WO2018053813A1 - Powered device and aerial wing outfit with powered device - Google Patents

Abstract

A powered device and an aerial wing outfit with a powered device. The invention comprises a control adjuster (8), and a highly oxygenated water storage chamber (1), catalytic reduction chamber (9), and jet propulsion compartment (3) connected in that order. The control adjuster (8) is used to control the flow of a highly oxygenated water stock solution flowing from the highly oxygenated water storage chamber (1) into the catalytic reduction chamber (9). The highly oxygenated water stock solution stored within the highly oxygenated water storage chamber (1) flows into the catalytic reduction chamber (9) and undergoes a reduction reaction within the catalytic reduction chamber (9). Propulsive power is generated by the reduction reaction generates a pushing force via the jet propulsion compartment (3). By using the highly oxygenated water as a raw material, the invention can avoid issues of flue gas emissions and other forms of environmental pollution caused by the use of fossil fuels, thereby realizing a clean form of power with zero pollution. The invention can provide propulsive power as an alternative to fossil fuels under an environment with thin air or low oxygen. A powered device and an aerial wing suit has a simple structure and low cost, and is environmentally friendly and easy to install.

Description

 Power device and flight wing suit with power device

 [0001] The present application relates to aircraft, and more particularly to a power unit and a flying wing with a power unit.

BACKGROUND OF THE INVENTION

 [0003] Coal, oil, and natural gas, as fossil fuels containing carbon or hydrocarbons, generate heat by generating heat energy by combustion with oxygen in the air. Since carbon, sulfur and other impurities in fossil fuels react with oxygen and nitrogen in the air at high temperatures, they generate harmful gases such as carbon dioxide, sulfur dioxide, and nitrogen oxides, and bring about greenhouse effects such as global climate change, acid rain and soil degeneration. Environmental problems such as air photochemical pollution have largely destroyed the ecological balance of the earth and the living conditions of human beings. As a long-term consideration of energy security, human beings urgently need to find an alternative energy source with little pollution, especially in the field of using energy as a transportation power application.

 [0004] Liquid fossil fuel blends require sufficient oxygen supply to burn and work normally. As human activities continue to expand into outer space and deep sea, these places are thin or even completely deprived of oxygen, and conventional fossil fuels cannot burn and lose their usefulness. This requires a new mode of energy supply that can provide power without relying on oxidation reactions in the absence of oxygen.

 SUMMARY OF THE INVENTION

 The present application provides a power unit and a flying wing device having the power unit.

 [0007] According to a first aspect of the present application, the present application provides a power unit including a control regulator and a sequentially connected high oxygen water storage chamber, a catalytic reduction reaction chamber, and an injection power compartment, wherein the control regulator is used for regulation The high-oxygen water storage chamber flows into the high-oxygen water liquid of the catalytic reduction reaction chamber, and the high-oxygen water liquid stored in the high-oxygen water storage chamber enters the catalytic reduction reaction chamber after the catalytic reduction A reduction reaction occurs in the reaction chamber, and the jet kinetic energy generated in the reduction reaction forms a driving force through the injection power compartment.

According to a second aspect of the present application, the present application provides a flying wing device having a power device, including a flying wing suit and a flight monitor, further comprising the above-described power device, the flight monitor and the power device setting In the flying wing suit, the power device is used to generate a catalytic reduction reaction chamber through a high oxygen aqueous liquid solution Thereafter, the generated jet kinetic energy is used to drive the flight wing, and the flight monitor is used to regulate the magnitude of the jet kinetic energy to regulate the flight speed of the flight wing.

 [0009] Since the above technical solutions are adopted, the beneficial effects of the present application are as follows:

[0010] In the specific embodiment of the present application, since high-oxygen water is used as a raw material for generating power, environmental pollution problems such as exhaust gas emissions due to the use of fossil fuels in the conventional transportation power can be avoided, thereby achieving zero-pollution cleaning. The power, especially in the environment of thin air or lack of oxygen, can replace the fossil fuel to provide jet power. The application has the advantages of simple structure, low cost, environmental friendliness and convenient installation.

BRIEF DESCRIPTION OF THE DRAWINGS

 1 is a schematic structural view of a power device of the present application in an embodiment;

2 is a schematic diagram of functional modules of a control regulator of the present application in an embodiment; [0013] FIG.

[0014] FIG. 3 is a schematic structural view of a flying wing with a power unit according to an embodiment of the present invention.

DETAILED DESCRIPTION

 [0016] The present application will be further described in detail below with reference to the accompanying drawings.

[0017] The present application proposes to utilize the jet kinetic energy released by the hydrogen peroxide in the catalytic reduction reaction, and based on the novel utilization idea of the kinetic energy characteristics released by the chemical reaction, in order to increase the oxygen content per unit volume of the oxygenated water, the release can be improved. The intensity of kinetic energy, this application uses high concentration of polyoxygen water as the working fluid, its concentration requirement is ≥5%, to distinguish the low concentration hydrogen peroxide which is used as medical disinfectant and civilian in the market, and this high concentration of hydrogen peroxide Known as "high oxygen water." Because the high-oxygen water early catalytic reduction reaction can not only release fresh oxygen gasification new water and form jet kinetic energy, but also has no toxic and harmful components in the product, it is a completely green and environmentally friendly process, so it is called zero pollution here. Jet kinetic energy.

[0018] Embodiment 1:

[0019] As shown in FIG. 1, an embodiment of the power device of the present application includes a control regulator 8, a high oxygen water storage chamber 1, a catalytic reduction reaction chamber 9, an injection power compartment 3, and a high oxygen water storage chamber. 1. The catalytic reduction reaction chamber 9 and the injection power compartment 3 are sequentially connected, and the control regulator 8 is used for regulating the high-oxygen water raw liquid flowing from the high-oxygen water storage chamber into the catalytic reduction reaction chamber, and is stored in the high-oxygen water storage chamber 1 at a high level. After entering the catalytic reduction reaction chamber 9, the oxygenated water solution undergoes a reduction reaction in the catalytic reduction reaction chamber 9, and the injection kinetic energy generated in the reduction reaction forms a driving force by the injection power cabin 3. In one embodiment, the high oxygen water storage chamber is provided with a feed port 0, and the catalytic reduction reaction chamber 9 may be provided with a slit 6 for injecting or removing the catalyst. [0020] In an embodiment, the control regulator 8 may include a terminal and a liquid shut-off valve 4, the terminal includes a processor 203, and the raw liquid shut-off valve 4 is disposed in the high-oxygen water storage chamber 1 and the catalytic reduction reaction chamber 9. The processor 203 is configured to control the liquid shut-off valve according to the user's instruction.

 [0021] In an embodiment, the control regulator 8 further includes a flow regulating pump 5, which is also disposed between the high oxygen water storage chamber 1 and the catalytic reduction reaction chamber 9, the flow regulating pump 5 and the raw liquid solution The shut-off valve 4 is connected in series, and the processor 203 is also used to control the flow regulating pump 5 according to a user's instruction.

 [0022] In another embodiment, the flow regulating pump 5 may be provided with a plurality of adjusting gear positions including 0 to MAX, and the terminal is further configured to control the flow regulating pump according to a user's instruction to adjust the high oxygen water. flow.

 [0023] As shown in FIG. 2, the terminal of the present application may further include an operation state parameter sampling input module 201, a control instruction parameter input module 202, a processor 203, a control parameter output module 204, and a communication module 205, and the input of the processor 203. The terminal is bidirectionally connected to the operating state parameter sampling input module 201 and the control command parameter input module 202, and the output end of the processor 203 is bidirectionally connected to the control parameter output module 204 and the communication module 205. The operating state parameter sampling input module 201 inputs parameters such as the liquid level of the high-oxygen aqueous solution in the high-oxygen water storage chamber 1 and the pump flow rate to the processor 203, and the control command parameter input module 202 starts/stops the device, and accelerates/decelerates the injection power. The instruction parameters are input to the processor 203, and after being processed by the processor 203, the signals are sent to the raw liquid shut-off valve 4 through the control parameter output module 204, and the flow regulating pump 5 is adjusted to realize the operation of the device, so that the injection power device is Connect with the application system in which it is located. The upper server 206 is connected to the communication module 205 by wire or wirelessly, and the user can also send an instruction to the processor 203 via the communication module 205 via the upper server 206.

 [0024] The injection power compartment 3 of the present application adopts a bell mouth structure, and the input end of the injection power compartment 3 is connected to the output end of the catalytic reduction reaction chamber 9, and the mixture of fresh water and nascent oxygen generated in the reduction reaction is described. The small port end of the injection power compartment 3 enters the injection power compartment 3, and generates a propulsive force of advancement by interacting with the external medium through the large mouth end.

 [0025] Embodiment 2:

[0026] As shown in FIG. 3, a flight device with a power unit of the present application, an embodiment thereof, includes a flight wing suit 18, a flight monitor 12, and a power unit in the first embodiment, a flight monitor 12 and The power unit is disposed on the flight wing suit 18, and after the power unit is used for catalytic reduction reaction by the high oxygen water liquid solution, the generated jet kinetic energy is used to drive the flight wing assembly 18, and the flight monitor 12 is used to adjust the magnitude of the jet kinetic energy. The flight speed of the flight wing assembly 18 is adjusted. The control regulator 8 in the power unit in this embodiment may be provided separately or integrated with the flight monitor 12 as a whole.

 [0027] The flying wing device with power device of the present application may further include a backpack 21 including a bag body, a strap 17 and a waist belt 16, a bottom portion of the bag body, and a power device portion disposed inside the bag body and jetting power The compartment 3 is placed outside the bag through the cornice, and the harness 17 and the waistband 16 are used to bind the bag to the flight wing suit 18.

 [0028] In one embodiment, the flight wing suit 18 may be an integrated structure. The batwings of the flying wing suits 18 may be provided with batwings 19, and the underarms of the flying wing suits 19 may be provided with connecting tails 20.

 [0029] The flight monitor 12 includes a flight monitoring box, a hand controller 13 and a digital display and sound unit (not shown), a flight monitoring box 12, an actual monitoring for flight state parameters, a flow control valve adjustment, and a process. The display of the status parameters, the hand controller and the digital display and sound unit are respectively connected to the flight monitoring box 12.

 [0030] The flight monitoring box 12, the hand controller 13 and the built-in earphone 14 together constitute a flight monitor to implement flight process monitoring and safety prompts, wherein the flight monitoring box 12 has the basic circuit structure of the terminal in the above example. The operating state parameter sampling input module includes various types of sensors capable of collecting data, and can realize monitoring of state parameters including flight altitude, flight speed, flight time, ambient temperature and humidity, and remaining content of flying power materials, and accepting The flow control valve is actually adjusted online under the command of the hand controller 13, and the power of the flight monitor 12 is supplied by the battery as a whole. The flight monitoring box 12 is bound to the waist belt 16 and placed in front of the human body to facilitate the display of the state parameters displayed on the flight monitoring box 12 by the eye during flight, and the flight controller parameters can be selected by the manual controller 13 to be built in. The headphone 14 of the coat is reported to the flighter by the voice, especially the safety warning of the remaining materials is beneficial to the flighter. Even if the flight strategy is adjusted, the hand controller should be small and can be placed in the transparent pocket of the palm for blind operation. .

 [0031] The above is a further detailed description of the present application in conjunction with the specific embodiments, and the specific implementation of the application is not limited to the description. For the ordinary person skilled in the art to which the present invention pertains, several simple deductions or substitutions may be made without departing from the spirit of the present application.

 technical problem

 Problem solution

 Advantageous effects of the invention

Claims

Claim  [Claim 1] A power unit, comprising: a control regulator and a high-oxygen water storage chamber, a catalytic reduction reaction chamber, and an injection power cabin, which are sequentially connected, wherein the control regulator is used to regulate the high-oxygen water a high-oxygen water liquid flowing into the catalytic reduction reaction chamber in the storage chamber, and a high-oxygen water liquid stored in the high-oxygen water storage chamber, after entering the catalytic reduction reaction chamber, is reduced in the catalytic reduction reaction chamber The reaction kinetic energy generated in the reduction reaction forms a driving force through the injection power compartment.  [Claim 2] The power unit according to claim 1, wherein the control regulator includes a terminal and a liquid shutoff valve, and the raw liquid shutoff valve is disposed in the high oxygen water storage chamber and catalytic reduction Between the reaction chambers, the terminal is configured to control the raw liquid shut-off valve according to a user's instruction.  [Claim 3] The power unit according to claim 2, wherein the control regulator further includes a flow regulating pump, the flow regulating pump is connected in series with the raw liquid shutoff valve, and the processor is further used The flow regulating pump is controlled according to a user's instruction.  [Claim 4] The power unit according to claim 1, wherein the control regulator includes a flow rate adjustment pump, and the flow rate adjustment pump is disposed in the high oxygen water storage chamber and Between the catalytic reduction reaction chambers, the flow regulating pump is provided with a plurality of adjustment gear positions including 0 to MAX, and the terminal is configured to control the flow regulating pump according to a user's instruction. The power device according to any one of claims 2 to 4, wherein the terminal comprises a processor, an operating state parameter sampling input module, a control command parameter input module, a control parameter output module, and a communication module, the input end of the processor is bidirectionally connected to the running state parameter sampling input module and the control command parameter input module, and the output end of the processor is bidirectionally connected to the control parameter output module and the communication module, the processor The raw liquid shutoff valve and the flow regulating pump are controlled by an output of the control parameter output module. [Claim 6] The power unit according to any one of claims 1 to 4, wherein the injection power compartment adopts a bell mouth structure, and an input end of the injection power compartment and the catalytic reduction reaction The output end of the chamber is connected, and a mixture of fresh water and nascent oxygen generated in the reduction reaction enters the injection power cabin through the small mouth end of the injection power cabin, and generates a forward push through interaction between the large mouth end and the external medium. force. The power unit according to claim 6, wherein said high oxygen water storage chamber is provided with a feed port. The power unit according to claim 6, wherein said catalytic reduction reaction chamber is provided with a slit for introducing or removing a catalyst. A flying wing device having a power unit, comprising a flying wing suit, characterized by further comprising a flight monitor and the power unit according to any one of claims 1 to 8, said flight monitor and said power The device is disposed on the flying wing suit, wherein the power device is configured to drive the flying wing device by an injection kinetic energy generated by a catalytic reduction reaction of a high oxygen aqueous liquid solution, wherein the flight monitor is configured to adjust a magnitude of the jet kinetic energy Adjusting the flight speed of the flying wing. A flying wing device with a power unit according to claim 9, further comprising a backpack, the backpack comprising a bag body, a shoulder strap and a waist belt, wherein the bottom of the bag body is provided with a mouthpiece, and the power device is partially disposed Within the enclosure and the jet power compartment is placed outside the enclosure through the cornice, the harness and the waistband are used to bind the enclosure to the flight wing garment. A flying wing device with a power unit according to claim 9, wherein said flying wing suit is an integrated structure. A flying wing device with a power unit according to claim 9, wherein a batwing is provided under the arm of the flying wing suit. A flying wing device with a power unit according to claim 12, wherein the flying wing suit is provided with a connecting tail. A flying wing device with a power unit according to claim 9, wherein said flight monitor comprises a flight monitoring box, a hand controller and a digital display and sound unit, said flight monitoring box for flight state parameters The actual monitoring, the adjustment of the flow control valve, and the display of the process state parameters, the flight monitoring box, the hand controller, and the digital display and sound unit respectively The processor connection