JP2008540240A5 - - Google Patents

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Publication number
JP2008540240A5
JP2008540240A5 JP2008511653A JP2008511653A JP2008540240A5 JP 2008540240 A5 JP2008540240 A5 JP 2008540240A5 JP 2008511653 A JP2008511653 A JP 2008511653A JP 2008511653 A JP2008511653 A JP 2008511653A JP 2008540240 A5 JP2008540240 A5 JP 2008540240A5
Authority
JP
Japan
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.)
Pending
Application number
JP2008511653A
Other versions
JP2008540240A (ja
Filing date
Publication date
Priority claimed from DE102005028688A external-priority patent/DE102005028688A1/de
Application filed filed Critical
Priority claimed from PCT/EP2006/004774 external-priority patent/WO2006122826A1/en
Publication of JP2008540240A publication Critical patent/JP2008540240A/ja
Publication of JP2008540240A5 publication Critical patent/JP2008540240A5/ja
Pending legal-status Critical Current

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JP2008511653A 2005-05-19 2006-05-19 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 Pending JP2008540240A (ja)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US68273605P 2005-05-19 2005-05-19
DE102005023117 2005-05-19
DE102005028688A DE102005028688A1 (de) 2005-05-19 2005-06-21 Konzept eines variablen Winglets zur lateralen Lastenreduktion zur kombinierten lateralen und vertikalen Lastenreduktion und zur Performanceverbesserung von Fortbewegungsmitteln
PCT/EP2006/004774 WO2006122826A1 (en) 2005-05-19 2006-05-19 Concept of a variable winglet for lateral load reduction for combined lateral and vertical load reduction, and for improving the performance of means of locomotion

Publications (2)

Publication Number Publication Date
JP2008540240A JP2008540240A (ja) 2008-11-20
JP2008540240A5 true JP2008540240A5 (ja) 2009-07-02

Family

ID=36691824

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2008511653A Pending JP2008540240A (ja) 2005-05-19 2006-05-19 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

Country Status (5)

Country Link
EP (1) EP1883577B8 (ja)
JP (1) JP2008540240A (ja)
CA (1) CA2602948A1 (ja)
DE (1) DE602006012036D1 (ja)
WO (1) WO2006122826A1 (ja)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8083185B2 (en) * 2007-11-07 2011-12-27 The Boeing Company Aircraft wing tip having a variable incidence angle
US9302766B2 (en) 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
DK2303685T3 (en) 2008-06-20 2016-01-18 Aviat Partners Inc KRUM wingtip
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
JP5602060B2 (ja) * 2011-02-28 2014-10-08 三菱重工業株式会社 風車翼およびこれを備えた風力発電装置ならびに風車翼の設計方法
ES2676415T3 (es) 2011-06-09 2018-07-19 Aviation Partners, Inc. Espiroide dividido
US10562613B2 (en) 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
WO2015085226A1 (en) * 2013-12-05 2015-06-11 Tamarack Aerospace Group, Inc. Wingtip device

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2521520A1 (fr) * 1982-02-15 1983-08-19 Daude Martine Ailettes marginales a angles d'attaque variables
US4455004A (en) * 1982-09-07 1984-06-19 Lockheed Corporation Flight control device for airplanes
DE3242584A1 (de) * 1982-11-18 1984-05-24 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Anordnung von zusatzflaechen an den spitzen eines tragfluegels
GB9321510D0 (en) * 1993-10-19 1993-12-22 Short Brothers Plc Aircraft flight control system
JP2622670B2 (ja) * 1994-10-05 1997-06-18 川崎重工業株式会社 超音速航空機の主翼
US5988563A (en) 1997-12-30 1999-11-23 Mcdonnell Douglas Corporation Articulating winglets
FR2841532B1 (fr) 2002-06-27 2004-12-17 Airbus France Avion a controle actif du vrillage de ses ailes
DE10313290B4 (de) * 2003-03-25 2005-12-29 Johannes Schweiger Strömungsmechanisch wirksame Fläche eines sich in einem Fluid bewegenden Geräts, insbesondere eines Fluggeräts, insbesondere Tragfläche oder Ruderfläche eines Fluggeräts
ES2280701T3 (es) * 2003-11-11 2007-09-16 Airbus Uk Limited Dispositivo de extremo de ala.

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