GB2186849B - Variable camber leading edge arrangements for aircraft wings - Google Patents

Variable camber leading edge arrangements for aircraft wings

Info

Publication number
GB2186849B
GB2186849B GB8703502A GB8703502A GB2186849B GB 2186849 B GB2186849 B GB 2186849B GB 8703502 A GB8703502 A GB 8703502A GB 8703502 A GB8703502 A GB 8703502A GB 2186849 B GB2186849 B GB 2186849B
Authority
GB
United Kingdom
Prior art keywords
leading edge
aircraft wings
variable camber
edge arrangements
camber leading
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
Application number
GB8703502A
Other versions
GB8703502D0 (en
GB2186849A (en
Inventor
John Brooke Clifford-Jones
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 Aerospace PLC filed Critical British Aerospace PLC
Publication of GB8703502D0 publication Critical patent/GB8703502D0/en
Publication of GB2186849A publication Critical patent/GB2186849A/en
Application granted granted Critical
Publication of GB2186849B publication Critical patent/GB2186849B/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/38—Adjustment of complete wings or parts thereof
    • B64C3/44—Varying camber
    • B64C3/48—Varying camber by relatively-movable parts of wing structures
    • 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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
GB8703502A 1986-02-19 1987-02-16 Variable camber leading edge arrangements for aircraft wings Expired GB2186849B (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB8603669 1986-02-19

Publications (3)

Publication Number Publication Date
GB8703502D0 GB8703502D0 (en) 1987-03-25
GB2186849A GB2186849A (en) 1987-08-26
GB2186849B true GB2186849B (en) 1989-11-08

Family

ID=10593066

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8703502A Expired GB2186849B (en) 1986-02-19 1987-02-16 Variable camber leading edge arrangements for aircraft wings

Country Status (1)

Country Link
GB (1) GB2186849B (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB8702782D0 (en) * 1987-02-07 1987-07-29 British Aerospace Aerodynamic control devices
GB9607707D0 (en) * 1996-04-13 1996-06-19 Broadbent Michael C A self-sealing parallelogram slat mechanism
JPH11509804A (en) * 1996-04-13 1999-08-31 マイケル クレイグ ブロードベント Variable camber wing mechanism
GB0114634D0 (en) 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
DE102005027749B4 (en) * 2005-06-16 2011-07-28 Airbus Operations GmbH, 21129 Buoyancy-enhancing flap, in particular nose flap, for an aerodynamically effective wing
US7753313B1 (en) * 2006-09-19 2010-07-13 The Boeing Company Composite wing slat for aircraft
GB0708641D0 (en) * 2007-05-04 2007-06-13 Goodrich Actuation Systems Ltd Actuator
DE102009026457A1 (en) 2009-05-25 2010-12-09 Eads Deutschland Gmbh Aerodynamic component with deformable outer skin
GB201006099D0 (en) 2010-04-13 2010-05-26 Airbus Operations Ltd Slat support assembly
US9296475B2 (en) 2013-09-24 2016-03-29 The Boeing Company System and method for reducing the stopping distance of an aircraft
US9327827B2 (en) 2013-09-24 2016-05-03 The Boeing Company Leading and trailing edge device deflections during descent of an aircraft
US9771141B2 (en) 2013-09-24 2017-09-26 The Boeing Company Leading edge system and method for approach noise reduction
US9359065B2 (en) 2013-09-24 2016-06-07 The Boeing Company System and method for optimizing performance of an aircraft
US9656741B2 (en) 2013-09-24 2017-05-23 The Boeing Company Control interface for leading and trailing edge devices
US9180962B2 (en) * 2013-09-24 2015-11-10 The Boeing Company Leading edge variable camber system and method
US9193440B2 (en) 2013-09-24 2015-11-24 The Boeing Company Variable camber flap system and method
US9821903B2 (en) 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
WO2021104940A1 (en) * 2019-11-25 2021-06-03 Airbus Operations Gmbh A wing for an aircraft

Also Published As

Publication number Publication date
GB8703502D0 (en) 1987-03-25
GB2186849A (en) 1987-08-26

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Legal Events

Date Code Title Description
732E Amendments to the register in respect of changes of name or changes affecting rights (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20050216