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

スラット展開機構 Download PDF

Info

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
Authority
JP
Japan
Prior art keywords
drive member
slat
pinion
drive
track
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
JP2011501295A
Other languages
English (en)
Japanese (ja)
Other versions
JP2011515277A5 (enExample
JP2011515277A (ja
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
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 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
Publication of JP5336575B2 publication Critical patent/JP5336575B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Images

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)
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
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 (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 (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
CA2719173C (en) 2014-06-17
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
JP5336575B2 (ja) スラット展開機構
EP2309150B1 (en) Actuator arrangement
US8424801B2 (en) Slat support assembly
US6802475B2 (en) Flight surface actuator
US6467733B1 (en) Aerodynamic control surface system
US7063292B2 (en) Actuation apparatus for a control flap arranged on a trailing edge of an aircraft airfoil
US9139286B2 (en) Hinge assembly for rotatably mounting a control surface on an aircraft
US20140271204A1 (en) Tiltrotor Control System With Two Rise/Fall Actuators
EP1985893A2 (en) Actuator arrangement
JP2011515277A5 (enExample)
AU2016278099B2 (en) Aircraft wing system
CN101909991B (zh) 用于飞机的高升力系统
GB2458683A (en) Aircraft slat deployment mechanism
US10618628B2 (en) Aircraft wing system
CN101037924B (zh) 一种高性能百页窗
CN220595041U (zh) 一种展翼型汽车尾翼用驱动机构、展翼型汽车尾翼及汽车
EP3667051B1 (en) Turbofan engine comprising a thrust reverser unit with tilting beams
CN109455292B (zh) 具有主翼和高升力体的翼型件以及飞行器

Legal Events

Date Code Title Description
A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20120228

A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20120228

TRDD Decision of grant or rejection written
A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20130628

A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20130702

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20130801

R150 Certificate of patent or registration of utility model

Free format text: JAPANESE INTERMEDIATE CODE: R150

R250 Receipt of annual fees

Free format text: JAPANESE INTERMEDIATE CODE: R250

LAPS Cancellation because of no payment of annual fees