DE69425670T2 - Nasenklappe/flügel-kombination - Google Patents

Nasenklappe/flügel-kombination

Info

Publication number
DE69425670T2
DE69425670T2 DE69425670T DE69425670T DE69425670T2 DE 69425670 T2 DE69425670 T2 DE 69425670T2 DE 69425670 T DE69425670 T DE 69425670T DE 69425670 T DE69425670 T DE 69425670T DE 69425670 T2 DE69425670 T2 DE 69425670T2
Authority
DE
Germany
Prior art keywords
nose valve
wing combination
wing
combination
nose
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 - Lifetime
Application number
DE69425670T
Other languages
English (en)
Other versions
DE69425670D1 (de
Inventor
T Bliesner
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=22534237&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE69425670(T2) "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
Publication of DE69425670D1 publication Critical patent/DE69425670D1/de
Application granted granted Critical
Publication of DE69425670T2 publication Critical patent/DE69425670T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime 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
    • 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)
  • Toys (AREA)
  • Blinds (AREA)
DE69425670T 1993-11-10 1994-11-03 Nasenklappe/flügel-kombination Expired - Lifetime DE69425670T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US08/150,374 US5544847A (en) 1993-11-10 1993-11-10 Leading edge slat/wing combination
PCT/US1994/012687 WO1995013214A1 (en) 1993-11-10 1994-11-03 Leading edge slat/wing combination

Publications (2)

Publication Number Publication Date
DE69425670D1 DE69425670D1 (de) 2000-09-28
DE69425670T2 true DE69425670T2 (de) 2000-12-28

Family

ID=22534237

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69425670T Expired - Lifetime DE69425670T2 (de) 1993-11-10 1994-11-03 Nasenklappe/flügel-kombination

Country Status (5)

Country Link
US (2) US5544847A (de)
EP (1) EP0728101B1 (de)
AU (1) AU8132394A (de)
DE (1) DE69425670T2 (de)
WO (1) WO1995013214A1 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9145199B2 (en) 2008-08-28 2015-09-29 Airbus Operations Gmbh High lift system for an aircraft with a high lift flap and method for adjusting the high lift flap

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US5927656A (en) * 1996-06-26 1999-07-27 The Boeing Company Wing leading edge flap and method therefor
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US6796534B2 (en) 2002-09-10 2004-09-28 The Boeing Company Method and apparatus for controlling airflow with a leading edge device having a flexible flow surface
US7059563B2 (en) 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
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US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
DE102005027749B4 (de) * 2005-06-16 2011-07-28 Airbus Operations GmbH, 21129 Auftriebserhöhende Klappe, insbesondere Nasenklappe, für einen aerodynamisch wirksamen Flügel
ES2341794T3 (es) * 2005-08-25 2010-06-28 Gkn Aerospace Services Limited Aleta auxiliar del borde de ataque del ala de un avion.
US20070102587A1 (en) * 2005-11-07 2007-05-10 The Boeing Company Wing leading edge slat system
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
EP1972547A1 (de) * 2007-03-21 2008-09-24 Asco Industries Flügelvorderkantenvorrichtung
EP2134597B1 (de) * 2007-03-09 2011-06-22 Asco Industries Flügel
DE102007020870A1 (de) 2007-05-04 2008-11-13 Airbus Deutschland Gmbh Hochauftriebssystem am Tragflügel eines Flugzeugs
GB0722425D0 (en) * 2007-11-15 2007-12-27 Airbus Uk Ltd Slat support funk plate
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
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
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
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
US10400818B2 (en) * 2007-12-06 2019-09-03 Roller Bearing Company Of America, Inc. Track roller bearings with rolling elements or liners
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
BE1018114A5 (fr) 2008-05-06 2010-05-04 Sonaca Sociutu Anonyme Aile d'aeronef comprenant un volet mobile de bord d'attaque equipe d'un rail suiveur contraint en deplacement selon une trajectoire en arc de cercle
DE102008050544A1 (de) 2008-10-06 2010-04-29 Airbus Deutschland Gmbh An der Tragfläche eines Flugzeugs angeordneter Vorflügel
US8226048B2 (en) * 2008-12-09 2012-07-24 The Boeing Company Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods
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US9261132B2 (en) 2009-04-24 2016-02-16 Roller Bearing Company Of America, Inc. Low friction bearing assembly and link apparatus
US8534610B1 (en) * 2009-07-17 2013-09-17 The Boeing Company Method and apparatus for a leading edge slat on a wing of an aircraft
US8534611B1 (en) 2009-07-17 2013-09-17 The Boeing Company Moveable leading edge device for a wing
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
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
GB201101274D0 (en) 2011-01-25 2011-03-09 Airbus Operations Ltd Leading edge device for an aircraft
DE102011082888B4 (de) * 2011-09-16 2016-01-07 Airbus Defence and Space GmbH Auftriebsklappenanordnung, Tragflügel sowie Flugzeug
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
GB2504744B (en) * 2012-08-08 2014-06-25 Eads Uk Ltd Aircraft wing with slat arrangement establishing laminar boundary layer flow
CN103287574B (zh) * 2013-01-05 2015-07-01 中国航空工业集团公司西安飞机设计研究所 一种飞机增升装置控制方法
US10017243B2 (en) * 2013-09-24 2018-07-10 The Boeing Company Adaptive trailing edge actuator system and method
US9180962B2 (en) 2013-09-24 2015-11-10 The Boeing Company Leading edge variable camber system and method
US9359065B2 (en) 2013-09-24 2016-06-07 The Boeing Company System and method for optimizing performance of an aircraft
US9193440B2 (en) 2013-09-24 2015-11-24 The Boeing Company Variable camber flap system and method
US9327827B2 (en) 2013-09-24 2016-05-03 The Boeing Company Leading and trailing edge device deflections during descent of an aircraft
US9771141B2 (en) * 2013-09-24 2017-09-26 The Boeing Company Leading edge system and method for approach noise reduction
US9254909B2 (en) 2013-09-24 2016-02-09 The Boeing Company Optimized flap positioning for go-around operations
US9296475B2 (en) 2013-09-24 2016-03-29 The Boeing Company System and method for reducing the stopping distance of an aircraft
US9656741B2 (en) 2013-09-24 2017-05-23 The Boeing Company Control interface for leading and trailing edge devices
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
US9821903B2 (en) 2014-07-14 2017-11-21 The Boeing Company Closed loop control of aircraft control surfaces
GB2533311A (en) * 2014-12-15 2016-06-22 Airbus Operations Ltd A track container
ES2746872T3 (es) 2015-06-18 2020-03-09 Bae Systems Plc Sistema de ala de una aeronave
EP3106386A1 (de) * 2015-06-18 2016-12-21 BAE Systems PLC Flugzeugflügelsystem
EP3310652B8 (de) 2015-06-18 2019-08-21 BAE Systems PLC Flugzeugflügelsystem
EP3299278B1 (de) * 2016-09-23 2020-06-03 Airbus Operations GmbH Vorflügelverfolgungsvorrichtung für einen flugzeugflügel
EP3395678B1 (de) 2017-04-26 2021-05-26 Asco Industries NV Führungsanordnung für eine hochauftriebsvorrichtungsträgerbahn einer tragflächenvorderkante
RU2746479C1 (ru) * 2017-04-28 2021-04-14 Эйрбас Оперейшнз Гмбх Консоль крыла для летательного аппарата
EP3615421B1 (de) 2017-04-28 2023-01-11 Airbus Operations GmbH Flügel für ein flugzeug
US10364019B2 (en) * 2017-12-13 2019-07-30 Thomas Hsueh Aircraft flap mechanism
EP3501977B1 (de) 2017-12-19 2021-08-11 Asco Industries NV Freisetzungssystem für eine hochauftriebsvorrichtung einer tragflächenvorderkante
US11192632B2 (en) 2018-10-15 2021-12-07 The Boeing Company Slat end seal and method for manufacturing the same
EP3718881B1 (de) 2019-03-29 2022-10-12 Airbus Operations GmbH Flügel für ein flugzeug
US11312473B2 (en) 2019-05-30 2022-04-26 The Boeing Company Aircraft slat aero-restoration seal door and method therefor
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US5544847A (en) * 1993-11-10 1996-08-13 The Boeing Company Leading edge slat/wing combination

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9145199B2 (en) 2008-08-28 2015-09-29 Airbus Operations Gmbh High lift system for an aircraft with a high lift flap and method for adjusting the high lift flap

Also Published As

Publication number Publication date
DE69425670D1 (de) 2000-09-28
US5839699A (en) 1998-11-24
AU8132394A (en) 1995-05-29
EP0728101A1 (de) 1996-08-28
WO1995013214A1 (en) 1995-05-18
EP0728101B1 (de) 2000-08-23
US5544847A (en) 1996-08-13

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Legal Events

Date Code Title Description
8363 Opposition against the patent
8365 Fully valid after opposition proceedings