GB926613A - Improvements in and relating to composite vertical take-off aircraft - Google Patents
Improvements in and relating to composite vertical take-off aircraftInfo
- Publication number
- GB926613A GB926613A GB1186358A GB1186358A GB926613A GB 926613 A GB926613 A GB 926613A GB 1186358 A GB1186358 A GB 1186358A GB 1186358 A GB1186358 A GB 1186358A GB 926613 A GB926613 A GB 926613A
- Authority
- GB
- United Kingdom
- Prior art keywords
- platform
- aircraft
- bar
- take
- engines
- 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.)
- Expired
Links
- 239000002131 composite material Substances 0.000 title abstract 4
- 238000010586 diagram Methods 0.000 abstract 1
- 230000006641 stabilisation Effects 0.000 abstract 1
- 238000011105 stabilization Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D5/00—Aircraft transported by aircraft, e.g. for release or reberthing during flight
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0091—Accessories not provided for elsewhere
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
Abstract
926,613. Composite aircraft. ENGLISH ELECTRIC CO. Ltd. April 10, 1959 [April 14, 1958], No. 11863/58. Class 4. A composite aircraft comprises a flying platform having a delta-shaped body 10 of aerodynamic sectional profile provided with stabilizer-fins 11, faired telescopic supporting legs 13, a pair of cockpits 12 and a plurality of turbo-jet engines 17 or ducted fans which may be swung bodily about transverse axes or may be provided with means to deflect the exhaust to provide initial vertical take-off and subsequent forward propulsion. Compressed air nozzles 18 or ducted fans are provided for control and stabilization. An aircraft to be flown on to and off the platform comprises a delta wing 1, fuselage 2 and a triangle undercarriage 3 with a retractable hook bar 5 located between and slightly in front of the main under-carriage legs, said bar being positioned to engage a forwardly-open hook-on gear 15 on the platform. The aircraft is loaded on to the platform by means of a cable operated by a winch 16 on the platform, which draws the aircraft up ramps 14, the rear legs 13 being telescoped to lower the back end of the platform for this purpose. Alternatively the aircraft could be loaded in a similar manner from the front, in which ease the twin cockpits 12 could be replaced by a single centrally disposed one. During take-off the platform is flown to appropriate altitude and a speed in excess of the stalling speed of the aeroplane, which is then free to fly off under its own powerupon release of connection 5, 15. During landing and when the aeroplane has almost alighted on the platform, the latter is accelerated in flight relative to the aircraft to engage the hooking gear 15 with the bar 5. The composite aircraft then carries out a vertical landing under the power of engines 17. A co-ordinating system comprising sensing devices, autostabilisers and computing devices is illustrated by block diagrams in Fig. 5 (not shown), whereby the relative movements of the aircraft and the platform may co-ordinate during landing and take-off. It is stated that the arrangement of lift engines on the platform provides a gas curtain for a ground cushion. Reference has been directed by the Comptroller to Specification 882,073.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1186358A GB926613A (en) | 1958-04-14 | 1958-04-14 | Improvements in and relating to composite vertical take-off aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1186358A GB926613A (en) | 1958-04-14 | 1958-04-14 | Improvements in and relating to composite vertical take-off aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB926613A true GB926613A (en) | 1963-05-22 |
Family
ID=9994064
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1186358A Expired GB926613A (en) | 1958-04-14 | 1958-04-14 | Improvements in and relating to composite vertical take-off aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB926613A (en) |
Cited By (15)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3285544A (en) * | 1964-02-26 | 1966-11-15 | Industrial Nucleonics Corp | Mid-air refueling system |
US4462560A (en) * | 1982-01-26 | 1984-07-31 | The United States Of America As Represented By The Secretary Of The Air Force | Airplane take-off system |
US4678141A (en) * | 1981-03-16 | 1987-07-07 | Grumman Aerospace Corporation | Aircraft launcher and retriever |
US5000398A (en) * | 1988-10-25 | 1991-03-19 | Rashev Michael S | Flying multi-purpose aircraft carrier and method of V/STOL assisted flight |
EP0581513A1 (en) * | 1992-07-25 | 1994-02-02 | British Aerospace Public Limited Company | Vertical take-off/landing of aircraft |
DE19602890A1 (en) * | 1996-01-27 | 1997-07-31 | Daimler Benz Aerospace Ag | Device for depositing and resuming a drone |
US9010690B1 (en) | 2014-07-24 | 2015-04-21 | Abdulrahman S. J. M. Al-Heraibi | Airborne recovery system for aircraft with disabled landing gear |
CN105584640A (en) * | 2016-03-10 | 2016-05-18 | 上海洲跃生物科技有限公司 | Vertical takeoff device of carrier-based aircraft |
CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
CN106882385A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | Take off mode and its device of a kind of aircraft |
CN106915450A (en) * | 2017-03-10 | 2017-07-04 | 佛山市神风航空科技有限公司 | The landing modes and its device of a kind of aircraft |
CN106945807A (en) * | 2017-03-21 | 2017-07-14 | 常州信息职业技术学院 | A kind of unmanned air cushion platform without flight-deck aircraft carrier |
CN107618665A (en) * | 2017-09-18 | 2018-01-23 | 佛山市神风航空科技有限公司 | A kind of method and device for increasing multi-rotor aerocraft flying distance |
CN107651196A (en) * | 2017-09-18 | 2018-02-02 | 佛山市神风航空科技有限公司 | A kind of double folding multi-rotor aerocraft |
CN111452975A (en) * | 2020-04-13 | 2020-07-28 | 宋有洲 | Multifunctional aircraft |
-
1958
- 1958-04-14 GB GB1186358A patent/GB926613A/en not_active Expired
Cited By (18)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3285544A (en) * | 1964-02-26 | 1966-11-15 | Industrial Nucleonics Corp | Mid-air refueling system |
US4678141A (en) * | 1981-03-16 | 1987-07-07 | Grumman Aerospace Corporation | Aircraft launcher and retriever |
US4462560A (en) * | 1982-01-26 | 1984-07-31 | The United States Of America As Represented By The Secretary Of The Air Force | Airplane take-off system |
US5000398A (en) * | 1988-10-25 | 1991-03-19 | Rashev Michael S | Flying multi-purpose aircraft carrier and method of V/STOL assisted flight |
EP0581513A1 (en) * | 1992-07-25 | 1994-02-02 | British Aerospace Public Limited Company | Vertical take-off/landing of aircraft |
US5465923A (en) * | 1992-07-25 | 1995-11-14 | British Aerospace Plc | Vertical take-off/landing of aircraft |
DE19602890A1 (en) * | 1996-01-27 | 1997-07-31 | Daimler Benz Aerospace Ag | Device for depositing and resuming a drone |
DE19602890C2 (en) * | 1996-01-27 | 1998-10-22 | Daimler Benz Aerospace Ag | Device for depositing and resuming a drone |
US9010690B1 (en) | 2014-07-24 | 2015-04-21 | Abdulrahman S. J. M. Al-Heraibi | Airborne recovery system for aircraft with disabled landing gear |
CN105584640A (en) * | 2016-03-10 | 2016-05-18 | 上海洲跃生物科技有限公司 | Vertical takeoff device of carrier-based aircraft |
CN106043689A (en) * | 2016-07-22 | 2016-10-26 | 绵阳空天科技有限公司 | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft |
CN106043689B (en) * | 2016-07-22 | 2019-08-27 | 绵阳空天科技有限公司 | Backpack Fixed Wing AirVehicle takes off vertically auxiliary system |
CN106882385A (en) * | 2017-03-10 | 2017-06-23 | 佛山市神风航空科技有限公司 | Take off mode and its device of a kind of aircraft |
CN106915450A (en) * | 2017-03-10 | 2017-07-04 | 佛山市神风航空科技有限公司 | The landing modes and its device of a kind of aircraft |
CN106945807A (en) * | 2017-03-21 | 2017-07-14 | 常州信息职业技术学院 | A kind of unmanned air cushion platform without flight-deck aircraft carrier |
CN107618665A (en) * | 2017-09-18 | 2018-01-23 | 佛山市神风航空科技有限公司 | A kind of method and device for increasing multi-rotor aerocraft flying distance |
CN107651196A (en) * | 2017-09-18 | 2018-02-02 | 佛山市神风航空科技有限公司 | A kind of double folding multi-rotor aerocraft |
CN111452975A (en) * | 2020-04-13 | 2020-07-28 | 宋有洲 | Multifunctional aircraft |
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