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WO2000064719A1 - Procede et de creation d'une decharge d'air et d'une poussee pour vehicule, dispositif de mise en oeuvre de ce procede et aeronef a effet de surface comprenant un dispositif de creation de decharge d'air et de poussee - Google Patents

Procede et de creation d'une decharge d'air et d'une poussee pour vehicule, dispositif de mise en oeuvre de ce procede et aeronef a effet de surface comprenant un dispositif de creation de decharge d'air et de poussee Download PDF

Info

Publication number
WO2000064719A1
WO2000064719A1 PCT/RU2000/000114 RU0000114W WO0064719A1 WO 2000064719 A1 WO2000064719 A1 WO 2000064719A1 RU 0000114 W RU0000114 W RU 0000114W WO 0064719 A1 WO0064719 A1 WO 0064719A1
Authority
WO
WIPO (PCT)
Prior art keywords
air
channel
vehicle
blower
blowing
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Ceased
Application number
PCT/RU2000/000114
Other languages
English (en)
Russian (ru)
Inventor
Alexandr Mikhailovich Makienko
Andrei Vladimirovich Pokrepa
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to AU46296/00A priority Critical patent/AU4629600A/en
Publication of WO2000064719A1 publication Critical patent/WO2000064719A1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V3/00—Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
    • B60V3/08—Aircraft, e.g. air-cushion alighting-gear therefor
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V1/00—Air-cushion
    • B60V1/08—Air-cushion wherein the cushion is created during forward movement of the vehicle by ram effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V1/00—Air-cushion
    • B60V1/14—Propulsion; Control thereof
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V1/00—Air-cushion
    • B60V1/22—Air-cushion provided with hydrofoils
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B60—VEHICLES IN GENERAL
    • B60V—AIR-CUSHION VEHICLES
    • B60V3/00—Land vehicles, waterborne vessels, or aircraft, adapted or modified to travel on air cushions
    • B60V3/06—Waterborne vessels

Definitions

  • the invention relates to hazardous substances in an air bag. in particular. May be used for cables. payroll board. designed to accommodate loads and ⁇ . e. Also, the invention may be used in aviation as a standard missile system. is a one-time mover of horizontal displacement. xxia. and also planes or planes. dynamic air-breathing effects.
  • the flying device is known - the balloon. a good fuselage. ⁇ - mul ⁇ . horizontal and vertical movement and air-reactive power
  • a flying device is known - a plane, containing a fuselage with
  • the screen is known. enclosed fuselage with cab for crew. Roundabouts with aerodynamic controls and a propulsion propulsion system. When this happens, the device is equipped with an air inlet and a traction in the form of an air inlet chamber. Designed bobo-
  • the propulsion system is made in the form of a diameter fan and is placed along the arm. Lateral fenders are placed on the arm of the boiler and are made in the form of inflatable elements from an elastic material. and the front one is installed
  • SIGNIFICANT FOX (DR. 26) ⁇ 00/64719 2 ⁇ / ⁇ / 00114
  • a quick transfusion device on a dynamic air bag is known. a good lack of energy and a cost-effective installation with mixed front and rear air blowers.
  • the nozzle is mounted with a deflecting nozzle.
  • the upper part of the arm was carried out with a fatal loss. shortly mixed in the direction of the nose from the plane of the mid-section. and it was located in the lower part of it, but it was not performed with the directional channels.
  • Each of the gears is equipped with one of the airships of a supercharged engine. moreover, the angle of inclination of each of the directional channels of the angle of inclination is inclined to the opposite
  • a secured horn or an integrated curtain is installed, which performs the function of the curtain of the curtain.
  • the screen is known. means of creating an air discharge and traction and
  • a well-known screen contains a fuselage. ⁇ . ooperation. air handling unit and traction device. inclusive of a simplicity and a compact, simple and practical design. Retracted from the nose of the tunzel. equipped with a front or rear center washer and equipped with an adjustable wiper for the end of life. The method of creating an air discharge and traction in a known environment
  • SIGNIFICANT FOX (DR. 26) ⁇ ⁇ 00/64719 ⁇ / ⁇ / 00114
  • the adjusted key is released to the last, the default and turns on the power installation. by airing in the tunnels.
  • a quick adjustment is made by changing the angle of the seam to be sewn. and also with the help of a special store tunnel 5 la. and this airbags. Providing a free download plan. traction force is generated.
  • the described expansion devices have a low amphibiousness and modesty
  • the objective of the claimed invention is the elimination of these shortcomings.
  • the claimed inventions may be used only in the case of ammunition (hydraulic equipment), as well as the use of ammunition (dynamically). and for transverse neighbors of other types (including incidents).
  • a commercial result for the device of creating an air discharge and a thrust for a transport device is achieved due to the device.
  • 15 v ⁇ lyuchayushem ⁇ v ⁇ nuyu v ⁇ zduh ⁇ duvnuyu sil ⁇ vuyu us ⁇ an ⁇ v ⁇ u, ⁇ as ⁇ l ⁇ zhennuyu in n ⁇ s ⁇ v ⁇ y chas ⁇ i ⁇ ans ⁇ n ⁇ g ⁇ s ⁇ eds ⁇ va, ⁇ y ⁇ y with n ⁇ s ⁇ v ⁇ y chas ⁇ i ⁇ d ⁇ ln ⁇ ⁇ as ⁇ l ⁇ zhenny ⁇ dduvn ⁇ y ⁇ anal and sha ⁇ ni ⁇ n ⁇ us ⁇ an ⁇ vlenny in ⁇ n ⁇ ev ⁇ y chas ⁇ i ⁇ anala shi ⁇ , vsh ⁇ lnyayushy ⁇ un ⁇ iyu ⁇ m ⁇ v ⁇ y curtain ⁇ dduvn ⁇ y ⁇ anal ⁇ b- ⁇
  • SIGNIFICANT FOX (DR. 26) ⁇ 00/64719 ⁇ / ⁇ / 00114
  • the inflatable channel is designed in the form of a 5th convenient version in a cross-section of a cut-out in the mixing part of the fuselage such a way. that the side channels of the channel, together with the corresponding mixing part of the fuselage, perform the skego function.
  • the direct air-blowing power unit can be cleaned in the form of a rotary fan with variable pitch.
  • the fan channel can be installed 15;
  • the wagon can be equipped with 20 wife of a wheeled chassis.
  • FIG. 2 shows the main view of the device with the device for creating an unloading and traction: 25 per FIG. 3 shown in the picture.
  • view of light on ⁇ ig. 4 illustrated view of the front.
  • the method of creating an air discharge and a traction for a transport device is implemented with the use of an air discharge device and a traction ( ⁇ ). Due to the fact that air discharges and thrusts are in place, the transport system will be discharged at the expense of the vehicle.
  • the 1st air blower unit 1 can be made in the form of motors, which can be tricked out by rotating the 7 fans with variable steps.
  • the ergonomate consumes around 9, vertical 10 and a horizontal 11 unit.
  • the chassis may also be equipped with a wheeled chassis. 12.
  • the device with the device of the air discharge and the traction operates the following way, realizing the claimed method of the creation of the air discharge.
  • the air duct which is used in the inlet part of the air duct 3, is designed to be drained from the air; Exit through this shell determines the amount of traction. Developed by air power plant.
  • SIGNIFICANT FOX (DR. 26) ⁇ 00/64719 ⁇ / ⁇ / 00114
  • the high pressures of the processors ensure that they have a practical, complete air discharge. there is high amphibiousness. substantially more
  • the power circuit is suitable for the creation of an air discharge and a pull rod that is equally suitable for use as a military vehicle. ⁇ ak and ⁇ ⁇ réelle ⁇ ley. as well as for payloads of the territory of the Republic of North Korea and Siniri and ⁇ . ⁇ .

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transportation (AREA)
  • Mechanical Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

Cette invention se rapporte au domaine des véhicules sur coussin d'air, et peut notamment être utilisée pour des navires et des plates-formes de transport servant à déplacer des charges, ainsi que pour des hydravions, etc. Ce procédé de création de décharge d'air et de poussée pour véhicule consiste à dévier le flux d'air provenant d'une installation motrice de soufflage d'air qui est située dans la partie avant du véhicule. Ce procédé consiste ensuite à ajuster l'angle d'inclinaison d'un volet qui joue le rôle de jupe arrière et qui est monté pivotant dans la partie d'extrémité du canal de soufflage. Ce canal est symétrique par rapport à l'axe longitudinal du véhicule, et le débit d'air généré par l'installation motrice de soufflage d'air est entièrement dirigé vers le canal de soufflage. Ce dernier est formé dans la partie inférieure de la partie déplacement du corps du véhicule, et est en forme de ∏ au niveau de sa section transversale. La partie déplacement du corps, dans la zone des parois latérales du canal de soufflage en forme de ∏, joue en outre le rôle d'ailerons. Ce dispositif et l'aéronef à effet de surface comprennent une installation motrice et de soufflage d'air rotative, un canal de soufflage longitudinal, et un volet monté pivotant dans la partie extrémité dudit canal.
PCT/RU2000/000114 1999-04-07 2000-04-05 Procede et de creation d'une decharge d'air et d'une poussee pour vehicule, dispositif de mise en oeuvre de ce procede et aeronef a effet de surface comprenant un dispositif de creation de decharge d'air et de poussee Ceased WO2000064719A1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU46296/00A AU4629600A (en) 1999-04-07 2000-04-05 Method for generating an air discharge and a thrust for a vehicle, device for realising the same and wing surface-effect aircraft comprising this air-discharge and thrust generating device

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
RU99106391 1999-04-07
RU99106391A RU2139212C1 (ru) 1999-04-07 1999-04-07 Способ создания воздушной разгрузки и тяги для транспортного средства, устройство для его осуществления и экранолет с устройством создания воздушной разгрузки и тяги

Publications (1)

Publication Number Publication Date
WO2000064719A1 true WO2000064719A1 (fr) 2000-11-02

Family

ID=20217824

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/RU2000/000114 Ceased WO2000064719A1 (fr) 1999-04-07 2000-04-05 Procede et de creation d'une decharge d'air et d'une poussee pour vehicule, dispositif de mise en oeuvre de ce procede et aeronef a effet de surface comprenant un dispositif de creation de decharge d'air et de poussee

Country Status (3)

Country Link
AU (1) AU4629600A (fr)
RU (1) RU2139212C1 (fr)
WO (1) WO2000064719A1 (fr)

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2235654C2 (ru) * 1999-12-29 2004-09-10 Данилов Владимир Петрович Экраноплан
RU2273572C2 (ru) * 2004-04-15 2006-04-10 Владимир Петрович Данилов Экраноплан
UA83820C2 (ru) * 2005-09-13 2008-08-26 Геннадий Алексеевич Павлов Экраноплан и его взлетно-посадочный комплекс
RU2297933C1 (ru) * 2005-12-29 2007-04-27 Виктор Георгиевич Сергеев Экраноплан
DE102009004239A1 (de) 2009-01-05 2010-07-08 Ivan Novikov-Kopp Verfahren zur komplexen Erhöhung von Aerodynamik- und Transporteigenschaften, Bodeneffektfahrzeug zur Ausführung des Verfahrens (Varianten) und Flugverfahren

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU18077A1 (ru) * 1929-01-19 1930-09-30 А.Н. Шамарин Амортизирующее чешуйчатое днище гидросамолета
US3826449A (en) * 1973-09-21 1974-07-30 Us Navy Inflation and evacuation system for an air cushion landing system
GB2120990A (en) * 1982-05-28 1983-12-14 Kjoelseth Paul Ground effect vehicle or aerofoil boat
SU1336422A1 (ru) * 1985-12-05 1999-05-27 Иркутский политехнический институт Экраноплан по схеме "утка"

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4010877A1 (de) * 1990-04-04 1991-10-10 Rhein Flugzeugbau Gmbh Staufluegelboot
RU2057664C1 (ru) * 1990-08-13 1996-04-10 Акционерное общество открытого типа "Центральное конструкторское бюро по судам на подводных крыльях им.Р.Е.Алексеева" Скеговый транспортный аппарат на динамической воздушной подушке
RU2097229C1 (ru) * 1993-07-05 1997-11-27 Леонид Николаевич Наволоцкий Экраноплан и способ продольного управления экранопланом
RU3917U1 (ru) * 1993-09-06 1997-04-16 Владимир Иосифович Петросян Экраноплан

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SU18077A1 (ru) * 1929-01-19 1930-09-30 А.Н. Шамарин Амортизирующее чешуйчатое днище гидросамолета
US3826449A (en) * 1973-09-21 1974-07-30 Us Navy Inflation and evacuation system for an air cushion landing system
GB2120990A (en) * 1982-05-28 1983-12-14 Kjoelseth Paul Ground effect vehicle or aerofoil boat
SU1336422A1 (ru) * 1985-12-05 1999-05-27 Иркутский политехнический институт Экраноплан по схеме "утка"

Also Published As

Publication number Publication date
RU2139212C1 (ru) 1999-10-10
AU4629600A (en) 2000-11-10

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