RU2502636C2 - Опорная сборка предкрылка - Google Patents

Опорная сборка предкрылка Download PDF

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Publication number
RU2502636C2
RU2502636C2 RU2011112784/11A RU2011112784A RU2502636C2 RU 2502636 C2 RU2502636 C2 RU 2502636C2 RU 2011112784/11 A RU2011112784/11 A RU 2011112784/11A RU 2011112784 A RU2011112784 A RU 2011112784A RU 2502636 C2 RU2502636 C2 RU 2502636C2
Authority
RU
Russia
Prior art keywords
slat
axis
bearing
support arm
support
Prior art date
Application number
RU2011112784/11A
Other languages
English (en)
Russian (ru)
Other versions
RU2011112784A (ru
Inventor
Саймон Джон 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 RU2011112784A publication Critical patent/RU2011112784A/ru
Application granted granted Critical
Publication of RU2502636C2 publication Critical patent/RU2502636C2/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
    • B64C9/02—Mounting or supporting thereof
    • 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)
  • Aviation & Aerospace Engineering (AREA)
  • Chain Conveyers (AREA)
  • Blinds (AREA)
  • Mechanical Engineering (AREA)
  • Automation & Control Theory (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
  • Bearings For Parts Moving Linearly (AREA)
RU2011112784/11A 2008-09-03 2009-08-27 Опорная сборка предкрылка RU2502636C2 (ru)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
GBGB0816022.8A GB0816022D0 (en) 2008-09-03 2008-09-03 Slat support assembly
GB0816022.8 2008-09-03
PCT/GB2009/051078 WO2010026410A2 (en) 2008-09-03 2009-08-27 Slat support assembly

Publications (2)

Publication Number Publication Date
RU2011112784A RU2011112784A (ru) 2012-10-10
RU2502636C2 true RU2502636C2 (ru) 2013-12-27

Family

ID=39866171

Family Applications (1)

Application Number Title Priority Date Filing Date
RU2011112784/11A RU2502636C2 (ru) 2008-09-03 2009-08-27 Опорная сборка предкрылка

Country Status (9)

Country Link
US (1) US9016636B2 (enExample)
EP (1) EP2318269B1 (enExample)
JP (1) JP5497764B2 (enExample)
CN (1) CN102143886B (enExample)
BR (1) BRPI0918493A2 (enExample)
CA (1) CA2734686C (enExample)
GB (1) GB0816022D0 (enExample)
RU (1) RU2502636C2 (enExample)
WO (1) WO2010026410A2 (enExample)

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* Cited by examiner, † Cited by third party
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GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
US10400818B2 (en) 2007-12-06 2019-09-03 Roller Bearing Company Of America, Inc. Track roller bearings with rolling elements or liners
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
GB201006099D0 (en) * 2010-04-13 2010-05-26 Airbus Operations Ltd Slat support assembly
GB201209686D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A slat support assembly
JP6144487B2 (ja) * 2012-12-26 2017-06-07 三菱航空機株式会社 フラップの展開装置、及び、航空機
CN103612749B (zh) * 2013-11-27 2016-06-22 中国航空工业集团公司西安飞机设计研究所 一种姿态可调整的前缘缝翼
GB2527490A (en) * 2014-04-17 2015-12-30 Ip Dept Airbus Operations Ltd A bearing block for a slat support assembly
EP3303122A2 (en) * 2015-06-03 2018-04-11 Aerosud Technology Solutions (pty) Ltd. Composite slat can assembly
GB201522327D0 (en) * 2015-12-17 2016-02-03 Airbus Operations Ltd Wing structure
EP3326909B1 (en) * 2016-11-23 2019-10-02 Airbus Operations GmbH Slat assembly
EP3378762A1 (en) 2017-03-24 2018-09-26 Airbus Operations GmbH Wing for an aircraft
EP3378760A1 (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
EP3395679B1 (en) * 2017-04-28 2021-09-01 Airbus Operations GmbH Wing for an aircraft
WO2018197265A1 (en) * 2017-04-28 2018-11-01 Airbus Operations Gmbh Wing for an aircraft
RU2746479C1 (ru) * 2017-04-28 2021-04-14 Эйрбас Оперейшнз Гмбх Консоль крыла для летательного аппарата
EP3444182B1 (en) * 2017-08-18 2023-01-18 Airbus Operations GmbH Wing for an aircraft
US10364019B2 (en) * 2017-12-13 2019-07-30 Thomas Hsueh Aircraft flap mechanism
EP3501977B1 (en) 2017-12-19 2021-08-11 Asco Industries NV Deployment system for an airfoil high lift leading edge device
WO2019154698A1 (en) * 2018-02-06 2019-08-15 Airbus Operations Gmbh Wing for an aircraft
US11192631B2 (en) * 2018-06-19 2021-12-07 Airbus Operations Gmbh Connection assembly for transmitting loads between two wing elements
US11383821B2 (en) * 2019-03-22 2022-07-12 Airbus Operations Gmbh Wing leading-edge device and a wing having such a wing leading-edge device
US11608156B2 (en) * 2019-03-26 2023-03-21 Yaborä Indústria Aeronáutica S.A. Lateral roller assemblies for wing leading edge slat tracks
MA53107A (fr) 2019-03-29 2021-05-19 Airbus Operations Gmbh Aile d'aéronef
US11420727B2 (en) 2019-07-25 2022-08-23 Airbus Operations Gmbh Airfoil arrangement for an aircraft
EP4032801B1 (en) 2021-01-22 2024-08-28 Airbus Operations GmbH Wing for an aircraft
EP4032803A1 (en) 2021-01-25 2022-07-27 Airbus Operations GmbH A linear drive device for an aircraft, a drive arrangement and an aircraft having such a linear drive device
US11897613B2 (en) 2021-06-08 2024-02-13 Airbus Operations Gmbh Wing for an aircraft
EP4137401B1 (en) * 2021-08-18 2025-12-17 Airbus Operations GmbH High-lift device connection assembly as well as wing and aircraft equipped therewith
BE1030173B1 (fr) * 2022-01-11 2023-08-10 Sonaca Volet mobile de bord d'attaque a chemins multiples de passage d'efforts
EP4400412B1 (en) * 2023-01-16 2026-08-12 Airbus Operations GmbH Track housing for an aircraft wing as well as wing for an aircraft
EP4491506A1 (en) 2023-07-12 2025-01-15 Airbus Operations GmbH Wing for an aircraft and high lift assembly
DE102024132505A1 (de) * 2024-11-07 2026-05-07 Airbus Operations Gmbh Flügel für ein Flugzeug
EP4772436A1 (en) * 2025-01-02 2026-07-08 AIRBUS Operations GmbH Support and carriage assemblies for a high lift body arrangement, as well as wing and aircraft comprising same

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB593303A (en) * 1944-03-06 1947-10-14 Sncan Guiding-device for slide-rod
EP0291328A2 (en) * 1987-05-13 1988-11-17 British Aerospace Public Limited Company A mechanism for supporting and extending a high lift device for aircraft wings
RU2114029C1 (ru) * 1997-07-03 1998-06-27 Титов Андрей Анатольевич Кинестетическое устройство управления двигателями самолета
RU30705U1 (ru) * 2003-02-03 2003-07-10 Федеральное государственное унитарное предприятие Лётно-исследовательский институт им. М.М.Громова Исполнительный механизм системы автоматического управления самолётом

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GB1572004A (en) 1978-03-30 1980-07-23 Hawker Siddeley Aviation Ltd Aircraft wings
US4286649A (en) 1980-06-16 1981-09-01 Rokop Corporation Apparatus for storing a continuous casting starting bar in elevated position
EP0045988B2 (en) * 1980-08-13 1993-10-06 The Boeing Company Extendible airfoil track assembly
US4614382A (en) * 1984-09-21 1986-09-30 Hiroshi Teramachi Straight sliding roller bearing
JPS6196213A (ja) * 1984-10-16 1986-05-14 Hiroshi Teramachi 直線摺動用ロ−ラ−ベアリング
US4753402A (en) * 1985-12-30 1988-06-28 The Boeing Company Biased leading edge slat apparatus
GB2304656B (en) * 1995-08-26 1999-10-13 British Aerospace Deployment mechanisms for aircraft auxiliary aerofoils
JPH10252763A (ja) * 1997-03-14 1998-09-22 Toyo Electric Mfg Co Ltd 軸受保持装置
FR2840657B1 (fr) 2002-06-05 2004-11-26 Roulements Soc Nouvelle Roulement a moyen d'engrenage integre
GB2390248A (en) * 2002-06-28 2003-12-31 Sony Uk Ltd Watermarking a reduced bandwidth version of material
US7101297B2 (en) * 2004-06-10 2006-09-05 Moog Inc. Compact actuator
GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
ES2427390T3 (es) * 2009-10-29 2013-10-30 Asco Industries Carril de guiado para dispositivo hipersustentador

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB593303A (en) * 1944-03-06 1947-10-14 Sncan Guiding-device for slide-rod
EP0291328A2 (en) * 1987-05-13 1988-11-17 British Aerospace Public Limited Company A mechanism for supporting and extending a high lift device for aircraft wings
RU2114029C1 (ru) * 1997-07-03 1998-06-27 Титов Андрей Анатольевич Кинестетическое устройство управления двигателями самолета
RU30705U1 (ru) * 2003-02-03 2003-07-10 Федеральное государственное унитарное предприятие Лётно-исследовательский институт им. М.М.Громова Исполнительный механизм системы автоматического управления самолётом

Also Published As

Publication number Publication date
GB0816022D0 (en) 2008-10-08
CA2734686A1 (en) 2010-03-11
RU2011112784A (ru) 2012-10-10
CN102143886B (zh) 2014-01-01
EP2318269A2 (en) 2011-05-11
JP5497764B2 (ja) 2014-05-21
US9016636B2 (en) 2015-04-28
WO2010026410A2 (en) 2010-03-11
CA2734686C (en) 2014-04-15
WO2010026410A3 (en) 2010-06-03
BRPI0918493A2 (pt) 2015-12-01
EP2318269B1 (en) 2015-01-28
CN102143886A (zh) 2011-08-03
JP2012501895A (ja) 2012-01-26
US20110168849A1 (en) 2011-07-14

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

Effective date: 20160828