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GB2260521B - An aircraft wing leading edge arrangement - Google Patents

An aircraft wing leading edge arrangement

Info

Publication number
GB2260521B
GB2260521B GB9122225A GB9122225A GB2260521B GB 2260521 B GB2260521 B GB 2260521B GB 9122225 A GB9122225 A GB 9122225A GB 9122225 A GB9122225 A GB 9122225A GB 2260521 B GB2260521 B GB 2260521B
Authority
GB
United Kingdom
Prior art keywords
leading edge
aircraft wing
wing leading
edge arrangement
arrangement
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 - Fee Related
Application number
GB9122225A
Other versions
GB2260521A (en
GB9122225D0 (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
Priority to GB9122225A priority Critical patent/GB2260521B/en
Publication of GB9122225D0 publication Critical patent/GB9122225D0/en
Publication of GB2260521A publication Critical patent/GB2260521A/en
Application granted granted Critical
Publication of GB2260521B publication Critical patent/GB2260521B/en
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64C9/22—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Catching Or Destruction (AREA)
GB9122225A 1991-10-19 1991-10-19 An aircraft wing leading edge arrangement Expired - Fee Related GB2260521B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9122225A GB2260521B (en) 1991-10-19 1991-10-19 An aircraft wing leading edge arrangement

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9122225A GB2260521B (en) 1991-10-19 1991-10-19 An aircraft wing leading edge arrangement

Publications (3)

Publication Number Publication Date
GB9122225D0 GB9122225D0 (en) 1991-12-04
GB2260521A GB2260521A (en) 1993-04-21
GB2260521B true GB2260521B (en) 1995-03-22

Family

ID=10703218

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9122225A Expired - Fee Related GB2260521B (en) 1991-10-19 1991-10-19 An aircraft wing leading edge arrangement

Country Status (1)

Country Link
GB (1) GB2260521B (en)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB9607707D0 (en) * 1996-04-13 1996-06-19 Broadbent Michael C A self-sealing parallelogram slat mechanism
WO1997038900A1 (en) * 1996-04-13 1997-10-23 Michael Craig Broadbent Variable camber wing mechanism
GB0114634D0 (en) * 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
DE102008056655A1 (en) * 2008-11-10 2010-05-27 Airbus Deutschland Gmbh Wing with a flap and a gap cover device and adjustment mechanism for a gap cover device
GB201018176D0 (en) 2010-10-28 2010-12-08 Airbus Operations Ltd Krueger
GB201209686D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A slat support assembly
FR3011226B1 (en) 2013-09-30 2017-05-19 Airbus Operations Sas HYPERSUSTENTER LEAK DEPENDENT SHUTTER SYSTEM FOR AN AIRCRAFT SAIL.
US10494083B2 (en) * 2016-11-21 2019-12-03 The Boeing Company Aircraft flap hinge
EP3575206A1 (en) * 2018-06-01 2019-12-04 Airbus Operations GmbH System for driving a flap arrangement between a retracted position and an extended position
EP3575207A1 (en) * 2018-06-01 2019-12-04 Airbus Operations GmbH System for driving a flap arrangement between a retracted position and an extended position
CN108791815A (en) * 2018-06-25 2018-11-13 李竟儒 It is a kind of to prevent the Aircraft Air device out of control for hitting stretch of flatland in a hilly area sea

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4042191A (en) * 1976-05-03 1977-08-16 The Boeing Company Slot seal for leading edge flap
EP0068737A1 (en) * 1981-06-18 1983-01-05 Lockheed Corporation Leading edge flap for an airfoil

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4042191A (en) * 1976-05-03 1977-08-16 The Boeing Company Slot seal for leading edge flap
EP0068737A1 (en) * 1981-06-18 1983-01-05 Lockheed Corporation Leading edge flap for an airfoil

Also Published As

Publication number Publication date
GB2260521A (en) 1993-04-21
GB9122225D0 (en) 1991-12-04

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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: 20051019