GB2003098A - Aircraft wings - Google Patents
Aircraft wingsInfo
- Publication number
- GB2003098A GB2003098A GB7829158A GB7829158A GB2003098A GB 2003098 A GB2003098 A GB 2003098A GB 7829158 A GB7829158 A GB 7829158A GB 7829158 A GB7829158 A GB 7829158A GB 2003098 A GB2003098 A GB 2003098A
- Authority
- GB
- United Kingdom
- Prior art keywords
- lift increasing
- region
- main portion
- increasing portion
- lift
- 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.)
- Granted
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C9/00—Adjustable control surfaces or members, e.g. rudders
- B64C9/14—Adjustable control surfaces or members, e.g. rudders forming slots
- B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Tires In General (AREA)
Abstract
An aircraft wing has a main portion to the rear of which is carried a lift increasing portion, and connecting means, including a rotary actuator 17 which accepts high speed/low torque rotation from a spanwise extending shaft 18 and converts this to a low speed/high torque output, connecting the lift increasing portion to the main portion for movement from a first position in which the leading region 2 of the lift increasing portion lies close to the trailing region 1 of the main portion to a second position in which a slot is formed between the trailing region and the leading region for lift increasing purposes, the connecting means providing pivotal movement of the lift increasing portion for aircraft control purposes in both the first and second positions. <IMAGE>
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB7829158A GB2003098B (en) | 1977-07-07 | 1978-07-07 | Aircraft wings |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2843377 | 1977-07-07 | ||
GB7829158A GB2003098B (en) | 1977-07-07 | 1978-07-07 | Aircraft wings |
Publications (2)
Publication Number | Publication Date |
---|---|
GB2003098A true GB2003098A (en) | 1979-03-07 |
GB2003098B GB2003098B (en) | 1982-01-27 |
Family
ID=26259373
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB7829158A Expired GB2003098B (en) | 1977-07-07 | 1978-07-07 | Aircraft wings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB2003098B (en) |
Cited By (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2467775A1 (en) * | 1979-10-19 | 1981-04-30 | British Aerospace | VARIABLE CAMBER WING |
FR2473982A1 (en) * | 1980-01-22 | 1981-07-24 | British Aerospace | WING AND SHUTTER ARRANGEMENT FOR AIRCRAFT |
FR2503661A1 (en) * | 1981-04-08 | 1982-10-15 | Ver Flugtechnische Werke | METHOD FOR OPTIMIZING THE CRUISE FLIGHT CONDITION OF TRANSSONIC WING AIRCRAFT AND DEVICE FOR IMPLEMENTING SAID METHOD |
EP0075966A2 (en) * | 1981-09-29 | 1983-04-06 | The Boeing Company | Aileron system for aircraft and method of operating the same |
US4471927A (en) * | 1981-09-29 | 1984-09-18 | The Boeing Company | Trailing edge flap assembly |
EP0154047A1 (en) * | 1984-03-09 | 1985-09-11 | The Boeing Company | Wing flap mechanism |
US4544118A (en) * | 1982-09-30 | 1985-10-01 | The Boeing Company | Drive mechanism for combined flap-aileron surface |
WO2008071399A1 (en) * | 2006-12-11 | 2008-06-19 | Airbus Deutschland Gmbh | Wing of an aircraft |
WO2010052022A2 (en) * | 2008-11-10 | 2010-05-14 | Airbus Operations Gmbh | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device |
EP2669190A1 (en) * | 2012-05-29 | 2013-12-04 | The Boeing Company | Rotary actuated high lift gapped aileron |
CN105620723A (en) * | 2014-10-31 | 2016-06-01 | 中国航空工业集团公司西安飞机设计研究所 | Flaperon |
US9580168B2 (en) * | 2014-12-19 | 2017-02-28 | The Boeing Company | Cove lip door slaved to trailing edge control device |
EP3398849A1 (en) * | 2017-05-02 | 2018-11-07 | Airbus Operations GmbH | Aerodynamic sealing and wing for an aircraft comprising such sealing |
CN115384757A (en) * | 2022-10-31 | 2022-11-25 | 北京启时智航科技有限公司 | Flaperon actuating mechanism and wing structure |
-
1978
- 1978-07-07 GB GB7829158A patent/GB2003098B/en not_active Expired
Cited By (31)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2467775A1 (en) * | 1979-10-19 | 1981-04-30 | British Aerospace | VARIABLE CAMBER WING |
US4395008A (en) * | 1980-01-22 | 1983-07-26 | British Aerospace Public Limited Company | Aircraft wing and flap arrangement |
FR2473982A1 (en) * | 1980-01-22 | 1981-07-24 | British Aerospace | WING AND SHUTTER ARRANGEMENT FOR AIRCRAFT |
DE3101847A1 (en) * | 1980-01-22 | 1981-12-24 | British Aerospace Public Ltd. Co., Weybridge, Surrey | AIRCRAFT WING WITH FLAP ARRANGEMENT |
FR2503661A1 (en) * | 1981-04-08 | 1982-10-15 | Ver Flugtechnische Werke | METHOD FOR OPTIMIZING THE CRUISE FLIGHT CONDITION OF TRANSSONIC WING AIRCRAFT AND DEVICE FOR IMPLEMENTING SAID METHOD |
NL8105237A (en) * | 1981-04-08 | 1982-11-01 | Ver Flugtechnische Werke | METHOD FOR OPTIMIZING THE CROSS-FLIGHT CONDITION OF AIRCRAFT WITH TRANSSONIC WINGS, AND AN APPARATUS FOR USING THE METHOD |
EP0075966A2 (en) * | 1981-09-29 | 1983-04-06 | The Boeing Company | Aileron system for aircraft and method of operating the same |
US4471927A (en) * | 1981-09-29 | 1984-09-18 | The Boeing Company | Trailing edge flap assembly |
EP0075966A3 (en) * | 1981-09-29 | 1985-11-13 | The Boeing Company | Aileron system for aircraft and method of operating the same |
US4705236A (en) * | 1981-09-29 | 1987-11-10 | The Boeing Company | Aileron system for aircraft and method of operating the same |
US4544118A (en) * | 1982-09-30 | 1985-10-01 | The Boeing Company | Drive mechanism for combined flap-aileron surface |
EP0154047A1 (en) * | 1984-03-09 | 1985-09-11 | The Boeing Company | Wing flap mechanism |
WO2008071399A1 (en) * | 2006-12-11 | 2008-06-19 | Airbus Deutschland Gmbh | Wing of an aircraft |
US8191835B2 (en) | 2006-12-11 | 2012-06-05 | Airbus Deutschland Gmbh | Wing of an aircraft |
WO2010052022A3 (en) * | 2008-11-10 | 2010-07-29 | Airbus Operations Gmbh | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device |
WO2010052022A2 (en) * | 2008-11-10 | 2010-05-14 | Airbus Operations Gmbh | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device |
US8584991B2 (en) | 2008-11-10 | 2013-11-19 | Airbus Operations Gmbh | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device |
CN102209662B (en) * | 2008-11-10 | 2015-11-25 | 空中客车营运有限公司 | There is the wing of Krueger flap and gap covering device and the regulating mechanism for gap covering device |
CN102209662A (en) * | 2008-11-10 | 2011-10-05 | 空中客车营运有限公司 | Vane having a regulating flap and a gap covering device and an adjusting mechanism for a gap covering device |
RU2625384C2 (en) * | 2012-05-29 | 2017-07-13 | Зе Боинг Компани | Rotation-driven aileron, set with a gap and creating high lift |
EP2669190A1 (en) * | 2012-05-29 | 2013-12-04 | The Boeing Company | Rotary actuated high lift gapped aileron |
EP2669189A1 (en) * | 2012-05-29 | 2013-12-04 | The Boeing Company | Rotary actuated high lift gapped aileron |
US9108715B2 (en) | 2012-05-29 | 2015-08-18 | The Boeing Company | Rotary actuated high lift gapped aileron |
EP2669189B1 (en) | 2012-05-29 | 2017-04-12 | The Boeing Company | Rotary actuated high lift gapped aileron |
EP2669190B1 (en) | 2012-05-29 | 2017-05-10 | The Boeing Company | Rotary actuated high lift gapped aileron |
CN105620723A (en) * | 2014-10-31 | 2016-06-01 | 中国航空工业集团公司西安飞机设计研究所 | Flaperon |
US9580168B2 (en) * | 2014-12-19 | 2017-02-28 | The Boeing Company | Cove lip door slaved to trailing edge control device |
EP3398849A1 (en) * | 2017-05-02 | 2018-11-07 | Airbus Operations GmbH | Aerodynamic sealing and wing for an aircraft comprising such sealing |
US11046419B2 (en) | 2017-05-02 | 2021-06-29 | Airbus Operations Gmbh | Aerodynamic sealing and wing for an aircraft comprising such sealing |
CN115384757A (en) * | 2022-10-31 | 2022-11-25 | 北京启时智航科技有限公司 | Flaperon actuating mechanism and wing structure |
CN115384757B (en) * | 2022-10-31 | 2023-01-24 | 北京启时智航科技有限公司 | Flaperon actuating mechanism and wing structure |
Also Published As
Publication number | Publication date |
---|---|
GB2003098B (en) | 1982-01-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB2003098A (en) | Aircraft wings | |
EP0538963B1 (en) | Three-position variable camber krueger leading edge flap | |
EP0239138A3 (en) | Aircraft wings with aileron-supported ground speed spoilers and trailing edge flaps | |
EP0838394A3 (en) | Slotted cruise trailing edge flap | |
GB1480821A (en) | Variable camber leading edge flaps | |
IL86840A (en) | Flutter exciter for testing of aircraft wings | |
US4365774A (en) | Convertible delta wing aircraft | |
US2334975A (en) | Aircraft | |
FR2309401A1 (en) | Rotary wing producing lift and thrust - has horizontal blades with pitch control, rotating about horizontal shaft | |
FR2452426A1 (en) | Lifting body aircraft for vertical or STOL service - has movable flap on trailing edge and tiltable propeller | |
GB2006133A (en) | Variable-camber aircraft wings | |
GB432124A (en) | Improvements in aircraft of the helicopter type | |
JPH0338080Y2 (en) | ||
GB2017020A (en) | Aircraft control surfaces | |
GB1484865A (en) | Drive arrangements for aircraft control surfaces | |
JPH035199Y2 (en) | ||
JPH0378319B2 (en) | ||
RU8678U1 (en) | HELICOPTER SCREW | |
GB559546A (en) | Improvements in aircraft flap actuating gear | |
EP0937642A3 (en) | Flight controls with automatic balance | |
GB656833A (en) | Improvements in or relating to direct lift aircraft | |
WO1989007073A3 (en) | Aircraft | |
GB8821220D0 (en) | Fuselage mounted flap drive for wing trailing edge flaps | |
CA1030130A (en) | Trailing edge flaps having spanwise aerodynamic slot opening and closing mechanism | |
Holla et al. | Evaluation of lift and drag of a family of conically cambered wings at off design Mach numbers(Lift and drag at off-design Mach numbers of conically cambered wings with subsonic leading edges and supersonic trailing edge) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
732 | Registration of transactions, instruments or events in the register (sect. 32/1977) | ||
PCNP | Patent ceased through non-payment of renewal fee |