JP5336575B2 - スラット展開機構 - Google Patents

スラット展開機構 Download PDF

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Publication number
JP5336575B2
JP5336575B2 JP2011501295A JP2011501295A JP5336575B2 JP 5336575 B2 JP5336575 B2 JP 5336575B2 JP 2011501295 A JP2011501295 A JP 2011501295A JP 2011501295 A JP2011501295 A JP 2011501295A JP 5336575 B2 JP5336575 B2 JP 5336575B2
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JP
Japan
Prior art keywords
drive member
slat
pinion
drive
track
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Expired - Fee Related
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JP2011501295A
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English (en)
Japanese (ja)
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JP2011515277A (ja
JP2011515277A5 (enExample
Inventor
マン，アラン
Original Assignee
エアバス オペレーションズ リミティド
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Application filed by エアバス オペレーションズ リミティド filed Critical エアバス オペレーションズ リミティド
Publication of JP2011515277A publication Critical patent/JP2011515277A/ja
Publication of JP2011515277A5 publication Critical patent/JP2011515277A5/ja
Application granted granted Critical
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    • 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
    • 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)
  • Blinds (AREA)
  • Auxiliary Devices For And Details Of Packaging Control (AREA)
  • Seats For Vehicles (AREA)
  • Chair Legs, Seat Parts, And Backrests (AREA)
JP2011501295A 2008-03-28 2009-03-12 スラット展開機構 Expired - Fee Related JP5336575B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0805599.8 2008-03-28
GBGB0805599.8A GB0805599D0 (en) 2008-03-28 2008-03-28 Slat deployment mechanism
PCT/GB2009/050239 WO2009118547A2 (en) 2008-03-28 2009-03-12 Slat deployment mechanism

Publications (3)

Publication Number Publication Date
JP2011515277A JP2011515277A (ja) 2011-05-19
JP2011515277A5 JP2011515277A5 (enExample) 2012-04-19
JP5336575B2 true JP5336575B2 (ja) 2013-11-06

Family

ID=39386871

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011501295A Expired - Fee Related JP5336575B2 (ja) 2008-03-28 2009-03-12 スラット展開機構

Country Status (9)

Country Link
US (1) US8511619B2 (enExample)
EP (1) EP2268540B1 (enExample)
JP (1) JP5336575B2 (enExample)
CN (1) CN102007036B (enExample)
AT (1) ATE521533T1 (enExample)
CA (1) CA2719173C (enExample)
GB (1) GB0805599D0 (enExample)
RU (1) RU2492110C2 (enExample)
WO (1) WO2009118547A2 (enExample)

Families Citing this family (30)

* 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
CN101988570B (zh) * 2009-07-31 2014-08-20 中国商用飞机有限责任公司 用于飞机缝翼作动器的齿轮齿条的设计方法
GB201005966D0 (en) * 2010-04-09 2010-05-26 Moog Wolverhampton Ltd Skew & loss detection system
GB201209686D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A slat support assembly
CN102975849A (zh) * 2012-12-14 2013-03-20 中国航空工业空气动力研究院 一种前探式前翼前缘襟翼结构
US9890814B2 (en) * 2014-06-03 2018-02-13 Roller Bearing Company Of America, Inc. Cage for hourglass roller bearings
EP3299278B1 (en) * 2016-09-23 2020-06-03 Airbus Operations GmbH A slat track device for an aircraft wing
FR3058983B1 (fr) * 2016-11-22 2018-11-02 Safran Electronics & Defense Actionneur a montage facilite
EP3378762A1 (en) 2017-03-24 2018-09-26 Airbus Operations GmbH Wing for an aircraft
EP3378760A1 (en) * 2017-03-24 2018-09-26 Airbus Operations GmbH Wing for an aircraft
EP3395678B1 (en) 2017-04-26 2021-05-26 Asco Industries NV Guidance assembly for an airfoil leading edge high-lift device carrier track
RU2746479C1 (ru) * 2017-04-28 2021-04-14 Эйрбас Оперейшнз Гмбх Консоль крыла для летательного аппарата
WO2018197265A1 (en) 2017-04-28 2018-11-01 Airbus Operations Gmbh Wing for an aircraft
EP3501977B1 (en) 2017-12-19 2021-08-11 Asco Industries NV Deployment system for an airfoil high lift leading edge device
EP3501978B1 (en) 2017-12-21 2021-03-10 Airbus Operations GmbH Wing for an aircraft
JP6929809B2 (ja) 2018-03-02 2021-09-01 三菱重工業株式会社 高揚力装置、翼及び航空機
US10889365B2 (en) * 2018-03-15 2021-01-12 The Boeing Company Auxiliary support system for a flap of an aircraft wing
GB2572216A (en) * 2018-03-23 2019-09-25 Airbus Operations Ltd Leading edge flight control surfaces
GB2579221A (en) * 2018-11-26 2020-06-17 Airbus Operations Ltd Aircraft control mechanism
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
MA53107A (fr) 2019-03-29 2021-05-19 Airbus Operations Gmbh Aile d'aéronef
US11427302B2 (en) * 2019-04-01 2022-08-30 Yaborã Indústria Aeronáutica S.A. Closure fairings for wing leading edge slat track openings
DE102019111118A1 (de) * 2019-04-30 2020-11-05 Airbus Operations Gmbh Hochauftriebsvorrichtung für ein Flugzeug
EP3858728B1 (en) * 2020-01-31 2024-05-01 Goodrich Actuation Systems Limited Panel actuation assembly
EP4112450A1 (en) * 2021-06-30 2023-01-04 Airbus Operations GmbH Wing for an aircraft
CN113460287A (zh) * 2021-09-03 2021-10-01 中国商用飞机有限责任公司 缝翼滑轨组件及其组装方法
US12606295B2 (en) * 2024-09-04 2026-04-21 The Boeing Company Aircraft wings and systems and methods for driving a slat of an aircraft wing
DE102024132504A1 (de) * 2024-11-07 2026-05-07 Airbus Operations Gmbh Flügel für ein Luftfahrzeug
BE1033281A1 (fr) * 2025-01-06 2026-07-31 Sonaca Sa Système de guidage et d'entraînement amélioré d'un volet mobile de bord d'attaque pour une aile d'aéronef
US12441455B1 (en) 2025-01-27 2025-10-14 The Boeing Company Wing assemblies and aircraft with gap-adjustment assemblies for slats

Family Cites Families (20)

* 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
US2938680A (en) * 1957-07-02 1960-05-31 North American Aviation Inc Multiple position airfoil slat
US2990140A (en) * 1958-10-24 1961-06-27 Lockheed Aircraft Corp Combination gust alleviator and highlift device for aircraft
US3272458A (en) * 1964-12-08 1966-09-13 Gen Dynamics Corp Means for positioning a rotating wing slat device
US3847369A (en) * 1973-03-08 1974-11-12 Us Navy Control surface deployment mechanism
DE3013774A1 (de) 1980-04-10 1981-10-15 Vereinigte Flugtechnische Werke Gmbh, 2800 Bremen Betaetigungsanordnung fuer fluegelklappen
US4753402A (en) * 1985-12-30 1988-06-28 The Boeing Company Biased leading edge slat apparatus
US4650140A (en) * 1985-12-30 1987-03-17 The Boeing Company Wind edge movable airfoil having variable camber
GB2204538B (en) * 1987-05-06 1990-12-12 British Aerospace Wing leading edge arrangements for aircraft
GB8711252D0 (en) * 1987-05-13 1987-07-15 British Aerospace High lift device
DE4107556C1 (enExample) * 1991-03-08 1992-05-14 Deutsche Airbus Gmbh, 2000 Hamburg, De
US5158252A (en) * 1991-10-24 1992-10-27 The Boeing Company Three-position variable camber Krueger leading edge flap
GB2304656B (en) * 1995-08-26 1999-10-13 British Aerospace Deployment mechanisms for aircraft auxiliary aerofoils
DE10133920B4 (de) * 2001-07-12 2004-05-13 Eads Deutschland Gmbh Auftriebsklappen-Mechanismus
CN100408428C (zh) * 2002-10-09 2008-08-06 波音公司 开缝的飞行器机翼
DE10328540B4 (de) * 2003-06-24 2008-02-14 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe
US20070102587A1 (en) * 2005-11-07 2007-05-10 The Boeing Company Wing leading edge slat system
EP2134597B1 (en) * 2007-03-09 2011-06-22 Asco Industries Wing
GB0805599D0 (en) * 2008-03-28 2008-04-30 Airbus Uk Ltd Slat deployment mechanism
GB2458683A (en) * 2008-03-28 2009-09-30 Airbus Uk Ltd Aircraft slat deployment mechanism

Also Published As

Publication number Publication date
JP2011515277A (ja) 2011-05-19
EP2268540B1 (en) 2011-08-24
GB0805599D0 (en) 2008-04-30
US8511619B2 (en) 2013-08-20
CN102007036A (zh) 2011-04-06
WO2009118547A2 (en) 2009-10-01
ATE521533T1 (de) 2011-09-15
CA2719173A1 (en) 2009-10-01
US20110036944A1 (en) 2011-02-17
RU2492110C2 (ru) 2013-09-10
WO2009118547A3 (en) 2009-11-26
CN102007036B (zh) 2013-11-20
RU2010142990A (ru) 2012-05-10
CA2719173C (en) 2014-06-17
EP2268540A2 (en) 2011-01-05

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