CA2719173C - Slat deployment mechanism - Google Patents

Slat deployment mechanism Download PDF

Info

Publication number
CA2719173C
CA2719173C CA2719173A CA2719173A CA2719173C CA 2719173 C CA2719173 C CA 2719173C CA 2719173 A CA2719173 A CA 2719173A CA 2719173 A CA2719173 A CA 2719173A CA 2719173 C CA2719173 C CA 2719173C
Authority
CA
Canada
Prior art keywords
drive member
slat
pinion
drive
rack
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
CA2719173A
Other languages
English (en)
French (fr)
Other versions
CA2719173A1 (en
Inventor
Alan Mann
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 CA2719173A1 publication Critical patent/CA2719173A1/en
Application granted granted Critical
Publication of CA2719173C publication Critical patent/CA2719173C/en
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • 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)
CA2719173A 2008-03-28 2009-03-12 Slat deployment mechanism Expired - Fee Related CA2719173C (en)

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
CA2719173A1 CA2719173A1 (en) 2009-10-01
CA2719173C true CA2719173C (en) 2014-06-17

Family

ID=39386871

Family Applications (1)

Application Number Title Priority Date Filing Date
CA2719173A Expired - Fee Related CA2719173C (en) 2008-03-28 2009-03-12 Slat deployment mechanism

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

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
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

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
US8511619B2 (en) 2013-08-20
WO2009118547A2 (en) 2009-10-01
CN102007036B (zh) 2013-11-20
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

Similar Documents

Publication Publication Date Title
CA2719173C (en) Slat deployment mechanism
GB2458683A (en) Aircraft slat deployment mechanism
US4475702A (en) Variable camber leading edge assembly for an airfoil
EP2309150B1 (en) Actuator arrangement
EP2134597B1 (en) Wing
CN107031819B (zh) 用于飞行器的可折叠机翼和具有可折叠机翼的飞行器
US9963220B2 (en) Flap deploying device and aircraft
US4702442A (en) Aircraft trailing edge flap apparatus
EP2433863B1 (en) Slat support assembly
CN103448905B (zh) 用于可旋转地将控制表面安装在飞行器上的铰接组件
EP1316501B1 (en) Aerodynamic control surface system
US7063292B2 (en) Actuation apparatus for a control flap arranged on a trailing edge of an aircraft airfoil
EP1985893A2 (en) Actuator arrangement
CN101909991A (zh) 用于飞机的高升力系统
EP0230061A1 (en) Trailing edge flaps
KR100558462B1 (ko) 수직 이착륙 비행체
EP1988308A2 (en) Actuator
DE102004008073A1 (de) Ausfahrtriebwerk
CN113879528B (zh) 推控一体扑翼机构
CN120735941B (zh) 一种可多维连续变体的机翼结构
CN116714801B (zh) 一种旋翼飞行器倾转结构
KR200301387Y1 (ko) 쌍회전 날개식 수직이착륙 비행체
JP2025176630A (ja) 無人航空機の離着陸ポート
CN120793158A (zh) 一种设有远心连杆倾转机构的倾转旋翼机
WO1984002506A1 (en) Variable camber leading edge assembly for an airfoil

Legal Events

Date Code Title Description
EEER Examination request

Effective date: 20140224

MKLA Lapsed

Effective date: 20180312