JP2011522730A5 - - Google Patents

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Publication number
JP2011522730A5
JP2011522730A5 JP2011512211A JP2011512211A JP2011522730A5 JP 2011522730 A5 JP2011522730 A5 JP 2011522730A5 JP 2011512211 A JP2011512211 A JP 2011512211A JP 2011512211 A JP2011512211 A JP 2011512211A JP 2011522730 A5 JP2011522730 A5 JP 2011522730A5
Authority
JP
Japan
Prior art keywords
bearing
support assembly
shaft
assembly according
guide 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.)
Granted
Application number
JP2011512211A
Other languages
English (en)
Japanese (ja)
Other versions
JP5352668B2 (ja
JP2011522730A (ja
Filing date
Publication date
Priority claimed from GBGB0810460.6A external-priority patent/GB0810460D0/en
Application filed filed Critical
Publication of JP2011522730A publication Critical patent/JP2011522730A/ja
Publication of JP2011522730A5 publication Critical patent/JP2011522730A5/ja
Application granted granted Critical
Publication of JP5352668B2 publication Critical patent/JP5352668B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2011512211A 2008-06-09 2009-06-02 支持アセンブリ Expired - Fee Related JP5352668B2 (ja)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GB0810460.6 2008-06-09
GBGB0810460.6A GB0810460D0 (en) 2008-06-09 2008-06-09 Support assembly
PCT/GB2009/050601 WO2009150445A1 (en) 2008-06-09 2009-06-02 Support assembly

Publications (3)

Publication Number Publication Date
JP2011522730A JP2011522730A (ja) 2011-08-04
JP2011522730A5 true JP2011522730A5 (enExample) 2012-06-07
JP5352668B2 JP5352668B2 (ja) 2013-11-27

Family

ID=39638360

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011512211A Expired - Fee Related JP5352668B2 (ja) 2008-06-09 2009-06-02 支持アセンブリ

Country Status (10)

Country Link
US (1) US8490927B2 (enExample)
EP (1) EP2282930B1 (enExample)
JP (1) JP5352668B2 (enExample)
CN (1) CN102046466B (enExample)
AT (1) ATE547322T1 (enExample)
BR (1) BRPI0915066A2 (enExample)
CA (1) CA2725479C (enExample)
GB (1) GB0810460D0 (enExample)
RU (1) RU2502637C2 (enExample)
WO (1) WO2009150445A1 (enExample)

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US8371520B2 (en) * 2009-07-31 2013-02-12 William Craig Easter Rapidly convertible hybrid aircraft and manufacturing method
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GB201008773D0 (en) 2010-05-26 2010-07-14 Airbus Uk Ltd Aircraft slat assembly
US9359972B2 (en) * 2011-08-31 2016-06-07 United Technologies Corporation Multi axis slide carriage system
GB201117340D0 (en) * 2011-10-07 2011-11-23 Airbus Uk Ltd Flat support
US8876065B2 (en) * 2011-10-21 2014-11-04 Gulfstream Aerospace Corporation Flap roller arrangement, flap assembly, and method for removing a roller assembly from a flap fitting
US9016623B2 (en) * 2011-11-30 2015-04-28 The Boeing Company Jam protection and alleviation for control surface linkage mechanisms
CN102554821B (zh) * 2011-12-28 2014-02-26 西北工业大学 一种外前襟翼定位器
GB201209686D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A slat support assembly
GB201222308D0 (en) * 2012-12-11 2013-01-23 Airbus Operations Ltd Support assembly
US9296471B2 (en) * 2013-10-06 2016-03-29 The Boeing Company Swing wing tip system, assembly and method with dual load path structure
GB2530326A (en) * 2014-09-22 2016-03-23 Airbus Operations Ltd A link for coupling an aircraft lift device to a track
US10472046B1 (en) 2016-02-03 2019-11-12 Lockheed Martin Corporation Internal wing control surface linkage system
EP3301017B1 (en) 2016-09-30 2019-08-07 Airbus Operations GmbH System for driving and guiding of a trailing edge control surface
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
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US10882601B2 (en) * 2017-10-13 2021-01-05 The Boeing Company Aircraft wings having improved deflection control ribs
EP3501977B1 (en) 2017-12-19 2021-08-11 Asco Industries NV Deployment system for an airfoil high lift leading edge device
CN108082449B (zh) * 2018-03-06 2022-06-10 中航通飞华南飞机工业有限公司 一种大型飞机舵面悬挂结构
US10889365B2 (en) * 2018-03-15 2021-01-12 The Boeing Company Auxiliary support system for a flap of an aircraft wing
GB2573120A (en) * 2018-04-24 2019-10-30 Airbus Operations Ltd Improved secondary locking mechanism
US11059563B2 (en) * 2018-09-06 2021-07-13 The Boeing Company Collapsible flap deployment system for a wing of an aircraft
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US11142299B2 (en) * 2019-05-31 2021-10-12 The Boeing Company Flap interconnect for deflection control
US11161594B2 (en) * 2019-09-25 2021-11-02 The Boeing Company Flap support breakaway and fail safety configuration
IT201900019385A1 (it) * 2019-10-21 2021-04-21 Leonardo Spa Gruppo rullo regolabile per la movimentazione di uno slat di un’ala di un aeromobile
US11338907B2 (en) * 2020-05-29 2022-05-24 The Boeing Company Actuation assemblies for flight control surfaces
CN113501126B (zh) * 2021-05-26 2024-05-10 中国商用飞机有限责任公司 一种用于飞行器的襟翼支持装置
CN113049211B (zh) * 2021-06-01 2021-08-10 中国空气动力研究与发展中心低速空气动力研究所 一种风洞试验装置
CN113933053B (zh) * 2021-09-15 2024-03-19 东北林业大学 非接触感应式摩擦电轴承传感器及其测试方法
US11754019B2 (en) 2021-12-17 2023-09-12 Rohr, Inc. Articulating slider for nacelle
CN114212240B (zh) * 2021-12-23 2023-08-29 成都市鸿侠科技有限责任公司 一种耐用型飞机襟翼滑轨及其加工工艺
US12024289B2 (en) * 2022-08-23 2024-07-02 Gulfstream Aerospace Corporation Reduced-friction roller and related assembly for a moveable control surface of an aircraft
EP4574653A1 (en) * 2023-12-20 2025-06-25 Airbus Operations GmbH Wing for an aircraft
CN118214352A (zh) * 2024-03-14 2024-06-18 天合光能股份有限公司 连接桥架机构及跟踪支架系统

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