ATE521533T1 - Ausfahrmechanismus für vorflügel - Google Patents

Ausfahrmechanismus für vorflügel

Info

Publication number
ATE521533T1
ATE521533T1 AT09724701T AT09724701T ATE521533T1 AT E521533 T1 ATE521533 T1 AT E521533T1 AT 09724701 T AT09724701 T AT 09724701T AT 09724701 T AT09724701 T AT 09724701T AT E521533 T1 ATE521533 T1 AT E521533T1
Authority
AT
Austria
Prior art keywords
pinion
drive member
rack
drive
drive shaft
Prior art date
Application number
AT09724701T
Other languages
German (de)
English (en)
Inventor
Alan Mann
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
Application granted granted Critical
Publication of ATE521533T1 publication Critical patent/ATE521533T1/de

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)
AT09724701T 2008-03-28 2009-03-12 Ausfahrmechanismus für vorflügel ATE521533T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
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 (1)

Publication Number Publication Date
ATE521533T1 true ATE521533T1 (de) 2011-09-15

Family

ID=39386871

Family Applications (1)

Application Number Title Priority Date Filing Date
AT09724701T ATE521533T1 (de) 2008-03-28 2009-03-12 Ausfahrmechanismus für vorflügel

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
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
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
ATE521533T1 (de) Ausfahrmechanismus für vorflügel
JP2011515277A5 (enExample)
ATE544974T1 (de) Stellantrieb
ATE543728T1 (de) Steuerungseinrichtung eines hubschrauber- hauptrotors
WO2014011252A3 (en) Geared architecture with speed change device for gas turbine engine
SG10201401514UA (en) Geared architecture for high speed and small volume fan drive turbine
DE602008002787D1 (de) Fräsvorrichtung
NO20093594A1 (no) Rotormekanisme for helikoptere
BRPI0921131A2 (pt) trem de pouso de aeronave.
ATE542767T1 (de) Auslösevorrichtung für einen geschwindigkeitsbegrenzer einer aufzugsanlage
ATE516118T1 (de) Greifmechanismus mit geteilter antriebswelle für einen greiferfinger
BR112012000935A2 (pt) trem de aterrissagem de aeronave, e, aeronave.
NO20093336A1 (no) Rotormekanisme for helikoptere
BRPI0814322A2 (pt) Processo de fabricação de uma peça mecânica, peça de mecânica, trem de pouso, turbomáquina, aeronave e, dispositivo de bobinamento.
UA104564C2 (uk) Коробка передач для механізованого сільськогосподарського знаряддя і механізоване сільськогосподарське знаряддя, що містить цю коробку передач
HK1197631A2 (en) Micrometric adjustment of the endshake of a timepiece wheel set
BR112014017362A2 (pt) ligação entre um veio de transmissão de um motor e um veio acionado de um dispositivo acionado
ATE546280T1 (de) Vorrichtung zum variablen antreiben einer hohlwelle mit einer innenliegenden spindel
DK2315646T3 (da) Fastgørelsesværktøj med en sensor med fleksibelt blad
BRPI0922369A2 (pt) correia dentada para acionamento de uma árvore de cames em motores de altas potência.
WO2009132364A3 (en) Incremental variable transmission
EA201190044A1 (ru) Исполнительный механизм для нисходящей скважины
WO2014180958A3 (de) Antriebssystem
WO2011149847A3 (en) The moving rail hanger
IN2012DN00931A (enExample)

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties