ATE354517T1 - Flugzeug mit elliptischen winglets - Google Patents

Flugzeug mit elliptischen winglets

Info

Publication number
ATE354517T1
ATE354517T1 AT01995382T AT01995382T ATE354517T1 AT E354517 T1 ATE354517 T1 AT E354517T1 AT 01995382 T AT01995382 T AT 01995382T AT 01995382 T AT01995382 T AT 01995382T AT E354517 T1 ATE354517 T1 AT E354517T1
Authority
AT
Austria
Prior art keywords
winglets
wings
airplane
intersection
elliptical
Prior art date
Application number
AT01995382T
Other languages
English (en)
Inventor
Fort F Felker
Original Assignee
Fort F Felker
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=24951310&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=ATE354517(T1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Fort F Felker filed Critical Fort F Felker
Application granted granted Critical
Publication of ATE354517T1 publication Critical patent/ATE354517T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B64C23/065—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices at the wing tips
    • B64C23/069—Influencing 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
    • 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
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Toys (AREA)
  • Registering, Tensioning, Guiding Webs, And Rollers Therefor (AREA)
  • Magnetic Resonance Imaging Apparatus (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Mechanical Coupling Of Light Guides (AREA)
  • Manufacturing Cores, Coils, And Magnets (AREA)
  • Physical Deposition Of Substances That Are Components Of Semiconductor Devices (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
AT01995382T 2000-12-11 2001-12-05 Flugzeug mit elliptischen winglets ATE354517T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US09/734,347 US6484968B2 (en) 2000-12-11 2000-12-11 Aircraft with elliptical winglets

Publications (1)

Publication Number Publication Date
ATE354517T1 true ATE354517T1 (de) 2007-03-15

Family

ID=24951310

Family Applications (1)

Application Number Title Priority Date Filing Date
AT01995382T ATE354517T1 (de) 2000-12-11 2001-12-05 Flugzeug mit elliptischen winglets

Country Status (7)

Country Link
US (1) US6484968B2 (de)
EP (1) EP1349778B1 (de)
AT (1) ATE354517T1 (de)
AU (1) AU2002225941A1 (de)
CA (1) CA2431488C (de)
DE (1) DE60126824T2 (de)
WO (1) WO2002047979A2 (de)

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DE10117721B4 (de) * 2001-04-09 2007-09-27 Gerd Heller Flügelspitzenverlängerung für einen Flügel
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FR2841532B1 (fr) * 2002-06-27 2004-12-17 Airbus France Avion a controle actif du vrillage de ses ailes
DK1583904T3 (da) * 2003-01-02 2013-12-16 Wobben Properties Gmbh Vindmøllerotorblad med reduceret akustisk emission
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
US6886778B2 (en) * 2003-06-30 2005-05-03 The Boeing Company Efficient wing tip devices and methods for incorporating such devices into existing wing designs
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US8544800B2 (en) * 2005-07-21 2013-10-01 The Boeing Company Integrated wingtip extensions for jet transport aircraft and other types of aircraft
GB0518755D0 (en) 2005-09-14 2005-10-19 Airbus Uk Ltd Wing tip device
FR2894558A1 (fr) * 2005-12-12 2007-06-15 Dassault Avions Aile a ailette d'extremite de voilure et aeronef comportant une telle aile
US7644892B1 (en) * 2006-07-06 2010-01-12 Alford Jr Lionel D Blended winglet
DE102006055090A1 (de) 2006-11-21 2008-05-29 Airbus Deutschland Gmbh Flügelendform für einen Flügel, insbesondere von Luftfahrzeugen
US7744038B2 (en) * 2007-06-15 2010-06-29 The Boeing Company Controllable winglets
GB0711942D0 (en) 2007-06-21 2007-08-01 Airbus Uk Ltd Winglet
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
US8128035B2 (en) * 2008-04-15 2012-03-06 The Boeing Company Winglets with recessed surfaces, and associated systems and methods
US9302766B2 (en) 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
DK2905222T3 (da) * 2008-06-20 2020-01-02 Aviation Partners Inc Krum vingespids
DE102009019542A1 (de) * 2009-04-30 2010-11-11 Airbus Deutschland Gmbh Nicht-planares Flügelendstück für Tragflügel von Flugzeugen sowie Tragflügel mit einem solchen Flügelendstück
CA2761317A1 (en) * 2009-05-05 2010-11-11 Aerostar Aircraft Corporation Aircraft winglet design having a compound curve profile
US20110127383A1 (en) 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet
US9162755B2 (en) 2009-12-01 2015-10-20 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
CN106218862B (zh) 2010-04-12 2018-12-11 空中客车运作有限责任公司 一种配置航空器的翼用于具体应用的方法以及其翼结构
GB201011843D0 (en) 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
US8382041B1 (en) 2010-08-04 2013-02-26 The United States Of America As Represented By The Secretary Of The Air Force Rakelet
DE102012103704A1 (de) 2011-04-30 2012-10-31 General Electric Co. Winglet für einen Rotorflügel einer Windkraftanlage
ES2783984T3 (es) 2011-06-09 2020-09-21 Aviation Partners Inc Espiroide dividido
EP2562084A1 (de) * 2011-08-25 2013-02-27 KPS Limited Drachen für ein System zur Gewinnung von Energie aus Wind
GB201115026D0 (en) * 2011-08-31 2011-10-12 Airbus Operations Ltd Aircraft lighting device
CN102358417B (zh) * 2011-09-02 2013-09-18 北京航空航天大学 一种民用客机的机翼环形翼梢小翼
GB201201609D0 (en) * 2012-01-31 2012-03-14 Airbus Operations Ltd A wing fin of an aircraft
US9103325B2 (en) 2012-03-20 2015-08-11 General Electric Company Winglet for a wind turbine rotor blade
US8936219B2 (en) 2012-03-30 2015-01-20 The Boeing Company Performance-enhancing winglet system and method
ES2747639T3 (es) 2013-02-05 2020-03-11 Tamarack Aerospace Group Inc Control de carga periódica de dispositivo controlable de modificación de flujo de aire
KR101325593B1 (ko) 2013-05-03 2013-11-06 국방과학연구소 부분 가동타에 수직끝판이 부착된 원통형 수중운동체
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
JP6758183B2 (ja) * 2013-12-05 2020-09-23 タマラック エアロスペース グループ インコーポレイテッド ウィングチップデバイス
GB2522245A (en) * 2014-01-20 2015-07-22 Airbus Operations Ltd A curved winglet
US9511850B2 (en) 2014-04-12 2016-12-06 The Boeing Company Wing tip device for an aircraft wing
US9637225B1 (en) 2015-11-16 2017-05-02 Textron Innovations Inc. Aircraft winglet
US11148788B2 (en) 2016-02-12 2021-10-19 Textron Innovation, Inc. Curved wingtip for aircraft
EP3269635A1 (de) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Flugzeugflügel
GB2559771A (en) * 2017-02-17 2018-08-22 Airbus Operations Ltd A rib arrangement in a wing tip device
GB2559968A (en) 2017-02-22 2018-08-29 Airbus Operations Ltd A winglet and method of designing a winglet
ES2905192T3 (es) * 2018-01-15 2022-04-07 The Aircraft Performance Company Gmbh Ala de avión
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
GB2628523A (en) * 2022-11-16 2024-10-02 Airbus Operations Ltd Aircraft wing
WO2024124085A1 (en) 2022-12-08 2024-06-13 Alliance For Sustainable Energy, Llc Negative tip vortices blade

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US4190219A (en) 1977-05-17 1980-02-26 Lockheed Corporation Vortex diffuser
US4205810A (en) 1977-12-19 1980-06-03 The Boeing Company Minimum drag wing configuration for aircraft operating at transonic speeds
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US4240597A (en) * 1978-08-28 1980-12-23 Gates Learjet Corporation Wing with improved leading edge for aircraft
US4382569A (en) * 1979-12-26 1983-05-10 Grumman Aerospace Corporation Wing tip flow control
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US5275358A (en) * 1991-08-02 1994-01-04 The Boeing Company Wing/winglet configurations and methods for aircraft
JPH06144384A (ja) * 1992-11-12 1994-05-24 Mitsubishi Heavy Ind Ltd 航空機のロール制御装置
US5348253A (en) * 1993-02-01 1994-09-20 Gratzer Louis B Blended winglet
DE29621652U1 (de) * 1996-12-13 1998-04-16 Zepf Hans Peter Aerodynamische Auslegung für Flugzeuge hoher Streckung mit positiver Tragflügelpfeilung
US5961068A (en) * 1997-10-23 1999-10-05 Northrop Grumman Corporation Aerodynamic control effector

Also Published As

Publication number Publication date
DE60126824T2 (de) 2007-10-31
WO2002047979A2 (en) 2002-06-20
CA2431488A1 (en) 2002-06-20
US20020092947A1 (en) 2002-07-18
AU2002225941A1 (en) 2002-06-24
EP1349778A2 (de) 2003-10-08
CA2431488C (en) 2011-04-19
DE60126824D1 (de) 2007-04-05
EP1349778A4 (de) 2006-06-07
EP1349778B1 (de) 2007-02-21
WO2002047979A3 (en) 2002-12-12
US6484968B2 (en) 2002-11-26

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