DE69003440D1 - Biegsame Abschlussvorrichtung für eine Flügelvorderkante. - Google Patents

Biegsame Abschlussvorrichtung für eine Flügelvorderkante.

Info

Publication number
DE69003440D1
DE69003440D1 DE90304928T DE69003440T DE69003440D1 DE 69003440 D1 DE69003440 D1 DE 69003440D1 DE 90304928 T DE90304928 T DE 90304928T DE 69003440 T DE69003440 T DE 69003440T DE 69003440 D1 DE69003440 D1 DE 69003440D1
Authority
DE
Germany
Prior art keywords
wing
leading edge
closing device
flexible closing
flexible
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
DE90304928T
Other languages
English (en)
Other versions
DE69003440T2 (de
Inventor
Anthony John Williams
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.)
Airbus Operations Ltd
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
Application granted granted Critical
Publication of DE69003440D1 publication Critical patent/DE69003440D1/de
Publication of DE69003440T2 publication Critical patent/DE69003440T2/de
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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
  • Operating, Guiding And Securing Of Roll- Type Closing Members (AREA)
DE90304928T 1989-05-09 1990-05-08 Biegsame Abschlussvorrichtung für eine Flügelvorderkante. Expired - Fee Related DE69003440T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB898910654A GB8910654D0 (en) 1989-05-09 1989-05-09 Flexible closing device for a wing leading edge

Publications (2)

Publication Number Publication Date
DE69003440D1 true DE69003440D1 (de) 1993-10-28
DE69003440T2 DE69003440T2 (de) 1994-01-20

Family

ID=10656461

Family Applications (1)

Application Number Title Priority Date Filing Date
DE90304928T Expired - Fee Related DE69003440T2 (de) 1989-05-09 1990-05-08 Biegsame Abschlussvorrichtung für eine Flügelvorderkante.

Country Status (4)

Country Link
US (1) US5044580A (de)
EP (1) EP0397438B1 (de)
DE (1) DE69003440T2 (de)
GB (1) GB8910654D0 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2718707B1 (fr) * 1994-04-18 1996-07-12 Aerospatiale Dispositif de protection d'une charnière de gouverne, notamment pour aéronef.
US6015117A (en) * 1996-04-13 2000-01-18 Broadbent; Michael C Variable camber wing mechanism
GB9607707D0 (en) * 1996-04-13 1996-06-19 Broadbent Michael C A self-sealing parallelogram slat mechanism
GB9816936D0 (en) 1998-08-05 1998-09-30 British Aerospace An aerofoil having a slat
US6170781B1 (en) 1999-01-21 2001-01-09 Northrop Grumman Corporation Door edge gap and radar signature mitigation door seal
GB0114634D0 (en) 2001-06-15 2001-08-08 Broadbent Michael C Contiguous variable camber device
US7249735B2 (en) * 2005-06-30 2007-07-31 The Boeing Company Translating conduit apparatus for an airplane or equipment
GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
GB201121435D0 (en) 2011-12-14 2012-01-25 Airbus Operations Ltd Aircraft wing assembly
CA3027311A1 (en) * 2016-06-17 2017-12-21 Bombardier Inc. Panels for obstructing air flow through apertures in an aircraft wing
US11235854B2 (en) * 2019-04-01 2022-02-01 Yaborä Indústria Aeronáutica S.A. Shutter door mechanism for wing leading edge slat cut-outs

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2400322A (en) * 1944-05-12 1946-05-14 Cons Vultee Aircraft Corp Flare pistol installation
US4640477A (en) * 1984-12-31 1987-02-03 The Boeing Company Closing device for an airfoil
GB2204538B (en) * 1987-05-06 1990-12-12 British Aerospace Wing leading edge arrangements for aircraft
GB8729655D0 (en) * 1987-12-19 1988-02-03 British Aerospace Wing leading edge arrangements for aircraft
US4838502A (en) * 1988-03-16 1989-06-13 The Boeing Company Resiliently deployable fairing for sealing an airframe cavity
US4951727A (en) * 1989-03-29 1990-08-28 The United States Of America As Represented By The Secretary Of The Navy Low storage-volume closure device for curved surface

Also Published As

Publication number Publication date
DE69003440T2 (de) 1994-01-20
GB8910654D0 (en) 1989-06-21
EP0397438A2 (de) 1990-11-14
EP0397438A3 (de) 1991-03-20
EP0397438B1 (de) 1993-09-22
US5044580A (en) 1991-09-03

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: BAE SYSTEMS PLC, FARNBOROUGH, HAMPSHIRE, GB

8327 Change in the person/name/address of the patent owner

Owner name: AIRBUS UK LTD., FILTON, BRISTOL, GB

8339 Ceased/non-payment of the annual fee