GB0805595D0 - Slat deployment mechanism - Google Patents

Slat deployment mechanism

Info

Publication number
GB0805595D0
GB0805595D0 GBGB0805595.6A GB0805595A GB0805595D0 GB 0805595 D0 GB0805595 D0 GB 0805595D0 GB 0805595 A GB0805595 A GB 0805595A GB 0805595 D0 GB0805595 D0 GB 0805595D0
Authority
GB
United Kingdom
Prior art keywords
deployment mechanism
slat deployment
slat
deployment
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.)
Withdrawn
Application number
GBGB0805595.6A
Other versions
GB2458683A (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.)
Airbus Operations Ltd
Original Assignee
Airbus Operations 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 Airbus Operations Ltd filed Critical Airbus Operations Ltd
Priority to GB0805595A priority Critical patent/GB2458683A/en
Publication of GB0805595D0 publication Critical patent/GB0805595D0/en
Publication of GB2458683A publication Critical patent/GB2458683A/en
Withdrawn legal-status Critical Current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
    • 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
    • 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
    • B64C2009/143—Adjustable control surfaces or members, e.g. rudders forming slots comprising independently adjustable elements for closing or opening the slot between the main wing and leading or trailing edge flaps

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Transmission Devices (AREA)
GB0805595A 2008-03-28 2008-03-28 Aircraft slat deployment mechanism Withdrawn GB2458683A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB0805595A GB2458683A (en) 2008-03-28 2008-03-28 Aircraft slat deployment mechanism

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB0805595A GB2458683A (en) 2008-03-28 2008-03-28 Aircraft slat deployment mechanism

Publications (2)

Publication Number Publication Date
GB0805595D0 true GB0805595D0 (en) 2008-04-30
GB2458683A GB2458683A (en) 2009-09-30

Family

ID=39386867

Family Applications (1)

Application Number Title Priority Date Filing Date
GB0805595A Withdrawn GB2458683A (en) 2008-03-28 2008-03-28 Aircraft slat deployment mechanism

Country Status (1)

Country Link
GB (1) GB2458683A (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0805599D0 (en) * 2008-03-28 2008-04-30 Airbus Uk Ltd Slat deployment mechanism
EP3395678B1 (en) 2017-04-26 2021-05-26 Asco Industries NV Guidance assembly for an airfoil leading edge high-lift device carrier track
EP3501977B1 (en) 2017-12-19 2021-08-11 Asco Industries NV Deployment system for an airfoil high lift leading edge device
GB2572216A (en) * 2018-03-23 2019-09-25 Airbus Operations Ltd Leading edge flight control surfaces
WO2020174084A1 (en) * 2019-02-28 2020-09-03 Airbus Operations Gmbh A wing leading-edge device and a wing having such a wing leading-edge device
US11383821B2 (en) 2019-03-22 2022-07-12 Airbus Operations Gmbh Wing leading-edge device and a wing having such a wing leading-edge device
MA53107A (en) 2019-03-29 2021-05-19 Airbus Operations Gmbh AIRCRAFT WING

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB517422A (en) * 1938-07-19 1940-01-30 Westland Aircraft Ltd Improvements in or relating to aircraft
GB539117A (en) * 1940-02-28 1941-08-28 Rene Jean Camille Tampier Improvements in or relating to aircraft controls
DE10328540B4 (en) * 2003-06-24 2008-02-14 Eads Deutschland Gmbh Actuating device for a rudder flap arranged on the trailing edge of the wing of an aircraft

Also Published As

Publication number Publication date
GB2458683A (en) 2009-09-30

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)