ATE416971T1 - Flugzeug mit aktiver verwindungskontrolle seiner tragflächen - Google Patents

Flugzeug mit aktiver verwindungskontrolle seiner tragflächen

Info

Publication number
ATE416971T1
ATE416971T1 AT03291277T AT03291277T ATE416971T1 AT E416971 T1 ATE416971 T1 AT E416971T1 AT 03291277 T AT03291277 T AT 03291277T AT 03291277 T AT03291277 T AT 03291277T AT E416971 T1 ATE416971 T1 AT E416971T1
Authority
AT
Austria
Prior art keywords
aircraft
plane
wing
wings
additional
Prior art date
Application number
AT03291277T
Other languages
English (en)
Inventor
Bernard Barriety
Original Assignee
Airbus France
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 Airbus France filed Critical Airbus France
Application granted granted Critical
Publication of ATE416971T1 publication Critical patent/ATE416971T1/de

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C23/00Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips
    • B64C23/072Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips using one or more wing tip airfoil devices, e.g. winglets, splines, wing tip fences or raked wingtips the wing tip airfoil devices being moveable in their entirety
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C3/00Wings
    • B64C3/38Adjustment of complete wings or parts thereof
    • B64C3/52Warping
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C5/00Stabilising surfaces
    • B64C5/08Stabilising surfaces mounted on, or supported by, wings
    • YGENERAL 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
    • Y02TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02TCLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00Aeronautics or air transport
    • Y02T50/10Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Walking Sticks, Umbrellas, And Fans (AREA)
  • Control Of Turbines (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Oxygen Or Sulfur (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
AT03291277T 2002-06-27 2003-05-28 Flugzeug mit aktiver verwindungskontrolle seiner tragflächen ATE416971T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0208011A FR2841532B1 (fr) 2002-06-27 2002-06-27 Avion a controle actif du vrillage de ses ailes

Publications (1)

Publication Number Publication Date
ATE416971T1 true ATE416971T1 (de) 2008-12-15

Family

ID=29717115

Family Applications (1)

Application Number Title Priority Date Filing Date
AT03291277T ATE416971T1 (de) 2002-06-27 2003-05-28 Flugzeug mit aktiver verwindungskontrolle seiner tragflächen

Country Status (6)

Country Link
US (1) US6827314B2 (de)
EP (1) EP1375342B1 (de)
AT (1) ATE416971T1 (de)
CA (1) CA2427357C (de)
DE (1) DE60325141D1 (de)
FR (1) FR2841532B1 (de)

Families Citing this family (67)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE10302514B4 (de) * 2003-01-23 2008-12-18 Eads Deutschland Gmbh Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche eines Fluggeräts
DE10351839B3 (de) * 2003-11-06 2005-06-16 Deutsches Zentrum für Luft- und Raumfahrt e.V. Verfahren zur Minimierung des Widerstands bei einem im Flug befindlichen Flugzeug
GB0326228D0 (en) * 2003-11-10 2003-12-17 Airbus Uk Ltd Wing tip device
US7475848B2 (en) * 2003-11-11 2009-01-13 Morgenstern John M Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
EP1531126B1 (de) * 2003-11-11 2007-02-07 Airbus UK Limited Aerodynamisch wirksame Flügelspitzenvorrichtung
DE102005028688A1 (de) * 2005-05-19 2006-11-30 Airbus Deutschland Gmbh Konzept eines variablen Winglets zur lateralen Lastenreduktion zur kombinierten lateralen und vertikalen Lastenreduktion und zur Performanceverbesserung von Fortbewegungsmitteln
EP1883577B8 (de) 2005-05-19 2010-03-10 Airbus Operations GmbH Konzept für ein variables winglet zur seitenlastverringerung für die kombinierte seiten- und vertikallastverringerung und zur leistungssteigerung durch fortbewegung
US8544800B2 (en) * 2005-07-21 2013-10-01 The Boeing Company Integrated wingtip extensions for jet transport aircraft and other types of aircraft
US7798443B2 (en) * 2006-12-18 2010-09-21 The Boeing Company Composite material for geometric morphing wing
US7744038B2 (en) * 2007-06-15 2010-06-29 The Boeing Company Controllable winglets
US7900876B2 (en) * 2007-08-09 2011-03-08 The Boeing Company Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods
US20090084904A1 (en) * 2007-10-02 2009-04-02 The Boeing Company Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods
DE102007059455A1 (de) * 2007-12-10 2009-06-25 Airbus Deutschland Gmbh Flügelspitzenverlängerung zur Reduktion von Wirbelschleppen bei Flugzeugen
US8128035B2 (en) * 2008-04-15 2012-03-06 The Boeing Company Winglets with recessed surfaces, and associated systems and methods
DE102008022452B4 (de) * 2008-05-08 2010-09-23 Bauhaus Luftfahrt E. V. Flugzeug mit aktiv steuerbaren Hilfsflügeln
CN102149599B (zh) 2008-06-20 2014-11-19 航空伙伴股份有限公司 弯曲的机翼末梢
US8944386B2 (en) 2011-06-09 2015-02-03 Aviation Partners, Inc. Split blended winglet
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
DE102009019542A1 (de) * 2009-04-30 2010-11-11 Airbus Deutschland Gmbh Nicht-planares Flügelendstück für Tragflügel von Flugzeugen sowie Tragflügel mit einem solchen Flügelendstück
US8434293B2 (en) 2009-08-06 2013-05-07 The Boeing Company High stiffness shape memory alloy actuated aerostructure
CA2783401A1 (en) * 2009-12-10 2011-06-16 University Of The Witwatersrand, Johannesburg Method for reducing in flight wake vortices and an aircraft wingtip arrangement used in such method
GB201011843D0 (en) 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
GB201018185D0 (en) * 2010-10-28 2010-12-08 Airbus Operations Ltd Wing tip device attachment apparatus and method
US10538307B2 (en) 2011-10-01 2020-01-21 The Boeing Company Hinged raked wing tip
US9499252B2 (en) 2011-10-01 2016-11-22 The Boeing Company Wing fold controller
US9290260B2 (en) 2011-10-01 2016-03-22 The Boeing Company Wing fold controller
US9211946B2 (en) 2011-10-01 2015-12-15 The Boeing Company Wing fold system with latch pins through multiple mating lugs
US9296469B2 (en) 2011-10-01 2016-03-29 The Boeing Company Horizontal folding wingtip
US8936219B2 (en) 2012-03-30 2015-01-20 The Boeing Company Performance-enhancing winglet system and method
EP3546342B1 (de) * 2012-10-30 2023-11-15 The Boeing Company Schwenkbare gepfeilte flügelspitze
US9469392B2 (en) 2012-10-30 2016-10-18 The Boeing Company Wing fold system rotating latch
US9481446B2 (en) 2012-10-30 2016-11-01 The Boeing Company System for latching and locking a foldable airfoil
US9415857B2 (en) 2012-10-30 2016-08-16 The Boeing Company Wing fold system
CA2829281C (en) * 2012-10-30 2017-05-30 The Boeing Company Wing fold controller
US9469391B1 (en) * 2013-04-26 2016-10-18 The Boeing Company Adaptive wing for an aircraft
US10696387B2 (en) * 2013-09-27 2020-06-30 Dann M Allen Helicopter rotor with a mechanical means for configuring rotor tips to control brown outs
US9296472B2 (en) * 2013-10-17 2016-03-29 The Boeing Company Wingtip control system
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
CN103625634B (zh) * 2013-12-17 2015-10-21 中国航天空气动力技术研究院 一种可拆卸可调倾角的翼梢小翼装置
GB2524827A (en) * 2014-04-04 2015-10-07 Airbus Operations Ltd A passenger aircraft with a downwardly foldable wing tip device
US9511850B2 (en) 2014-04-12 2016-12-06 The Boeing Company Wing tip device for an aircraft wing
WO2016019467A1 (en) 2014-08-05 2016-02-11 Ryan Church Structure with rigid winglet adapted to traverse a fluid environment
GB2533413A (en) 2014-12-19 2016-06-22 Airbus Operations Ltd Lifting Surfaces
CN105480404B (zh) * 2015-12-21 2018-07-03 哈尔滨工业大学 一种用于提高气动效率的可变安装角翼梢小翼结构
GB2546246A (en) * 2016-01-05 2017-07-19 Airbus Operations Ltd An aircraft wing with a movable wing tip device for load alleviation
EP3269635A1 (de) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Flugzeugflügel
GB2563261A (en) * 2017-06-08 2018-12-12 Airbus Operations Ltd Controlling aerodynamic spanload control devices
US10370084B2 (en) * 2017-07-21 2019-08-06 The Boeing Company Methods and apparatus to adjust folding wing tips
EP3486164A1 (de) * 2017-11-17 2019-05-22 Airbus Operations GmbH Verfahren und steuereinheit zur steuerung der betätigung eines klappbaren flügelendabschnitts eines flügels eines flugzeugs
EP3495258A1 (de) 2017-12-06 2019-06-12 Airbus Operations GmbH Flügel für ein flugzeug
EP3511243B1 (de) * 2018-01-15 2021-12-29 The Aircraft Performance Company GmbH Flugzeugflügel
CN108216572B (zh) * 2018-01-23 2020-12-01 中国航空工业集团公司沈阳飞机设计研究所 一种多曲轴驱动的柔性翼面组件及具有其的机翼
FR3079209A1 (fr) * 2018-03-22 2019-09-27 Francois Geli Avion gros porteur bi-reacteur a voilure non-planaire a geometrie variable
US11440638B2 (en) * 2018-05-03 2022-09-13 Airbus Operations Gmbh Wing for an aircraft
US11319054B2 (en) * 2018-05-31 2022-05-03 Airbus Operations Gmbh Wing arrangement for an aircraft
US11370526B2 (en) * 2018-05-31 2022-06-28 Airbus Operations Gmbh Latching device for a wing arrangement for an aircraft
US11214353B2 (en) * 2018-06-01 2022-01-04 Airbus Operations Gmbh Wing arrangement for an aircraft and aircraft
EP3587252A1 (de) * 2018-06-28 2020-01-01 Airbus Operations GmbH Arretiersystem zum arretieren einer ersten flugzeugkomponente in bezug auf eine zweite flugzeugkomponente
US11307598B2 (en) * 2018-07-27 2022-04-19 Ahmad Fareed Aldarwish Autonomous aircraft control systems and related methods
GB2576929A (en) * 2018-09-07 2020-03-11 Airbus Operations Ltd A wing tip device
US11254412B2 (en) * 2019-03-29 2022-02-22 The Boeing Company Foldable raked wing tips having aerodynamic devices
WO2021073706A1 (en) 2019-10-19 2021-04-22 Oddershede Magnus Wingtip
CN113955069B (zh) * 2021-10-26 2023-07-14 中国运载火箭技术研究院 一种基于主动流动控制的高速飞行器减阻闭环控制方法
GB2616252A (en) * 2022-01-31 2023-09-06 Airbus Operations Ltd Aircraft with movable wing tip device
GB2615311A (en) * 2022-01-31 2023-08-09 Airbus Operations Ltd Aircraft wing with movable wing tip device
GB2628523B (en) * 2022-11-16 2025-07-09 Airbus Operations Ltd Aircraft wing
GB2630990B (en) * 2023-06-16 2026-01-28 Airbus Operations Ltd An aircraft wing with a moveable wing tip

Family Cites Families (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2149956C3 (de) 1971-10-07 1974-03-28 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Hochauftriebsflügel
DE2756107C2 (de) * 1977-12-16 1980-02-28 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Hochwirksames Seitenleitwerk mit variabler Flügelgeometrie
FR2521520A1 (fr) * 1982-02-15 1983-08-19 Daude Martine Ailettes marginales a angles d'attaque variables
US4538779A (en) * 1982-09-30 1985-09-03 The Boeing Company Caster type empennage assembly for aircraft
DE3242584A1 (de) * 1982-11-18 1984-05-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung von zusatzflaechen an den spitzen eines tragfluegels
GB8310224D0 (en) * 1983-04-15 1983-05-18 British Aerospace Wing tip arrangement
US4776542A (en) * 1987-05-27 1988-10-11 Vigyan Research Associates, Inc. Aircraft stall-spin entry deterrent system
US5070458A (en) * 1989-03-31 1991-12-03 Honeywell Inc. Method of analyzing and predicting both airplane and engine performance characteristics
US5072894A (en) * 1989-10-02 1991-12-17 Rockwell International Corporation Apparatus and method for increasing the angle of attack operating range of an aircraft
US5275358A (en) * 1991-08-02 1994-01-04 The Boeing Company Wing/winglet configurations and methods for aircraft
US5348253A (en) * 1993-02-01 1994-09-20 Gratzer Louis B Blended winglet
US5478031A (en) * 1993-09-29 1995-12-26 Rockwell International Corporation Airspeed control system which utilizes pitch hold command when pilot throttle changes oppose elevator control
JP3645038B2 (ja) * 1996-07-05 2005-05-11 富士重工業株式会社 航空機の飛行制御装置
US5988563A (en) * 1997-12-30 1999-11-23 Mcdonnell Douglas Corporation Articulating winglets
DE19926832B4 (de) * 1999-06-12 2005-09-15 Airbus Deutschland Gmbh Unterschallflugzeug vorzugsweise mit gepfeilten Tragflügeln
FR2802656B1 (fr) * 1999-12-16 2002-02-15 Eurocopter France Systeme de commande de vol pour aeronef a voilure tournante, notamment pour helicoptere
US6484968B2 (en) * 2000-12-11 2002-11-26 Fort F. Felker Aircraft with elliptical winglets

Also Published As

Publication number Publication date
US6827314B2 (en) 2004-12-07
DE60325141D1 (de) 2009-01-22
CA2427357A1 (fr) 2003-12-27
FR2841532A1 (fr) 2004-01-02
EP1375342B1 (de) 2008-12-10
FR2841532B1 (fr) 2004-12-17
US20040000619A1 (en) 2004-01-01
CA2427357C (fr) 2012-01-10
EP1375342A1 (de) 2004-01-02

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