DE60325141D1 - Flugzeug mit aktiver Verwindungskontrolle seiner Tragflächen - Google Patents

Flugzeug mit aktiver Verwindungskontrolle seiner Tragflächen

Info

Publication number
DE60325141D1
DE60325141D1 DE60325141T DE60325141T DE60325141D1 DE 60325141 D1 DE60325141 D1 DE 60325141D1 DE 60325141 T DE60325141 T DE 60325141T DE 60325141 T DE60325141 T DE 60325141T DE 60325141 D1 DE60325141 D1 DE 60325141D1
Authority
DE
Germany
Prior art keywords
plane
wing
airplane
wings
additional
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
DE60325141T
Other languages
English (en)
Inventor
Bernard Barriety
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Operations SAS filed Critical Airbus Operations SAS
Application granted granted Critical
Publication of DE60325141D1 publication Critical patent/DE60325141D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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)
  • Heterocyclic Carbon Compounds Containing A Hetero Ring Having Oxygen Or Sulfur (AREA)
  • Pharmaceuticals Containing Other Organic And Inorganic Compounds (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Control Of Turbines (AREA)
DE60325141T 2002-06-27 2003-05-28 Flugzeug mit aktiver Verwindungskontrolle seiner Tragflächen Expired - Lifetime DE60325141D1 (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
DE60325141D1 true DE60325141D1 (de) 2009-01-22

Family

ID=29717115

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60325141T Expired - Lifetime DE60325141D1 (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 (65)

* 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
DE60311659T2 (de) * 2003-11-11 2007-11-22 Airbus Uk Ltd., Filton Aerodynamisch wirksame Flügelspitzenvorrichtung
US7475848B2 (en) * 2003-11-11 2009-01-13 Morgenstern John M Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
JP2008540240A (ja) 2005-05-19 2008-11-20 エアバス・ドイチュラント・ゲーエムベーハー 横方向の負荷を低減し、横方向及び縦方向の複合負荷を低減するとともに、移動手段の性能を高めるための可変翼の構想
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
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
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
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
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
CN102762453B (zh) * 2009-12-10 2015-03-25 约翰内斯堡威特沃特斯兰德大学 减少飞行尾迹涡流的方法和在其中使用的飞行器翼尖装置
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
DK3372493T3 (da) * 2011-06-09 2019-12-09 Aviation Partners Inc Den delt-formet blandede winglet
US9290260B2 (en) 2011-10-01 2016-03-22 The Boeing Company Wing fold controller
US9499252B2 (en) 2011-10-01 2016-11-22 The Boeing Company Wing fold controller
US10538307B2 (en) 2011-10-01 2020-01-21 The Boeing Company Hinged raked wing tip
US9296469B2 (en) 2011-10-01 2016-03-29 The Boeing Company Horizontal folding wingtip
US9211946B2 (en) 2011-10-01 2015-12-15 The Boeing Company Wing fold system with latch pins through multiple mating lugs
US8936219B2 (en) 2012-03-30 2015-01-20 The Boeing Company Performance-enhancing winglet system and method
US9481446B2 (en) 2012-10-30 2016-11-01 The Boeing Company System for latching and locking a foldable airfoil
EP2727826B1 (de) * 2012-10-30 2019-06-26 The Boeing Company Schwenkbarer Winglet
US9469392B2 (en) 2012-10-30 2016-10-18 The Boeing Company Wing fold system rotating latch
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
CN106574603B (zh) * 2014-08-05 2019-12-24 瑞安·丘奇 具有适于横穿流体环境的刚性小翼的结构
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
US11370526B2 (en) * 2018-05-31 2022-06-28 Airbus Operations Gmbh Latching device for a wing arrangement for an aircraft
US11319054B2 (en) * 2018-05-31 2022-05-03 Airbus Operations Gmbh 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

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
EP1375342A1 (de) 2004-01-02
CA2427357C (fr) 2012-01-10
EP1375342B1 (de) 2008-12-10
US6827314B2 (en) 2004-12-07
FR2841532A1 (fr) 2004-01-02
CA2427357A1 (fr) 2003-12-27
ATE416971T1 (de) 2008-12-15
US20040000619A1 (en) 2004-01-01
FR2841532B1 (fr) 2004-12-17

Similar Documents

Publication Publication Date Title
DE60325141D1 (de) Flugzeug mit aktiver Verwindungskontrolle seiner Tragflächen
AU2003299548A1 (en) Slotted aircraft wing
WO2009029796A3 (en) Oblique blended wing body aircraft
JP2009501678A5 (de)
RU2017105216A (ru) Раздвоенный сопряженный винглет
US20170073062A1 (en) Variable Geometry Wingtip
US4132375A (en) Vortex-lift roll-control device
CN210235305U (zh) 一种可变机翼外翼后掠角和可倾斜小翼的飞翼式飞机
US20050116116A1 (en) Wing employing leading edge flaps and winglets to achieve improved aerodynamic performance
US7004428B2 (en) Lift and twist control using trailing edge control surfaces on supersonic laminar flow wings
US11685519B2 (en) Wing tips and wing tip construction and design methods
CN203558201U (zh) 一种飞机机翼
Moore et al. X-29 forward swept wing aerodynamic overview
US2667351A (en) Nonlifting towed target glider
US6378803B1 (en) Aircraft lift arrangement
US5249762A (en) Strakes for landing speed reduction
CN109677587B (zh) 一种可兼顾高低速飞行的斜置翼飞机的控制方法
CA2503270A1 (en) Laminar flow wing for transonic cruise
CN204802070U (zh) 一种机翼可变形飞行器
CN209454975U (zh) 一种飞行器翼面折叠机构
CN109703758B (zh) 双向飞翼飞行器气动外形和设计方法
CA2290028A1 (en) Spoiler for wings
CN204637576U (zh) 一种抛撒物品的遥控飞机
US8128031B2 (en) Spar for sailwings
RU2086467C1 (ru) Крыло самолета

Legal Events

Date Code Title Description
8364 No opposition during term of opposition
R082 Change of representative

Ref document number: 1375342

Country of ref document: EP

Representative=s name: MEISSNER & MEISSNER, 14199 BERLIN, DE