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GB2003098A - Aircraft wings - Google Patents

Aircraft wings

Info

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
Application number
GB7829158A
Other versions
GB2003098B (en
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.)
British Aircraft Corp Ltd
Original Assignee
British Aircraft Corp Ltd
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 British Aircraft Corp Ltd filed Critical British Aircraft Corp Ltd
Priority to GB7829158A priority Critical patent/GB2003098B/en
Publication of GB2003098A publication Critical patent/GB2003098A/en
Application granted granted Critical
Publication of GB2003098B publication Critical patent/GB2003098B/en
Expired legal-status Critical Current

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>
GB7829158A 1977-07-07 1978-07-07 Aircraft wings Expired GB2003098B (en)

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)

* Cited by examiner, † Cited by third party
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
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
EP0075966A3 (en) * 1981-09-29 1985-11-13 The Boeing Company Aileron system for aircraft and method of operating the same
WO2008071399A1 (en) * 2006-12-11 2008-06-19 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
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

Cited By (29)

* Cited by examiner, † Cited by third party
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
DE3101847A1 (en) * 1980-01-22 1981-12-24 British Aerospace Public Ltd. Co., Weybridge, Surrey AIRCRAFT WING WITH FLAP ARRANGEMENT
US4395008A (en) * 1980-01-22 1983-07-26 British Aerospace Public Limited Company Aircraft wing and 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
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
US8191835B2 (en) 2006-12-11 2012-06-05 Airbus Deutschland Gmbh Wing of an aircraft
WO2008071399A1 (en) * 2006-12-11 2008-06-19 Airbus Deutschland Gmbh Wing of an aircraft
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
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
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
RU2625384C2 (en) * 2012-05-29 2017-07-13 Зе Боинг Компани Rotation-driven aileron, set with a gap and creating high lift
US9108715B2 (en) 2012-05-29 2015-08-18 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
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
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
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

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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