RU2502637C2 - Опорный узел - Google Patents

Опорный узел Download PDF

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Publication number
RU2502637C2
RU2502637C2 RU2010154308/11A RU2010154308A RU2502637C2 RU 2502637 C2 RU2502637 C2 RU 2502637C2 RU 2010154308/11 A RU2010154308/11 A RU 2010154308/11A RU 2010154308 A RU2010154308 A RU 2010154308A RU 2502637 C2 RU2502637 C2 RU 2502637C2
Authority
RU
Russia
Prior art keywords
bearing
shaft
flap
guide track
bearing housing
Prior art date
Application number
RU2010154308/11A
Other languages
English (en)
Russian (ru)
Other versions
RU2010154308A (ru
Inventor
Саймон ПАРКЕР
Original Assignee
Эйрбас Оперейшнз Лимитед
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 Эйрбас Оперейшнз Лимитед filed Critical Эйрбас Оперейшнз Лимитед
Publication of RU2010154308A publication Critical patent/RU2010154308A/ru
Application granted granted Critical
Publication of RU2502637C2 publication Critical patent/RU2502637C2/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
    • B64C9/16—Adjustable control surfaces or members, e.g. rudders forming slots at the rear of the wing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C23/00—Bearings for exclusively rotary movement adjustable for aligning or positioning
    • F16C23/06—Ball or roller bearings
    • F16C23/08—Ball or roller bearings self-adjusting
    • F16C23/082—Ball or roller bearings self-adjusting by means of at least one substantially spherical surface
    • F16C23/086—Ball or roller bearings self-adjusting by means of at least one substantially spherical surface forming a track for rolling elements
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C13/00—Rolls, drums, discs, or the like; Bearings or mountings therefor
    • F16C13/006—Guiding rollers, wheels or the like, formed by or on the outer element of a single bearing or bearing unit, e.g. two adjacent bearings, whose ratio of length to diameter is generally less than one
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C19/00—Bearings with rolling contact, for exclusively rotary movement
    • F16C19/02—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows
    • F16C19/14—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load
    • F16C19/18—Bearings with rolling contact, for exclusively rotary movement with bearing balls essentially of the same size in one or more circular rows for both radial and axial load with two or more rows of balls
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Bearings For Parts Moving Linearly (AREA)
  • Support Of The Bearing (AREA)
  • Insulation, Fastening Of Motor, Generator Windings (AREA)
  • Percussion Or Vibration Massage (AREA)
  • Forklifts And Lifting Vehicles (AREA)
  • Pallets (AREA)
  • Rolling Contact Bearings (AREA)
RU2010154308/11A 2008-06-09 2009-06-02 Опорный узел RU2502637C2 (ru)

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 (2)

Publication Number Publication Date
RU2010154308A RU2010154308A (ru) 2012-07-20
RU2502637C2 true RU2502637C2 (ru) 2013-12-27

Family

ID=39638360

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2010154308/11A RU2502637C2 (ru) 2008-06-09 2009-06-02 Опорный узел

Country Status (10)

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

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US8371520B2 (en) * 2009-07-31 2013-02-12 William Craig Easter Rapidly convertible hybrid aircraft and manufacturing method
GB0913473D0 (en) * 2009-08-04 2009-09-16 Airbus Operations Ltd Support assembly
US8221146B2 (en) * 2010-01-11 2012-07-17 Tyco Electronics Corporation Linearly actuated connector mating interface
DE102010006447A1 (de) * 2010-02-01 2011-08-04 Airbus Operations GmbH, 21129 Verbindungsvorrichtung
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
EP3395678B1 (en) 2017-04-26 2021-05-26 Asco Industries NV Guidance assembly for an airfoil leading edge high-lift device carrier track
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
EP3615422B1 (en) * 2017-04-28 2024-10-30 Airbus Operations GmbH Wing for an aircraft
US10882601B2 (en) * 2017-10-13 2021-01-05 The Boeing Company Aircraft wings having improved deflection control ribs
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
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
DE102018132674A1 (de) * 2018-12-18 2020-06-18 Endress+Hauser Conducta Gmbh+Co. Kg Flügelscharnier für ein Feldgerätgehäuse sowie Feldgerätgehäuse mit Flügelscharnier
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
US12509213B2 (en) * 2023-05-17 2025-12-30 The Boeing Company Auxiliary flap assembly
CN117302507B (zh) * 2023-09-15 2026-03-03 中国商用飞机有限责任公司 用于包括襟翼的机翼的襟翼支撑组件和包括襟翼的机翼
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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US3785594A (en) * 1971-03-12 1974-01-15 British Aircraft Corp Ltd Aircraft flap system
US4248486A (en) * 1978-12-15 1981-02-03 Pneumo Corporation Spherical bearing assembly with stress relief
US4471927A (en) * 1981-09-29 1984-09-18 The Boeing Company Trailing edge flap assembly
US5219232A (en) * 1991-11-27 1993-06-15 Tiodize Company, Inc. Floating bushing roller bearing
RU45708U1 (ru) * 2004-12-30 2005-05-27 Открытое акционерное общество "Туполев" (ОАО "Туполев") Механизм управления аэродинамическими поверхностями самолета

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Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3785594A (en) * 1971-03-12 1974-01-15 British Aircraft Corp Ltd Aircraft flap system
US4248486A (en) * 1978-12-15 1981-02-03 Pneumo Corporation Spherical bearing assembly with stress relief
US4471927A (en) * 1981-09-29 1984-09-18 The Boeing Company Trailing edge flap assembly
US5219232A (en) * 1991-11-27 1993-06-15 Tiodize Company, Inc. Floating bushing roller bearing
RU45708U1 (ru) * 2004-12-30 2005-05-27 Открытое акционерное общество "Туполев" (ОАО "Туполев") Механизм управления аэродинамическими поверхностями самолета

Also Published As

Publication number Publication date
CN102046466A (zh) 2011-05-04
JP2011522730A (ja) 2011-08-04
CA2725479C (en) 2013-12-10
JP5352668B2 (ja) 2013-11-27
CN102046466B (zh) 2013-07-24
GB0810460D0 (en) 2008-07-09
CA2725479A1 (en) 2009-12-17
EP2282930A1 (en) 2011-02-16
RU2010154308A (ru) 2012-07-20
EP2282930B1 (en) 2012-02-29
US20110042525A1 (en) 2011-02-24
US8490927B2 (en) 2013-07-23
ATE547322T1 (de) 2012-03-15
WO2009150445A1 (en) 2009-12-17
BRPI0915066A2 (pt) 2015-10-27

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Date Code Title Description
MM4A The patent is invalid due to non-payment of fees

Effective date: 20160603