CN102007036B - 缝翼展开机构 - Google Patents

缝翼展开机构 Download PDF

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Publication number
CN102007036B
CN102007036B CN2009801108148A CN200980110814A CN102007036B CN 102007036 B CN102007036 B CN 102007036B CN 2009801108148 A CN2009801108148 A CN 2009801108148A CN 200980110814 A CN200980110814 A CN 200980110814A CN 102007036 B CN102007036 B CN 102007036B
Authority
CN
China
Prior art keywords
drive member
slat
bearing
miniature gears
drive
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
CN2009801108148A
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English (en)
Chinese (zh)
Other versions
CN102007036A (zh
Inventor
阿兰·曼
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
Publication of CN102007036A publication Critical patent/CN102007036A/zh
Application granted granted Critical
Publication of CN102007036B publication Critical patent/CN102007036B/zh
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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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
    • 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)
  • Seats For Vehicles (AREA)
  • Chair Legs, Seat Parts, And Backrests (AREA)
  • Auxiliary Devices For And Details Of Packaging Control (AREA)
CN2009801108148A 2008-03-28 2009-03-12 缝翼展开机构 Expired - Fee Related CN102007036B (zh)

Applications Claiming Priority (3)

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

Publications (2)

Publication Number Publication Date
CN102007036A CN102007036A (zh) 2011-04-06
CN102007036B true CN102007036B (zh) 2013-11-20

Family

ID=39386871

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2009801108148A Expired - Fee Related CN102007036B (zh) 2008-03-28 2009-03-12 缝翼展开机构

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 (27)

* 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
EP3378760A1 (en) * 2017-03-24 2018-09-26 Airbus Operations GmbH Wing for an aircraft
EP3378762A1 (en) 2017-03-24 2018-09-26 Airbus Operations GmbH Wing for an aircraft
ES2878314T3 (es) 2017-04-26 2021-11-18 Asco Ind Nv Conjunto de guía para una pista portadora del dispositivo hipersustentador del borde delantero aerodinámico
EP3615421B1 (en) 2017-04-28 2023-01-11 Airbus Operations GmbH Wing for an aircraft
JP6915088B2 (ja) * 2017-04-28 2021-08-04 エアバス オペレーションズ ゲーエムベーハーＡｉｒｂｕｓ Ｏｐｅｒａｔｉｏｎｓ ＧｍｂＨ 航空機用の翼
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
EP3718881B1 (en) 2019-03-29 2022-10-12 Airbus Operations GmbH Wing for an aircraft
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
US12441455B1 (en) 2025-01-27 2025-10-14 The Boeing Company Wing assemblies and aircraft with gap-adjustment assemblies for slats

Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938680A (en) * 1957-07-02 1960-05-31 North American Aviation Inc Multiple position airfoil slat
CN1720167A (zh) * 2002-10-09 2006-01-11 波音公司 开缝的飞行器机翼
US20070102587A1 (en) * 2005-11-07 2007-05-10 The Boeing Company Wing leading edge slat system

Family Cites Families (17)

* 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
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
DE10328540B4 (de) * 2003-06-24 2008-02-14 Eads Deutschland Gmbh Betätigungseinrichtung für eine an der Hinterkante des Tragflügels eines Flugzeugs angeordnete Ruderklappe
WO2008110521A1 (en) * 2007-03-09 2008-09-18 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

Patent Citations (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2938680A (en) * 1957-07-02 1960-05-31 North American Aviation Inc Multiple position airfoil slat
CN1720167A (zh) * 2002-10-09 2006-01-11 波音公司 开缝的飞行器机翼
US20070102587A1 (en) * 2005-11-07 2007-05-10 The Boeing Company Wing leading edge slat system

Also Published As

Publication number Publication date
CN102007036A (zh) 2011-04-06
CA2719173A1 (en) 2009-10-01
US20110036944A1 (en) 2011-02-17
ATE521533T1 (de) 2011-09-15
RU2492110C2 (ru) 2013-09-10
EP2268540A2 (en) 2011-01-05
JP5336575B2 (ja) 2013-11-06
CA2719173C (en) 2014-06-17
US8511619B2 (en) 2013-08-20
WO2009118547A2 (en) 2009-10-01
WO2009118547A3 (en) 2009-11-26
EP2268540B1 (en) 2011-08-24
RU2010142990A (ru) 2012-05-10
GB0805599D0 (en) 2008-04-30
JP2011515277A (ja) 2011-05-19

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C06 Publication
PB01 Publication
C10 Entry into substantive examination
SE01 Entry into force of request for substantive examination
C14 Grant of patent or utility model
GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20131120

Termination date: 20210312