-lithium battery using medium / low temperature ionic liquid, metal and air battery using high oxygen ion conductor nano thin film or anion exchange membrane Noble metal-free fuel cell or secondary metal filled with specific metals such as lithium and sodium only in the interior of a unique structure of tubular carbon nanofiber (CNF) that has multiple nanogates that can only enter and exit ions A lightweight, small, large-capacity battery or capacitor, such as a battery selectively prepared as a negative electrode material for a battery, as described above for a capacitor or secondary battery (battery), is placed under the shock absorber. , Lower the center of gravity of the flying object When the flying object of the personal aerial work is levitated when the mind is at the bottom, it prevents it from rotating in the top and bottom direction. A wire or rope or wire is hung at the lower end, and this wire, rope or wire in the front, back, left or right direction is equipped with a human or radio control device and a small computer with a built-in automatic posture control program. Or, by pulling the wire manually or mechanically, the center of gravity of the flying object for personal aerial work is moved back and forth and left and right to control the flight in the horizontal direction, and at the same time the motor current for levitation By adjusting and synchronizing with the adjustment device, flight control of hovering and movement in the vertical direction is performed to perform personal work flight. Radio control maneuvering device that enables forward, backward, ascending, descending, left and right movements as corps movements, transmitters (receivers), receivers, servos, motor amplifiers, speed controllers, wirings, wiring tools, etc. There is a method of automatically controlling while working with a device that combines a switchboard, switches, and computer. The personal aerial work flying object is controlled manually by a control switch provided at the hand of the passenger, by a radio control radio transmitter (propo) The rope or wire is hung from the lower end of the battery to the ground, the lower end is fixed to the ground, and the human being on the ground is hung from the personal aerial work flying object. To move the flying object of personal aerial work from the ground Yes, only for work, there is a method of transmitting electricity to the required height by placing a battery or power supply unit on the ground, instead of an electric motor for the upper flying body of a personal aerial work flying object to gain lifting force A method using an internal combustion engine is a method using a light-weight internal combustion engine made of a light metal such as titanium or aluminum instead of the electric motor of the above-mentioned flying object. Forced air-cooled whole heat-dissipating fiber reinforced resin metal composite internal combustion engine, which is a description of composite internal combustion engine, directly applies heat and explosion to the high temperature wear-resistant part covering the internal combustion part, ie cylinder head, cylinder, piston, piston ring, connecting rod, crankshaft The receiving part is a layer of lightweight metal such as titanium or aluminum and a steel woof around a layer of wear-resistant and heat-resistant metal. By applying a heat transfer layer of Lullock wool glass wool and a stress transmission rod that transmits explosive force to the fiber reinforced resin layer, stress is transmitted from the metal layer through the heat buffer layer to the fiber reinforced resin layer and directly to the metal part by forced air cooling. Cold air is blown and heat is released from a plurality of small holes opened in the entire casing, and the entire casing of the internal combustion engine such as an oil pan is configured to share a metal or fiber reinforced resin honeycomb structure. The outside of the titanium or aluminum layer is a radiating fin outside the engine of the air-cooled motorcycle. The height is 19.5 mm to 33 mm, the thickness is about 1.95 mm to 3.3 mm, and the range is 1.95 mm to 3.3 mm. Multiple processing is performed to wrap the surface of the metal layer at intervals of about millimeters, and a heat buffer layer is formed on the outside of the metal radiating fin. It is surrounded by a heat buffer layer in which a steel wool layer, a rock wool layer and a glass wool layer, which are compressed from the inside, are provided to form an air-containing layer and comes into contact with the heat buffer layer from the outside The inner surface of the fiber reinforced resin is 19.5mm to 33mm in height, 1.95mm to 3.3mm in thickness, and 1.95mm to 3.3mm in the interval of about 1.95mm to 3.3mm. A honeycomb structure made of metal or fiber reinforced resin is wrapped around the outside of the heat resistant fiber reinforced resin, which is wrapped in a layer of fiber reinforced resin such as heat resistant carbon fiber reinforced resin. The cylinder heads and cylinders that receive the explosive force of the internal combustion chamber, which is responsible for the mechanical structural members related to the strength of the internal combustion engine, are commercially available. The length of one split chopstick is from the support part of the metal layer to the support part of the heat-resistant fiber reinforced resin layer, and a plurality of metal rods having a diameter of 6 mm to 9 mm are provided at intervals of about 33 mm to 195 mm. Layers of wool and rock wool













A rod that penetrates through the layer of lath wool and spreads radially like sea urchin thorns to transmit the explosive force from the metal layer to the heat-resistant fiber reinforced resin layer and to the honeycomb structure layer made of metal or fiber reinforced resin. Both ends of the material are supported by a support part provided in a metal layer and a layer of heat-resistant fiber reinforced resin, the rod that transmits the explosive force is threaded, and the stress transmission rod is threaded into the screw hole cut in the groove of the support The steel wool layer, rock wool layer and glass wool layer are supported by the tips of the inner and outer radiating fins from the compressed inside, and are responsible for overall heat dissipation This heat-resistant heat-resistant fiber reinforced resin that bears the burden is covered with a two-dimensional or three-dimensional honeycomb structure made of metal or fiber reinforced resin, etc. Metal and fiber reinforced resin in which a plurality of small holes having a diameter of about 0.195 mm to 3.3 mm are opened at intervals of about 1.95 mm to 33 mm to achieve overall heat dissipation throughout the fiber reinforced resin and the honeycomb structure. This is an internal combustion engine that combines a honeycomb structure with a honeycomb structure, and the overall heat dissipation is like a dragonfly wing feather, with a thin trachea with a diameter of 0.195 to 3.3 millimeters for heat dissipation. It opens radially from the inside of the internal combustion engine to the outside at intervals of about 1.95 mm to 33 mm, and is opened at the front of the internal combustion engine by the power of the internal combustion engine rotating or by the power of the turbocharger using the exhaust exhaust of the engine. Rotating the blades of the opening, the air is blown and the air diameter is 19.5mm to 33mm There is a forced air cooling dedicated pipe that is distributed and branched so that air is directly blown to the metal fins of the cylinder using a forced air cooling dedicated pipe. Titanium is directly blown to the heat radiating fins of metal such as titanium or aluminum surrounding the internal combustion section to perform forced air cooling. Alternatively, the aluminum radiating fins dissipate heat, dissipate the entire air through the heat buffer layers in the order of steel wool rock wool glass wool, and the heat dissipated air has a honeycomb structure of heat-resistant fiber reinforced resin and metal or fiber reinforced resin. A plurality of diameters 0.195 mm to 3.95 mm inside the heat-resistant fiber reinforced resin layer and the honeycomb structure layer through a thin tube having a diameter of 0.195 mm to 3.3 mm, such as a feather of a dragonfly penetrating therethrough. There are tubules at intervals of about 1.95 mm to about 33 mm. This is to dissipate heat from the whole internal combustion engine through a small hole. This is to disperse the heat so that the resin does not melt with heat. The lower suspension body uses a battery and a fuel tank under the shock absorber. There is a method of installing a battery and a gasoline tank in the vehicle. Forced air-cooled whole heat-dissipating fiber reinforced resin metal composite internal combustion engine can be used as a gasoline engine or a diesel engine. Heavy electric control device, battery and gasoline There is a method of sending the fuel from the ground and sending the fuel to the air vehicle in the air with a pump through the oil supply pipe, and the piston engine type or rotary engine type internal combustion engine, generator and electric motor. Combined and integrated forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable flywheel Luke converter clutch forced air cooling Whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator Electric coil disk stacked generator motor output power transmission transmission integrated hybrid device is forced air cooling when the internal combustion engine is started by the motor and the output of the internal combustion engine increases Overall heat dissipation fiber reinforced resin metal composite internal combustion engine generator motor Torque of internal combustion engine by torque converter and clutch in hybrid device The inner disk is fiber reinforced resin and the outer periphery of the disk is metal fiber reinforced resin A metal wheel that can be increased and decreased while the metal is automatically rotated by computer control. Metal wheel on the outer periphery of this wheel is 360 degrees along the circumference like a shield segment. The equally divided segment is the relationship between the sectors and tracks in the cluster area of the floppy disk. The method of increasing the amount of metal on the outer periphery, which has a concentrically layered structure like the above, is that the metal segments are hooked on the rotating metal outer claws, and the claws form an arc like a claw The claw can be moved in and out by rotating the claw.When removing the metal segment, the claw is pulled in and the segment is separated from the spring wheel by centrifugal force and separated by a rotatable claw provided on the wall of the circumferential wheel. This mechanism can be used to adjust the rotational force of the rotating machine. This mechanism can be used to adjust the rotational force of the rotating machine. The momentum-adjustable flywheel adjusts the angular momentum in conjunction with the computer to ensure a stable angular momentum, and then sends a part of the output of the internal combustion engine to the motor / generator to generate power and output the power to the external compound. There is a method of transmitting power to the electric motor of this. To obtain electric power, the power of the internal combustion engine is obtained and then power generation is performed, and the fine adjustment of the output such as thrust is an advantage of the electric motor that obtains thrust if necessary. Is an internal combustion engine generator that can control the energy in total by using a computer and share the distribution of the motor and motor angular momentum adjustable spring wheel torque converter clutch computer integrated hybrid device, the above is forced air cooling overall heat dissipation fiber reinforced resin metal composite internal combustion engine The rotary engine method is a rotary engine and forced air-cooled whole heat radiation fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor forced air cooling whole heat radiation fiber reinforced resin metal composite rotor permanent magnet fixed This unit can be used as a sub-coil disk stack type electric motor / generator. Combined and laminated, forced air-cooled whole heat-dissipating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable spring wheel torque converter clutch forced air-cooling whole heat-dissipating fiber reinforced resin metal composite generator motor output power generation integrated power transmission hybrid device, here Is a description of forced air-cooled whole heat radiating fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor, the disk stacking type electric motor has a rotor with a diameter of 19.5 mm to 330 mm in thickness 1. 95 to 33 mm metal or fiber reinforced plastic disc shape with a circular diameter of 1.95 to 33 mm inside 3 or 6 or 12 or 16 or 32 in a concentric radial position from the axis There are multiple holes that fit in the disc of A disk that fixes holes in a concentric circle radially from the shaft toward the electric motor shaft and is fixed with permanent magnets. Permanent magnets such as magnets are embedded and fixed, and the permanent magnet is fixed so that the magnetic flux is perpendicular to the disk surface. The disk of the electric coil is fixed to the rotating shaft of the electric motor. The magnetic flux of the electric coil is the disk. Is the same size as the disk of the magnet, but the shaft portion of the electric motor is a hole and passes through the shaft of the electric motor and is permanent with a gap of 0.195mm to 0.33mm At the position where the magnet and the electric coil face each other, an electric coil thicker than the permanent magnet is fixed at the position corresponding to the permanent magnet, and the copper enamel wire of the electric coil or room temperature The laminated ceramic type coil formation with nitrogen circulation glass amorphous or ceramic coating in the conductive pipe is not a coil but a three-dimensionally laminated coil and insulator to form a coil. There is a method in which a ceramic coil and an insulation coating ceramic are simultaneously formed by a three-dimensional solid atomic layering technique, or a high melting point glass or ceramic is used to make a female coil and a good conductive metal with a low melting temperature is made of glass or There is a method of manufacturing a heat-resistant coil made of glass or ceramic that is insulated by injecting with an inert gas gas while keeping the temperature in a female coil of a ceramic coil. Disks with holes in the central axis arranged radially on the circumference are fixed to the casing of the electric motor The disk that fixes the electric coil is made of metal or fiber reinforced resin. The permanent magnet disk and the electric coil disk are alternately laminated. The disk with the permanent magnet fixed is an electric coil from both sides. The electric coil that is sandwiched becomes a brushless motor that rotates the permanent magnet in phase with the rotation direction. This principle is based on fixing the disk that fixed the permanent magnet to the casing of the electric motor and fixed the disk that fixed the electric coil. The method of the brush motor fixed to the shaft of the electric motor may be the method of forced air cooling whole heat dissipation rotor permanent magnet stator electric coil disk laminated electric motor is metal and carbon fiber, the other part is fiber reinforced resin Forced air cooling is performed with blades fixed to the shaft of the electric motor, and the air passes through a plurality of holes formed obliquely at an angle of the blades with respect to the rotation direction of the disk. The air that has been cooled with air is passed backwards to cool the disk and dissipate heat. The hot air radiated from the entire casing has a diameter of 0.195 mm to 3.3 mm and is spaced at intervals of about 19.5 mm to 33 mm. The number of permanent magnets and electric coils is arranged for multiple shafts and casings compared to conventional electric motors that radiate heat from the whole electric motor through a small hole, eliminating the problem of heat dissipation and the rotation direction of the disk A plurality of holes with a diameter of about 0.195 mm to about 3.3 mm drilled at an interval of about 1.95 mm to 33 mm and inclined at an angle of about 19.5 to 33 degrees with respect to the rotating surface. Depending on the method that solves the problem of heat dissipation by becoming a kind of blower by rotating, the electric conductor is made into a pipe shape There is a method of cooling the inside by the above method.Also, the disks are all powerful electric coil disks, and the alternating current is generated in such a way that the disk with the opposite direction of the magnetic flux of each coil and the disk with its axis fixed rotates. This method, which may be given, will be all electric coil brush electric motor, the above is a description of forced air cooling whole heat radiation fiber reinforced resin metal composite rotor permanent magnet stator electric coil disk stacking type electric motor, from here Bird Strike Prevention Device Fiber Reinforced Resin Metal Composite Turbine Stacked Electric Motor is a turbine stacked type electric motor. The disk of the disk stacked type electric motor is processed into a complete blade shape, and permanent magnets and electric coils are fixed to the blades. The blades are made by alternately laminating the permanent magnet layers and the electric coil layers so that they look like jet engine intake turbines. This is a description of the bird strike avoidance device, which is a description of the bird strike avoidance device. The blade for blade strike is made of steel, stainless steel or aluminum alloy steel with the tip of cutting the wind of the blade in order from the entire surface of the intake blade. When a bird strike occurs after processing like a sharp blade, the bird is cut with a multi-stage blade-shaped steel blade, and the meat pieces that are cut into pieces or minced meat pieces are removed from the sides of the engine or motor by centrifugal force. A flute that tends to splatter toward the blade is provided on the side of the casing to guide the meat piece to a position where the flesh of the electric motor or jet engine is likely to splatter by a sensor that detects the bird strike by guiding the blade to the position where the flesh is to fly. The engine or motor can be opened from a small window-shaped opening -The normal jet engine method that temporarily ejects and discharges with the internal wind is to prevent the bird's meat pieces from reaching the burning part of the jet engine and to minimize damage to the engine due to bird strike. The above is a description of the bird strike avoidance device, and a neodymium magnet at a position where the direction of magnetic flux is parallel to the blade rotation axis on the blades of the turbine blades having a pitch angle and obliquely arranged using this device. The electric motor in the shape of an intake turbine of a jet engine in which layers of permanent magnets and electric coils, such as alternating layers, are easily replaced, and the output can be controlled freely without the need for complicated mechanisms. Light turbine and noise-free jet turbine type by using fiber reinforced resin as the turbine that can solve the problem Aviation fuel that can be used in passenger aircraft and can be used in passenger aircraft to produce aircraft using a jet turbine-shaped electric motor for noise reduction by generating electricity with a lightweight internal combustion engine of gasoline or light oil or heavy oil Instead of a gasoline engine or heavy oil
Or diesel oil












It is possible to generate electricity with a diesel engine and to purify the exhaust gas through a soundproofing muffler and exhaust gas purification catalyst ceramic. At the same time, the aircraft attaches silicon-type solar cells or polymer organic thin-film solar cells to the whole or a part of the aircraft over the sea of clouds. It is useful for preventing air pollution or economically and safely for fuel explosions. Inside a jet turbine-shaped heat fiber reinforced resin-metal composite that generates power by a low fuel consumption internal combustion engine and obtains thrust of flight. Electric motor can be driven, or at the same time forced air cooling whole heat-dissipating fiber reinforced resin metal composite internal combustion engine angular momentum adjustable bounce wheel torque converter clutch forced at the rear of jet turbine shaped heat fiber reinforced resin metal composite electric motor as hybrid type Air cooling whole heat radiation fiber reinforced resin metal composite generator By combining the power transmission integrated hybrid device, the output, power generation and power transmission by the internal combustion engine are integrated and computer management is performed, and it becomes possible to control the distribution of energy sharing, and the internal combustion engine obtains thrust and power while the power is converted into an electric motor. The above is a description of the bird strike prevention device fiber reinforced resin metal composite turbine laminated electric motor, which can transmit power and assist the battery power, and can charge the battery with surplus power. From here, it is a description of the method of using a turbine stack type electric motor for a personal aerial work flying object. Permanent magnets and electric coils are arranged concentrically around the circumference of the blade, and magnets and electric coils are arranged. The top of the upper aircraft using blade electric motors with alternating layers as the flying object for personal aerial work The pure method is a method in which the upper blade and the lower blade are sandwiched so that the upper blade and the lower blade are rotated in reverse directions with a blade having a permanent magnet fixed above and below a disk to which the electric coil is fixed. A magnetic flux from N to S is formed in a concentric circle along a circle inside the circumference of a disk made of fiber reinforced resin or a metal or a combination of metal and fiber reinforced resin with a diameter of about 3300 mm from 33 mm. The disk is arranged in a radial direction from double to triple concentric circles so that the direction of the magnetic flux is perpendicular to the disk surface, that is, the magnetic flux is perpendicular to the disk surface, that is, a honeycomb with no wind Honeycomb through which wind passes) The structure or fiber reinforced resin can be directly opened at intervals of about 1.95 mm to 33 mm in consideration of mechanical distribution. Wind that has a shape with a plurality of holes with a diameter of about 0.195 mm to 3.3 mm or a mesh shape that supports an electric coil, and the wind path is slanted according to the pitch angle of the blade. There is a shaft at the center of the disk that is for the passage of the shaft, and the shaft protrudes from the center of the two faces of the stator disk. This shaft has a hole through which the shaft passes through the center so as to sandwich the disk of the stator's electric coil Two blade windmills with a pinch are sandwiched from above and below. The blade of this blade windmill has a permanent magnet such as a neodymium magnet at a position facing the electric coil with a gap of 0.19 mm to 0.33 mm. The two blade wind turbines, in which the alternating current is sent to the electrical coils that are in opposite phases to each other, rotate in the opposite direction and blow the wind downward. The blade that prevents the entire aircraft from rotating by the frame shape or the net-shaped blade guard is protected from the damage of the blade. The internal combustion engine generator-motor hybrid device, which is attached to the body and constitutes a personal aerial work flying object, can be combined with forced air cooling whole heat radiating fiber reinforced resin metal composite internal combustion engine. The method of using the balloon to obtain the ascending force of the upper flying body of the personal aerial work flying object, which is attached to the body as a personal aerial work flying object, is a combination of hot air balloon, gas balloon, hot air balloon, and gas balloon. Individual air working flight using balloons is composed of upper flying body and lower suspended body, and upper flying body using hot air balloon Consists of an envelope (ball skin), a load tape, and a wire. The envelope material is made of nylon or polyester chemical fiber that is airtightly coated with polyurethane, and is the smallest unit of the envelope. A ball or bag shape or cylindrical shape reinforced with load tape by vertically stitching gores that are vertically sewn together horizontally and reinforced with load tape, or a number of parts receiving the load vertically. Load tape, which is reinforced with a nylon or polyester road tape or carbon fiber reinforced resin wire netting, is sewn on the crown ring at the top of the emperope, the lower end is a suspension cable and the following backpack Suspensions that are connected and share the load The cable is made of steel, stainless steel, carbon fiber reinforced resin wire, twisted wire, Kevlar fiber reinforced resin wire or twisted wire, and the load tape is horizontally oriented like a barrel tag to prevent the envelope from tearing. Also used in multiple, the peripheral part of the burner at the opening part of the envelope has a glass squirt shape of the following kerosene lamp with a supplementary cloth called a triangular scoop or skirt shaped skirt for introducing hot air There is a method in which the net replaces this skirt or scoop. There is a method in which an auxiliary fabric called a skirt covers the upper hemisphere of the squirt sphere made of net to facilitate the recovery of hot air. The part that receives heat is called Menox. The method of using a hot air balloon that uses materials as a gas balloon is airtight. The envelope is tied to the following torch with a belt and the floating gas is ejected from the torch.This envelope is mainly sewn with a thread such as polyester, and the place requiring heat resistance is sewn with a thread such as Nomex. A solenoid valve made of carbon fiber reinforced resin that exhales hot air is opened and closed at the top or middle of the envelope. It is controlled by manual, wireless, and automatic control. The lower suspension body is about 195mm to 9900mm in length and 1950mm to 99000mm in length, and the size of the lower suspension is about the size of a rucksack that you carry when climbing up Everest from the size of a school bag used by elementary school students. It consists of a backpack and a backpack peripheral device. The belts to be carried can be joined with the buckle at the position in front of the chest, the belt is wrapped from the backpack's back to the belly, the belt is wrapped around the front of the belly and the person is fixed to the lower suspension body with the buckle etc. A belt hangs down on the seat part from the contact part and the two rings provided on the belt of the seat part allow humans to pass both feet and stabilize the buttocks from the shoulder to the chest and around the belly and How to fix the occupant to the backpack that suspends the shock absorbing device under the human foot that carries the backpack and the back center part of this belt that is going to fix the heel part with a belt In detail, the backpack is like a school bag used by elementary school students, and the right and left belts that fix the body and backpack by passing the arms through the left and right belts The belt is stretched from the left and right sides of the backpack to fix the abdomen of the passenger, which can be fixed using a buckle at the chest. The belt extends downward from the backpack's back and can be fixed on the backpack, and the belt has two rings that allow both feet to pass through. A shock absorbing device in which a belt extends further beyond the wheel that passes both feet, and the shock absorbing material is fixed to the tip of the belt, rope material or bar material, which can fix the heel portion of the passenger The propane gas cylinder and the digestive gas cylinder below the battery and the battery, condenser, power supply controller, autopilot, video camera, etc. The peripheral device of the pack is a horizontal cylindrical envelope take-up device having a horizontal length of about 1950 mm located at the upper part of the backpack, and a guide for winding the envelope (ball skin). There is a method of forming a link shape that passes through the ball skin) and a hopper shape made of resin etc., and the uppermost end of the envelope is connected to the winding device with a string or wire, so that the fishing boat net can be unwound and rolled up As a detailed description of the winder, the envelope winder has a guide or hopper for winding the envelope behind the winder, and a cable that guides winding from the top of the envelope passes through the hopper. The envelope is fixed to the rotary shaft of the winder and The suspension cable can be taken up together with the envelope. The envelope take-up device, which has a mechanism that opens manually or automatically, can be moved by the motor in the backpack, and the right lever is viewed from the passenger. The right lever extends from the right side of the backpack, and the switch that unwinds and winds the envelope is attached to the right lever, and the right lever can be moved up and down, left and right and back and forth like the control stick of a zero-type ship fighter The movement of flying objects The method with multiple propellers or fans in order to interlock with the vertical and horizontal movements is a propeller or fan that is linked with the device that changes the position of the aircraft. It is linked with the front / rear direction output, and it is linked with the up / down / left / right direction rudder behind the fan guard, and the position of the personal aerial work flying object can be operated. The right lever that realizes autopilot changes the position of the top, bottom, left and right, and the left lever changes the position of the top and bottom. From the top center of the backpack, the diameter is 19.5mm to 33mm. 195mm to 3300mm pipe-shaped metal or resin here called torch Or there is a cylinder that leads propane made of carbon fiber reinforced resin or glass fiber reinforced resin, and a small burner is installed at the top end of the cylinder of this torch, and an ignition device and a fire extinguishing nozzle are near the small burner. The left handle attached controls the rough vertical movement of the flying object for personal aerial work, and the left handle extends from the left side of the backpack so that it can be operated with the left hand when viewed from the back. There is a lever and the amount of gas can be adjusted by turning the handle of the left lever. The gas has a changeover switch such as propane gas for hot air balloon and helium gas for rising or propane helium mixed gas. These switches with a fire extinguisher switch and the left lever are electrically connected to the autopilot and are A valve that adjusts the amount of propane inside the torch is installed on the left lever as viewed from the side of the backpack side that realizes maneuvering and automatic maneuvering, and hot air or floating gas exhaust valve is opened and closed on the valve A valve that adjusts the amount of propane and a hot air exhaust solenoid valve that are equipped with buttons are electrically connected to the autopilot device, realizing manual, wireless, and autopilot. A heat-resistant metal or fiber-reinforced resin called a combustion guard net around the vicinity of the combustion section of the pipe that guides propane gas connected to a propane cylinder or a floating gas cylinder installed under the shock absorber A net-shaped tube with a diameter of 66 to 195 mm and a length of 195 to 3300 mm surrounds the small burner. This net-shaped cylinder is structured so that it can move up and down around the cylinder that sends propane, and when storing the envelope, the cylinder that sends propane completely fits in the center of this net cylinder and the burner is When used, this cylindrical net extends to the top of the small burner.













The combustion guard net which prevents the envelope (ball skin) from burning with the heat of the burner is like a glass squirt of a kerosene lamp so that the envelope (ball skin) does not burn with the heat of the burner when the small burner is ignited The bottom of the mesh swells in a spherical shape with a diameter of 330 mm to 990 mm, and the method of extending the maximum cylindrical mesh upward is a small burner where the bottom of the cylindrical mesh protects the periphery of the burner. A shaft that rotates the prober or the fan extends from the center of the back surface of the backpack where the digestion fluid is ejected when the envelope (ball skin) is burned by the heat of the burner. The diameter of the backpack is about 19.5 mm to 33 mm and the length is about 19.5 mm to 66 mm. The electric motor described in the scope of claims of the present invention is installed horizontally in the middle of the interior of this electric motor. The fan guard and shape of the home electric fan, in which the propeller or fan of the previous period is fixed to the tip of the electric motor shaft The fan guard air that is similar has a cross-shaped rudder in the direction in which the air blows, and on the right side of the person riding on the side of the backpack, the lever extends from the backpack side to the right hand position and this right lever is By moving it up and down, left and right, the rudder fixed to the fan guard guides the air blown back and forth back and forth and left and right to move the individual aerial work body up and down and left and right.This lever is electrically connected to the autopilot. The control of the radio control and the automatic control are realized. Rise and fall are roughly adjusted by adjusting the valve on the left hand lever of the passenger. Adjusting the buoyancy of the hot air balloon by adjusting the fire power of the left lever valve adjusts the amount of floating gas such as helium etc., the gas balloon method rescues the rescuer by radio control automatic control and in the air with a video camera Capable of shooting, manual, wireless, automatic control is possible. The crew is equipped with the above-mentioned shock absorbing human sleeping bag and shock absorbing air bag and free fall on the upper part of the envelope unwinding and winding device This is a gas balloon method that is equipped with a ballot chute that is detected by a sensor and opened automatically by a person's will or automatically. The material is a carbon fiber reinforced resin wire having a diameter of 0.195 to 3.3 millimeters, and a grid of 330 to 1950 millimeters. The shape of the mesh knitted by the square mesh is 0.195 mm to 3.3 mm thick woven with a polyethylene terephthalate cloth inside the mesh of the carbon fiber reinforced resin wire having the same size as the hot air balloon method. This gas balloon is heat-treated and heat-treated from the inside of a polyethylene terephthalate cloth bag that adheres a 3 mm cloth to the inside of the mesh to make a gas balloon airtight with latex rubber, natural rubber or urethane resin. The tip of the hot-air balloon torch described above is introduced into the gas balloon and is air-tight, and helium gas or hydrogen gas cylinder is installed instead of the propane gas cylinder, that is, the gas inside the balloon, that is, hot air. As a hot air balloon or gas balloon by changing to hydrogen (explosion is prohibited because it explodes) or helium The balloon opening can be used for the hot air balloon method to collect the heated air and the gas balloon method has the gas outlet tube inside the envelope and the gas balloon method has the tip of the opening. This bundling method is like a flare skirt made of thin silicon rubber or rubber-based resin fibers in an airtight manner, and is tightly bound with a band to prevent gas leakage as much as possible. As long as the time or air floating time can be obtained, it is assumed that gas will leak to some extent. The personal air work flying object combining an electric motor or an internal combustion engine and a balloon is divided into an upper flying object and a lower suspension object. The ice-cream cup cone-shaped saddle type envelope storage device is a method for storing the envelope and envelope of the upper flying object. Motor motor or internal combustion engine through a universal joint that can freely change the direction of the electric motor to the tip of the arm that extends in the shape of a cantilever around the cup cone shape cup A propeller or fan is attached to the shaft of an electric motor or internal combustion engine, and the tip of the lower part of the cup cone shape that moves the balloon up and down, front and rear, left and right by changing the direction of the electric motor or internal combustion engine is described above. Electric motors or internal combustion engines and hot air balloons or gas balloons or heat and gas combined balloons that can be boarded by humans with a lower suspension body are manually, wirelessly, or automatically operated. The ice cream cup cone shaped bowl is a cone A circle with a small radius in the shape of a base, a circle with a large radius on the bottom surface is the top surface, and a circle with a small radius on the bottom has a lower ring made of metal or fiber reinforced resin. From the three points where the circumference is divided into three parts, the branches forming the ridges are from three places that extend from the ring surface to the left and right at an angle of about 30 to 60 degrees with respect to the ring surface. Since there are two each, there are a total of six, each one forming a helix according to each angle. The front end of the helix is connected to the upper link at a point at the outer periphery with a central angle of 60 degrees. The intersection of the mesh that is meshed and is knitted regularly is fixed with epoxy resin etc. The lower link is divided into three parts, the upper part is divided into six parts, and the three parts connected by the belt member knitted into the mesh ridge are described Because the lower ring is actually 1 The split method is that the upper ring will be divided into 24, which is twice the twelve. The twelve split may be 36, the lower link may be any number of dynamically adapted anyway, and the upper is double that anyway. In this way, an object like a large trash can is formed in the truncated cone with the bottom of the truncated cone that combines the envelope storage with the side of the truncated cone shaped like a bowl and the structure of the upper flying object. The storage method in which the envelope is stored in the cage with the frustum open upward is that the point inside the load tape divided inside the balloon due to mechanical considerations, that is, the balloon is the earth, and the balloon loads like meridians and parallels. This envelope in which a flexible wire that also serves as a suspension cable of metal, resin, or carbon fiber reinforced resin is hung from the intersection of the meridian and latitude that is reinforced with tape. Multiple flexible suspension cable wires inside the loop can be wound or unwound by rotating this roller, which is fixed to the roller of the suspension cable winder installed in the lower part of the cup cone shaped cage. The envelope is melted by heat at the bottom of the cup cone-shaped bowl, which can be stored inside the cup cone-shaped bowl opened up or removed from the cup cone-shaped bowl. The method of using heat and gas with a gap between the envelope and the burner that takes heat into consideration to a lesser extent is that the gas outlet is located inside the cup cone-shaped bowl and the gas outlet is the envelope Cup-cone bowl with the tip of the burner serving as a gas injection hole inside Is a cup cone-shaped kite with a small burner surrounded by a combustion guard net installed at the bottom of the envelope at a distance where the envelope is unburned and stored, and serves to transmit the lifting force of the balloon to the lower suspension body As described in the claims, the ice cream cup cone type flying body can be used as a sealed hot gas balloon by mixing and burning propane gas and helium gas. It can be applied to the aerial vehicle, and is used in accordance with the Aviation Law to maintain the order of safety.

Images