RU2492110C2 - Механизм выпуска предкрылка - Google Patents

Механизм выпуска предкрылка Download PDF

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Publication number
RU2492110C2
RU2492110C2 RU2010142990/11A RU2010142990A RU2492110C2 RU 2492110 C2 RU2492110 C2 RU 2492110C2 RU 2010142990/11 A RU2010142990/11 A RU 2010142990/11A RU 2010142990 A RU2010142990 A RU 2010142990A RU 2492110 C2 RU2492110 C2 RU 2492110C2
Authority
RU
Russia
Prior art keywords
drive element
slat
gear
drive
mechanism according
Prior art date
Application number
RU2010142990/11A
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English (en)
Russian (ru)
Other versions
RU2010142990A (ru
Inventor
Алан МАНН
Original Assignee
ЭЙРБАС ЮКей ЛИМИТЕД
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Application filed by ЭЙРБАС ЮКей ЛИМИТЕД filed Critical ЭЙРБАС ЮКей ЛИМИТЕД
Publication of RU2010142990A publication Critical patent/RU2010142990A/ru
Application granted granted Critical
Publication of RU2492110C2 publication Critical patent/RU2492110C2/ru

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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)
RU2010142990/11A 2008-03-28 2009-03-12 Механизм выпуска предкрылка RU2492110C2 (ru)

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 (2)

Publication Number Publication Date
RU2010142990A RU2010142990A (ru) 2012-05-10
RU2492110C2 true RU2492110C2 (ru) 2013-09-10

Family

ID=39386871

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010142990/11A RU2492110C2 (ru) 2008-03-28 2009-03-12 Механизм выпуска предкрылка

Country Status (9)

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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2765168C2 (ru) * 2016-09-23 2022-01-26 Эйрбас Оперейшнз Гмбх Направляющее устройство для предкрылка крыла воздушного судна

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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
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
EP3395678B1 (en) 2017-04-26 2021-05-26 Asco Industries NV Guidance assembly for an airfoil leading edge high-lift device carrier track
EP3615422B1 (en) 2017-04-28 2024-10-30 Airbus Operations GmbH Wing for an aircraft
JP6840893B2 (ja) 2017-04-28 2021-03-10 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
ES2886667T3 (es) 2017-12-19 2021-12-20 Asco Ind Nv Sistema de despliegue para un dispositivo de borde de ataque de sustentación elevada de perfil aerodinámico
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
US11845550B2 (en) * 2019-02-28 2023-12-19 Airbus Operations Gmbh 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
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
US12441455B1 (en) 2025-01-27 2025-10-14 The Boeing Company Wing assemblies and aircraft with gap-adjustment assemblies for slats

Citations (3)

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Publication number Priority date Publication date Assignee Title
US2938680A (en) * 1957-07-02 1960-05-31 North American Aviation Inc Multiple position airfoil slat
US3272458A (en) * 1964-12-08 1966-09-13 Gen Dynamics Corp Means for positioning a rotating wing slat device
RU2238219C2 (ru) * 2001-07-12 2004-10-20 Еадс Дойчланд Гмбх Механизм управления элементом механизации крыла

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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
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 (https=) 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
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
US8245982B2 (en) * 2007-03-09 2012-08-21 Asco Industries Wing
GB2458683A (en) * 2008-03-28 2009-09-30 Airbus Uk Ltd Aircraft slat deployment mechanism
GB0805599D0 (en) * 2008-03-28 2008-04-30 Airbus Uk Ltd 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
US3272458A (en) * 1964-12-08 1966-09-13 Gen Dynamics Corp Means for positioning a rotating wing slat device
RU2238219C2 (ru) * 2001-07-12 2004-10-20 Еадс Дойчланд Гмбх Механизм управления элементом механизации крыла

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2765168C2 (ru) * 2016-09-23 2022-01-26 Эйрбас Оперейшнз Гмбх Направляющее устройство для предкрылка крыла воздушного судна

Also Published As

Publication number Publication date
RU2010142990A (ru) 2012-05-10
WO2009118547A3 (en) 2009-11-26
JP2011515277A (ja) 2011-05-19
CA2719173A1 (en) 2009-10-01
JP5336575B2 (ja) 2013-11-06
EP2268540A2 (en) 2011-01-05
ATE521533T1 (de) 2011-09-15
US8511619B2 (en) 2013-08-20
CA2719173C (en) 2014-06-17
US20110036944A1 (en) 2011-02-17
CN102007036B (zh) 2013-11-20
EP2268540B1 (en) 2011-08-24
GB0805599D0 (en) 2008-04-30
CN102007036A (zh) 2011-04-06
WO2009118547A2 (en) 2009-10-01

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MM4A The patent is invalid due to non-payment of fees

Effective date: 20170313