DE3668438D1 - Federbeladene vorderkantenklappe. - Google Patents

Federbeladene vorderkantenklappe.

Info

Publication number
DE3668438D1
DE3668438D1 DE8686201364T DE3668438T DE3668438D1 DE 3668438 D1 DE3668438 D1 DE 3668438D1 DE 8686201364 T DE8686201364 T DE 8686201364T DE 3668438 T DE3668438 T DE 3668438T DE 3668438 D1 DE3668438 D1 DE 3668438D1
Authority
DE
Germany
Prior art keywords
spring
front edge
edge flap
loaded front
loaded
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.)
Expired - Fee Related
Application number
DE8686201364T
Other languages
English (en)
Inventor
James B Cole
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Boeing Co
Original Assignee
Boeing Co
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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=25215536&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE3668438(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Boeing Co filed Critical Boeing Co
Application granted granted Critical
Publication of DE3668438D1 publication Critical patent/DE3668438D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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
    • B64C9/24—Adjustable control surfaces or members, e.g. rudders forming slots at the front of the wing by single flap
    • 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
    • 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
    • Y02T50/30—Wing lift efficiency

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Blinds (AREA)
  • Specific Sealing Or Ventilating Devices For Doors And Windows (AREA)
  • Perforating, Stamping-Out Or Severing By Means Other Than Cutting (AREA)
DE8686201364T 1985-12-30 1986-08-01 Federbeladene vorderkantenklappe. Expired - Fee Related DE3668438D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US06/814,604 US4753402A (en) 1985-12-30 1985-12-30 Biased leading edge slat apparatus

Publications (1)

Publication Number Publication Date
DE3668438D1 true DE3668438D1 (de) 1990-03-01

Family

ID=25215536

Family Applications (2)

Application Number Title Priority Date Filing Date
DE8686201364T Expired - Fee Related DE3668438D1 (de) 1985-12-30 1986-08-01 Federbeladene vorderkantenklappe.
DE19863643157 Withdrawn DE3643157A1 (de) 1985-12-30 1986-12-17 Vorgespannte vorderkantenvorfluegeleinrichtung

Family Applications After (1)

Application Number Title Priority Date Filing Date
DE19863643157 Withdrawn DE3643157A1 (de) 1985-12-30 1986-12-17 Vorgespannte vorderkantenvorfluegeleinrichtung

Country Status (4)

Country Link
US (1) US4753402A (de)
EP (1) EP0230681B2 (de)
JP (1) JPS62157895A (de)
DE (2) DE3668438D1 (de)

Families Citing this family (57)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
US5544847A (en) * 1993-11-10 1996-08-13 The Boeing Company Leading edge slat/wing combination
GB2304656B (en) * 1995-08-26 1999-10-13 British Aerospace Deployment mechanisms for aircraft auxiliary aerofoils
US5927656A (en) * 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
US6644168B1 (en) * 2002-08-12 2003-11-11 General Dynamics Armament And Technical Products, Inc. System and method for active control of recoil mechanism
GB0410375D0 (en) * 2004-05-10 2004-06-16 Airbus Uk Ltd High lift device for an aircraft
US7101297B2 (en) * 2004-06-10 2006-09-05 Moog Inc. Compact actuator
EP1757519B1 (de) * 2005-08-25 2010-03-31 GKN Aerospace Services Limited Vorflügel für eine Flugzeugtragfläche
US20070102587A1 (en) * 2005-11-07 2007-05-10 The Boeing Company Wing leading edge slat system
DE102006030315A1 (de) * 2006-06-30 2008-01-17 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs
US7912548B2 (en) * 2006-07-21 2011-03-22 Cardiac Pacemakers, Inc. Resonant structures for implantable devices
GB0708641D0 (en) * 2007-05-04 2007-06-13 Goodrich Actuation Systems Ltd Actuator
JP4699487B2 (ja) 2007-05-25 2011-06-08 三菱重工業株式会社 高揚力発生装置、翼および高揚力発生装置の騒音低減構造
US7913949B2 (en) 2007-06-11 2011-03-29 The Boeing Company Symmetric leading edge device and method to delay flow separation
GB0721284D0 (en) * 2007-10-31 2007-12-12 Airbus Uk Ltd Actuation system for leading edge high-lift device
GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
US20140131512A1 (en) * 2007-12-06 2014-05-15 Roller Bearing Company Of America, Inc. Seal and electrical conductor for lined track rollers used on actuation system for aircraft lift assisting devices
US10023302B2 (en) * 2007-12-06 2018-07-17 Roller Bearing Company Of America, Inc. Actuation system for a lift assisting device and lined track rollers used therein
US10400818B2 (en) * 2007-12-06 2019-09-03 Roller Bearing Company Of America, Inc. Track roller bearings with rolling elements or liners
US20140339358A1 (en) * 2007-12-06 2014-11-20 Roller Bearing Company Of America, Inc. Electrical conductor for lined track rollers used on actuation system for aircraft lift assisting devices
US8025257B2 (en) * 2007-12-06 2011-09-27 Roller Bearing Company Of America, Inc. Actuation system for a lift assisting device and roller bearings used therein
US20110220762A1 (en) * 2007-12-06 2011-09-15 Roller Bearing Company Of America, Inc. Actuation system for a lift assisting device and roller bearings used therein
GB0805599D0 (en) * 2008-03-28 2008-04-30 Airbus Uk Ltd Slat deployment mechanism
GB0810460D0 (en) * 2008-06-09 2008-07-09 Airbus Uk Ltd Support assembly
GB0810724D0 (en) 2008-06-12 2008-07-16 Airbus Uk Ltd Slat assembly
GB0816022D0 (en) * 2008-09-03 2008-10-08 Airbus Uk Ltd Slat support assembly
DE102008050544A1 (de) 2008-10-06 2010-04-29 Airbus Deutschland Gmbh An der Tragfläche eines Flugzeugs angeordneter Vorflügel
GB0906074D0 (en) 2009-04-08 2009-05-20 Airbus Uk Ltd Track container
US9261132B2 (en) 2009-04-24 2016-02-16 Roller Bearing Company Of America, Inc. Low friction bearing assembly and link apparatus
ES2427390T3 (es) * 2009-10-29 2013-10-30 Asco Industries Carril de guiado para dispositivo hipersustentador
GB201008773D0 (en) * 2010-05-26 2010-07-14 Airbus Uk Ltd Aircraft slat assembly
DE102011018906A1 (de) * 2011-04-28 2012-10-31 Airbus Operations Gmbh Hochauftriebssystem für ein Flugzeug und Verfahren zum Beeinflussen der Hochauftriebseigenschaften eines Flugzeugs
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
GB201121435D0 (en) * 2011-12-14 2012-01-25 Airbus Operations Ltd Aircraft wing assembly
EP2844886B1 (de) 2012-04-30 2018-11-07 Roller Bearing Company of America, Inc. Hybride lageranordnung mit wälzkörper und gleitlager
GB201209686D0 (en) * 2012-05-31 2012-07-18 Airbus Operations Ltd A slat support assembly
GB2530326A (en) * 2014-09-22 2016-03-23 Airbus Operations Ltd A link for coupling an aircraft lift device to a track
GB2533311A (en) * 2014-12-15 2016-06-22 Airbus Operations Ltd A track container
GB201522327D0 (en) * 2015-12-17 2016-02-03 Airbus Operations Ltd Wing structure
AT518606A1 (de) * 2016-04-29 2017-11-15 Facc Ag Aerodynamischer Profilkörper für ein Flugzeug
GB2562019A (en) * 2016-11-14 2018-11-07 Airbus Operations Ltd Roller components
EP3326909B1 (de) 2016-11-23 2019-10-02 Airbus Operations GmbH Vorflügelanordnung
EP3339165B1 (de) * 2016-12-22 2020-09-09 Goodrich Actuation Systems Limited Flügelvorflügelaktuatortrennungserkennung
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
CN110546065B (zh) * 2017-04-28 2023-09-05 空中客车运作有限责任公司 飞行器的机翼和其中的连接组件以及具有这种机翼的飞机
US11577819B2 (en) 2017-04-28 2023-02-14 Airbus Operations Gmbh Wing for an aircraft
US10364019B2 (en) * 2017-12-13 2019-07-30 Thomas Hsueh Aircraft flap mechanism
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
WO2019154698A1 (en) * 2018-02-06 2019-08-15 Airbus Operations Gmbh Wing for an aircraft
GB2579221A (en) * 2018-11-26 2020-06-17 Airbus Operations Ltd Aircraft control mechanism
US11840336B2 (en) 2019-05-28 2023-12-12 Airbus Operations Gmbh Antivibration kit-of-parts and parts therefor, airfoil structure and aircraft provided therewith
US11420727B2 (en) * 2019-07-25 2022-08-23 Airbus Operations Gmbh Airfoil arrangement for an aircraft
GB2588899A (en) * 2019-11-12 2021-05-19 Airbus Operations Ltd Aircraft wings having moveable structures
EP3878734B1 (de) * 2020-03-11 2023-07-19 Airbus Operations GmbH Führungselement für eine hochauftriebsprofilanordnung eines flugzeugs, hochauftriebsprofilanordnung und herstellungsverfahren
EP4032801B1 (de) * 2021-01-22 2024-08-28 Airbus Operations GmbH Flügel für ein flugzeug
EP4140878A1 (de) 2021-08-31 2023-03-01 Airbus Operations GmbH Flügel für ein flugzeug

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1780838A (en) * 1927-07-09 1930-11-04 Handley Page Ltd Means for controlling aeroplanes
US1830019A (en) * 1931-05-06 1931-11-03 Edward H Davis Airplane
US2361574A (en) * 1940-02-28 1944-10-31 Tampier Rene Aircraft
US2406475A (en) * 1944-02-19 1946-08-27 Samuel H Pearis Slotted airplane wing
US2938680A (en) * 1957-07-02 1960-05-31 North American Aviation Inc Multiple position airfoil slat
EP0227643A3 (de) * 1980-08-13 1988-07-20 The Boeing Company Führungseinbau für einen ausziehbaren Tragflügel
US4422606A (en) * 1981-06-25 1983-12-27 Munroe Ronald G Automatic leading edge slat for aircraft
FR2547270B1 (fr) * 1983-06-10 1985-09-06 Boeing Co Mecanisme d'extension et de retraction pour un volet de bord d'attaque d'une aile d'avion

Also Published As

Publication number Publication date
EP0230681A2 (de) 1987-08-05
US4753402A (en) 1988-06-28
EP0230681B1 (de) 1990-01-24
EP0230681B2 (de) 1993-04-14
EP0230681A3 (en) 1988-01-07
DE3643157A1 (de) 1987-07-02
JPS62157895A (ja) 1987-07-13

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8366 Restricted maintained after opposition proceedings
8339 Ceased/non-payment of the annual fee