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RU93043825A - COMBINED AIRCRAFT - Google Patents

COMBINED AIRCRAFT

Info

Publication number
RU93043825A
RU93043825A RU93043825/11A RU93043825A RU93043825A RU 93043825 A RU93043825 A RU 93043825A RU 93043825/11 A RU93043825/11 A RU 93043825/11A RU 93043825 A RU93043825 A RU 93043825A RU 93043825 A RU93043825 A RU 93043825A
Authority
RU
Russia
Prior art keywords
aircraft
tunnel
lifting screw
landing
land
Prior art date
Application number
RU93043825/11A
Other languages
Russian (ru)
Other versions
RU2012512C1 (en
Inventor
В.М. Капин
В.А. Ивчин
Н.С. Павленко
Е.Л. Погребинский
В.В. Субботин
О.Н. Майоров
Original Assignee
Фирма "ВИСТ"
Filing date
Publication date
Application filed by Фирма "ВИСТ" filed Critical Фирма "ВИСТ"
Priority to RU9393043825A priority Critical patent/RU2012512C1/en
Priority claimed from RU9393043825A external-priority patent/RU2012512C1/en
Application granted granted Critical
Publication of RU2012512C1 publication Critical patent/RU2012512C1/en
Priority to US08/432,148 priority patent/US5873545A/en
Priority to EP94927134A priority patent/EP0667283B1/en
Priority to ES94927134T priority patent/ES2113676T3/en
Priority to CZ951213A priority patent/CZ121395A3/en
Priority to NZ273413A priority patent/NZ273413A/en
Priority to PCT/RU1994/000207 priority patent/WO1995007215A1/en
Priority to CA002148797A priority patent/CA2148797A1/en
Priority to DE59405105T priority patent/DE59405105D1/en
Priority to PL94309029A priority patent/PL309029A1/en
Priority to JP7508617A priority patent/JPH08503672A/en
Priority to AU76682/94A priority patent/AU679564B2/en
Priority to NO951788A priority patent/NO951788L/en
Priority to FI952208A priority patent/FI952208A/en
Publication of RU93043825A publication Critical patent/RU93043825A/en

Links

Claims (1)

Использование: изобретение относится к авиастроению и может использоваться в летательных аппаратах вертикального взлета и посадки. Сущность изобретения: комбинированный летательный аппарат содержит корпус в виде центрального толстого крыла с вертикальным открытым тоннелем, в котором установлен подъемный винт. Аппарат имеет также боковые крылья, хвостовое оперение и маршевые винты, и оснащен посадочным устройством на воздушной подушке, охватывающим выход из тоннеля. Особенностью изобретения является согласование размеров подъемного винта и посадочного устройства на воздушной подушке. Силовая установка летательного аппарата включает два блока двигателей, размещенных с двух сторон тоннеля и соединенных с подъемным винтом и маршевыми винтами. Изобретение позволяет летательному аппарату взлетать и садиться на неподготовленные площадки, а также совершить посадку при отказе одного из блоков двигателей.Usage: the invention relates to aircraft manufacturing and can be used in aircraft of vertical take-off and landing. The inventive combined aircraft contains a body in the form of a central thick wing with a vertical open tunnel, in which a lifting screw is installed. The device also has side wings, tail and marching propellers, and is equipped with an air cushion landing device covering the exit from the tunnel. A feature of the invention is the coordination of the size of the lifting screw and landing device on an air cushion. The power plant of the aircraft includes two engine blocks located on both sides of the tunnel and connected to the lifting screw and propellers. The invention allows the aircraft to take off and land on unprepared sites, and also to land in case of failure of one of the engine blocks.
RU9393043825A 1993-09-07 1993-09-07 Hybrid flying vehicle RU2012512C1 (en)

Priority Applications (14)

Application Number Priority Date Filing Date Title
RU9393043825A RU2012512C1 (en) 1993-09-07 1993-09-07 Hybrid flying vehicle
JP7508617A JPH08503672A (en) 1993-09-07 1994-09-02 Compound airplane
AU76682/94A AU679564B2 (en) 1993-09-07 1994-09-02 Hybrid aircraft
CZ951213A CZ121395A3 (en) 1993-09-07 1994-09-02 Combined aircraft
DE59405105T DE59405105D1 (en) 1993-09-07 1994-09-02 COMBINED AIRCRAFT
ES94927134T ES2113676T3 (en) 1993-09-07 1994-09-02 HYBRID AIRCRAFT.
US08/432,148 US5873545A (en) 1993-09-07 1994-09-02 Combined flying machine
NZ273413A NZ273413A (en) 1993-09-07 1994-09-02 Vtol aircraft with rotor in central vertical duct powered by propellor drives
PCT/RU1994/000207 WO1995007215A1 (en) 1993-09-07 1994-09-02 Hybrid aircraft
CA002148797A CA2148797A1 (en) 1993-09-07 1994-09-02 Combined flying machine
EP94927134A EP0667283B1 (en) 1993-09-07 1994-09-02 Hybrid aircraft
PL94309029A PL309029A1 (en) 1993-09-07 1994-09-02 Combination-type aircraft
FI952208A FI952208A (en) 1993-09-07 1995-05-08 Combined aircraft
NO951788A NO951788L (en) 1993-09-07 1995-05-08 Combined airplane

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
RU9393043825A RU2012512C1 (en) 1993-09-07 1993-09-07 Hybrid flying vehicle

Publications (2)

Publication Number Publication Date
RU2012512C1 RU2012512C1 (en) 1994-05-15
RU93043825A true RU93043825A (en) 1997-04-10

Family

ID=20147191

Family Applications (1)

Application Number Title Priority Date Filing Date
RU9393043825A RU2012512C1 (en) 1993-09-07 1993-09-07 Hybrid flying vehicle

Country Status (14)

Country Link
US (1) US5873545A (en)
EP (1) EP0667283B1 (en)
JP (1) JPH08503672A (en)
AU (1) AU679564B2 (en)
CA (1) CA2148797A1 (en)
CZ (1) CZ121395A3 (en)
DE (1) DE59405105D1 (en)
ES (1) ES2113676T3 (en)
FI (1) FI952208A (en)
NO (1) NO951788L (en)
NZ (1) NZ273413A (en)
PL (1) PL309029A1 (en)
RU (1) RU2012512C1 (en)
WO (1) WO1995007215A1 (en)

Families Citing this family (41)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2092381C1 (en) * 1995-10-31 1997-10-10 Акционерное общество закрытого типа "Тюменьэкотранс" Hybrid airship
DE19752758C2 (en) * 1997-11-28 2001-07-12 Hans Fruth Vertical take-off and landing transport aircraft (fuselage glider)
USD418805S (en) * 1998-11-24 2000-01-11 Sikorsky Aircraft Corporation Unmanned multi-mode vertical take off and landing aircraft
US6270038B1 (en) 1999-04-22 2001-08-07 Sikorsky Aircraft Corporation Unmanned aerial vehicle with counter-rotating ducted rotors and shrouded pusher-prop
US6170778B1 (en) * 1999-04-22 2001-01-09 Sikorsky Aircraft Corporation Method of reducing a nose-up pitching moment on a ducted unmanned aerial vehicle
DZ3349A1 (en) * 2000-07-28 2002-02-07 Henkel Kgaa NEW AMYLOLYTIC ENZYME FROM BACILLUS SP. A 7-7 (DSM 12368) AND WASHING AND CLEANING PRODUCTS CONTAINING SAID AMYLOLYTIC ENZYME
US6848649B2 (en) * 2000-10-03 2005-02-01 Charles Gilpin Churchman V/STOL biplane aircraft
US6672538B2 (en) * 2002-05-23 2004-01-06 Sikorsky Aircraft Corporation Transmission for a coaxial counter rotating rotor system
WO2004101357A2 (en) * 2002-08-30 2004-11-25 Qaxu Technology Inc. Homeostatic flying hovercraft
US6732972B2 (en) 2002-09-13 2004-05-11 Frank S. Malvestuto, Jr. High-lift, low-drag, stall-resistant airfoil
US6715574B1 (en) * 2002-10-18 2004-04-06 Aeromobile, Inc. Airstream control system for a hovercraft
US7059931B2 (en) * 2003-05-27 2006-06-13 Veratech Aero-Rpv Corporation Reduced visibility rotorcraft and method of controlling flight of reduced visibility rotorcraft
US20050230525A1 (en) * 2004-03-30 2005-10-20 Paterro Von F C Craft with magnetically curved space
US7946526B2 (en) * 2004-11-05 2011-05-24 Nachman Zimet Rotary-wing vehicle system
WO2007120199A2 (en) 2005-11-09 2007-10-25 Morgan Aircraft, Llc Aircraft attitude control configuration
FR2929243B1 (en) * 2008-03-25 2010-04-23 Eurocopter France RAPID HYBRID HELICOPTER WITH EXTENDABLE HIGH DISTANCE
US8220737B2 (en) * 2008-06-06 2012-07-17 Frontline Aerospace, Inc. VTOL aerial vehicle
JP2010023820A (en) * 2008-07-22 2010-02-04 Keiichi Aoyanagi Vertical taking-off and landing aircraft
US8240597B2 (en) * 2008-08-06 2012-08-14 Honeywell International Inc. UAV ducted fan lip shaping
RU2422309C1 (en) * 2010-01-11 2011-06-27 Александр Иосифович Филимонов Combined flight vehicle
CN101837195B (en) * 2010-01-21 2012-02-08 罗之洪 Model airplane with vertical takeoff and landing
RU2010104373A (en) * 2010-02-08 2011-08-20 Александр Иосифович Филимонов (RU) AIRPLANE AIRPLANE WITH AEROSTATIC UNLOADING
US8579227B2 (en) * 2011-01-24 2013-11-12 J. Kellogg Burnham Vertical and horizontal flight aircraft “sky rover”
PL2690010T3 (en) 2012-07-27 2015-03-31 Airbus Helicopters Deutschland GmbH Compound helicopter with tail booms
US9004973B2 (en) 2012-10-05 2015-04-14 Qfo Labs, Inc. Remote-control flying copter and method
EP2738091B1 (en) * 2012-11-30 2015-07-22 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Vertical take-off and landing (VTOL) aerial vehicle and method of operating such a VTOL aerial vehicle
CN103231803A (en) * 2013-04-27 2013-08-07 哈尔滨飞机工业集团有限责任公司 Small unmanned aircraft configuration
CN103448910A (en) * 2013-08-31 2013-12-18 西北工业大学 Aircraft capable of vertically taking off and landing at high speed
RU2546359C1 (en) * 2014-02-18 2015-04-10 Александр Иосифович Филимонов Aerodynamic ground-effect craft of off-aerodrome location
GB2528489A (en) 2014-07-23 2016-01-27 Cassidian Ltd Improvements in and relating to unmanned aerial vehicles
CN109808877A (en) * 2014-12-26 2019-05-28 深圳智航无人机有限公司 A kind of unmanned plane variable wing and its method
US9914528B2 (en) * 2015-02-25 2018-03-13 Embraer S.A. Airframe-integrated propeller-driven propulsion systems
CN105015770A (en) * 2015-07-29 2015-11-04 张飞 Vertical take-off and landing aircraft with wing body blended with single duct
RU2603808C1 (en) * 2015-10-22 2016-11-27 Российская Федерация в лице Министерства промышленности и торговли Российской Федерации (Минпромторг России) Aircraft with air-cushion landing gear
US10258888B2 (en) 2015-11-23 2019-04-16 Qfo Labs, Inc. Method and system for integrated real and virtual game play for multiple remotely-controlled aircraft
GB2555439A (en) * 2016-10-27 2018-05-02 Mono Aerospace Ip Ltd Vertical take-off and landing aircraft and control method
USD808329S1 (en) * 2017-01-18 2018-01-23 Aurora Flight Sciences Corporation Lenticular aircraft
US11712637B1 (en) 2018-03-23 2023-08-01 Steven M. Hoffberg Steerable disk or ball
CN109335004B (en) * 2018-11-30 2024-04-26 福建星图智控科技有限公司 Micro unmanned aerial vehicle equipped with hybrid power
CN113353254B (en) * 2021-07-14 2023-02-28 空中舞者(威海)航空动力技术有限公司 Vertical take-off and landing gyroplane
WO2024035714A1 (en) * 2022-08-09 2024-02-15 Pete Bitar Compact and lightweight drone delivery device called an arcspear electric jet drone system having an electric ducted air propulsion system and being relatively difficult to track in flight

Family Cites Families (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3002709A (en) * 1955-12-19 1961-10-03 C L Cochran And Associates Aircraft adapted for vertical ascent and descent
US3049320A (en) * 1958-07-11 1962-08-14 Charles J Fletcher Annular wing aircraft
US2988301A (en) * 1958-10-28 1961-06-13 Charles J Fletcher Ducted fan aircraft
DE1246422B (en) * 1962-07-31 1967-08-03 British Aircraft Corp Ltd Hovercraft with side jet curtains
US3221831A (en) * 1963-12-13 1965-12-07 Donglas Aircraft Company Inc Winged surface effect vehicles
USRE29023E (en) * 1965-10-22 1976-11-02 Means and method of rotor augmented lift for airplanes
US3559921A (en) * 1969-04-24 1971-02-02 Eugene L Timperman Standing take-off and landing vehicle (a gem/stol vehicle)
US3689011A (en) * 1969-07-11 1972-09-05 Dorant Torelli Aircraft
GB1331655A (en) * 1971-04-01 1973-09-26 Pedrick A P Design of saucer shaped flying machines
GB1400034A (en) * 1972-10-23 1975-07-16 Scenic Flying Ltd Improvements in or relating to aircraft
GB1405737A (en) * 1974-03-08 1975-09-10 Pedrick A P Large flat based aircraft capable of hovering flight particularly for the transport of lengths of pipe line
FR2303709A2 (en) * 1975-03-10 1976-10-08 Ferre Pierre Vertical take off and landing aircraft - has lifting rotor within fuselage with hinged deflection shutters
US4196877A (en) * 1977-06-15 1980-04-08 Mutrux Jean L Aircraft
US4298175A (en) * 1979-03-21 1981-11-03 Textron Inc. Airplane wing and undercarriage construction
SE446965B (en) * 1984-05-17 1986-10-20 Skold Bjorn Ake SVEVARKONSTRUKTION
US5035377A (en) * 1985-02-28 1991-07-30 Technolizenz Establishment Free standing or aircraft lift generator
US4757962A (en) * 1987-04-09 1988-07-19 Terrence Grant Amphibious vehicle
US5152478A (en) * 1990-05-18 1992-10-06 United Technologies Corporation Unmanned flight vehicle including counter rotating rotors positioned within a toroidal shroud and operable to provide all required vehicle flight controls
US5277380A (en) * 1992-06-22 1994-01-11 United Technologies Corporation Toroidal fuselage structure for unmanned aerial vehicles having ducted, coaxial, counter-rotating rotors

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