ES2533402T3 - Aleta activa - Google Patents

Aleta activa Download PDF

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Publication number
ES2533402T3
ES2533402T3 ES10821429.7T ES10821429T ES2533402T3 ES 2533402 T3 ES2533402 T3 ES 2533402T3 ES 10821429 T ES10821429 T ES 10821429T ES 2533402 T3 ES2533402 T3 ES 2533402T3
Authority
ES
Spain
Prior art keywords
aircraft
wing
fin
air flow
flap
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.)
Active
Application number
ES10821429.7T
Other languages
English (en)
Spanish (es)
Inventor
Nicholas R. Guida
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.)
Tamarack Aerospace Group Inc
Original Assignee
Tamarack Aerospace Group Inc
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 Tamarack Aerospace Group Inc filed Critical Tamarack Aerospace Group Inc
Application granted granted Critical
Publication of ES2533402T3 publication Critical patent/ES2533402T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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
    • B64C23/076Influencing 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 comprising one or more separate moveable members thereon affecting the vortices, e.g. flaps
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C13/00Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B64C13/02Initiating means
    • B64C13/16Initiating means actuated automatically, e.g. responsive to gust detectors
    • 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
    • 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)
  • Automation & Control Theory (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
ES10821429.7T 2009-12-01 2010-11-12 Aleta activa Active ES2533402T3 (es)

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US797742 2004-03-10
US26553409P 2009-12-01 2009-12-01
US265534P 2009-12-01
US12/797,742 US20110127383A1 (en) 2009-12-01 2010-06-10 Active winglet
US890557 2010-09-24
US12/890,557 US7900877B1 (en) 2009-12-01 2010-09-24 Active winglet
PCT/US2010/056586 WO2011068659A2 (en) 2009-12-01 2010-11-12 Active winglet

Publications (1)

Publication Number Publication Date
ES2533402T3 true ES2533402T3 (es) 2015-04-09

Family

ID=43639207

Family Applications (1)

Application Number Title Priority Date Filing Date
ES10821429.7T Active ES2533402T3 (es) 2009-12-01 2010-11-12 Aleta activa

Country Status (6)

Country Link
US (7) US20110127383A1 (enExample)
EP (1) EP2346734B1 (enExample)
JP (3) JP5542955B2 (enExample)
AU (1) AU2010326260B2 (enExample)
ES (1) ES2533402T3 (enExample)
WO (1) WO2011068659A2 (enExample)

Families Citing this family (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8544800B2 (en) * 2005-07-21 2013-10-01 The Boeing Company Integrated wingtip extensions for jet transport aircraft and other types of aircraft
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
ES3040742T3 (en) * 2008-06-20 2025-11-04 Aviation Partners Inc Curved wing tip
DE102009019542A1 (de) * 2009-04-30 2010-11-11 Airbus Deutschland Gmbh Nicht-planares Flügelendstück für Tragflügel von Flugzeugen sowie Tragflügel mit einem solchen Flügelendstück
US9162755B2 (en) * 2009-12-01 2015-10-20 Tamarack Aerospace Group, Inc. Multiple controllable airflow modification devices
US20110127383A1 (en) * 2009-12-01 2011-06-02 Guida Associates Consulting, Inc. Active winglet
GB201011843D0 (en) * 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
FR2970699B1 (fr) * 2011-01-25 2014-11-28 Lisa Airplanes Avion motorise a structure mixte hydrodynamique et aerodynamique pour le decollage et l'atterrissage sur l'eau, le sol ou la neige
EP2718183B1 (en) * 2011-06-09 2018-02-28 Aviation Partners, Inc. The split spiroid
EP2551737B1 (en) * 2011-07-28 2015-04-29 Airbus Defence and Space GmbH Method and apparatus for minimizing dynamic structural loads of an aircraft
DE102011116841B4 (de) * 2011-10-25 2017-10-26 Airbus Defence and Space GmbH Höhenluftfahrzeug, Luftfahrzeugverband und Verfahren zum Betreiben eines Luftfahrzeugverbands
GB201120862D0 (en) * 2011-12-05 2012-01-18 Airbus Operations Ltd A wingtip fin of an aircraft
ES2964283T3 (es) * 2012-04-03 2024-04-05 Tamarack Aerospace Group Inc Dispositivos múltiples de modificación de flujo de aire controlables
US8788122B1 (en) 2012-08-24 2014-07-22 The Boeing Company Wing load alleviation methods and apparatus
EP3594115B1 (en) * 2013-02-05 2023-08-23 Tamarack Aerospace Group, Inc. Controllable airflow modification device periodic load control
US9845159B2 (en) * 2013-03-07 2017-12-19 United Technologies Corporation Conjoined reverse core flow engine arrangement
WO2015050617A2 (en) * 2013-07-15 2015-04-09 Design Intelligence Incorporated, LLC Unmanned aerial vehicle (uav) with inter-connecting wing sections
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
EP3077281A4 (en) 2013-12-05 2017-07-26 Tamarack Aerospace Group, Inc. Wingtip device
USD732657S1 (en) * 2014-02-27 2015-06-23 Delta T Corporation Winglet
GB2535488A (en) * 2015-02-17 2016-08-24 Airbus Operations Ltd An arrangement for effecting movement of a wing tip device between a flight configuration and a ground configuration
DE102015008974A1 (de) * 2015-07-10 2017-01-12 Liebherr-Aerospace Lindenberg Gmbh Winglet mit steuerbarem Luftwiderstandselement
CN106802205B (zh) * 2015-11-26 2019-08-02 中国飞行试验研究院 一种消除剖面内载荷影响的飞行载荷测量方法
GB2551554B (en) * 2016-06-22 2018-08-15 Airbus Operations Ltd Methods of configuring a wing tip device on an aircraft
EP3269635A1 (en) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Airplane wing
US10710702B2 (en) * 2016-08-12 2020-07-14 Aviation Partners, Inc. Shape adaptive airfoil
RU2637149C1 (ru) * 2016-11-02 2017-11-30 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Спироидный винглет
US10745107B1 (en) * 2017-05-08 2020-08-18 Government Of The United States, As Represented By The Secretary Of The Air Force Rapid flap deflection for high lift transients
USD858421S1 (en) * 2017-09-28 2019-09-03 Tesla, Inc. Winglet
EP3492374A3 (en) * 2017-11-29 2019-09-04 Airbus Operations Limited Retrofit flight control surface
GB201719806D0 (en) * 2017-11-29 2018-01-10 Airbus Operations Ltd Retrofit flight control surface
ES2905192T3 (es) * 2018-01-15 2022-04-07 The Aircraft Performance Company Gmbh Ala de avión
GB2576929A (en) * 2018-09-07 2020-03-11 Airbus Operations Ltd A wing tip device
GB2580930A (en) * 2019-01-30 2020-08-05 Airbus Operations Ltd Fairing for folding wing tip
WO2022087607A1 (en) * 2020-10-20 2022-04-28 Roland Industries, Inc. Mono-winged drone
CN113665787B (zh) * 2021-09-24 2023-11-24 肇庆市海特复合材料技术研究院 一种复合材料无人机机翼结构
GB2615311A (en) * 2022-01-31 2023-08-09 Airbus Operations Ltd Aircraft wing with movable wing tip device
GB2616252A (en) * 2022-01-31 2023-09-06 Airbus Operations Ltd Aircraft with movable wing tip device
US11897601B2 (en) 2022-02-16 2024-02-13 Jetzero, Inc. Aircraft and methods of use for aerodynamic control with winglet surfaces
GB2628523B (en) * 2022-11-16 2025-07-09 Airbus Operations Ltd Aircraft wing
USD1073579S1 (en) 2023-09-08 2025-05-06 Textron Innovations, Inc. Blended falx winglet
US12428138B2 (en) 2023-09-08 2025-09-30 Textron Innovations Inc. Blended falx winglet
CN117208195A (zh) * 2023-10-31 2023-12-12 南京航空航天大学 飞行器尾翼伸缩机构、单体飞行器和组合式飞行器

Family Cites Families (72)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US692304A (en) * 1901-01-28 1902-02-04 John B Kenison Chimney.
US2074201A (en) 1934-01-29 1937-03-16 Avions Kellner Bechereau Soc Airfoil used in aeronautics
US2418301A (en) * 1942-07-24 1947-04-01 Miles Aircraft Ltd Aircraft supporting surface
US2576981A (en) 1949-02-08 1951-12-04 Vogt Richard Twisted wing tip fin for airplanes
US3218005A (en) * 1961-12-06 1965-11-16 Calderon Alberto Alvarez High lift system for high speed aircraft
DE2149956C3 (de) 1971-10-07 1974-03-28 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Hochauftriebsflügel
US3845918A (en) 1972-12-07 1974-11-05 Rochester Applied Science Ass Vortex dissipator
US4017041A (en) 1976-01-12 1977-04-12 Nelson Wilbur C Airfoil tip vortex control
US4172574A (en) 1976-06-16 1979-10-30 National Research Development Corporation Fluid stream deflecting members for aircraft bodies or the like
US4190219A (en) 1977-05-17 1980-02-26 Lockheed Corporation Vortex diffuser
DE2756107C2 (de) * 1977-12-16 1980-02-28 Messerschmitt-Boelkow-Blohm Gmbh, 8000 Muenchen Hochwirksames Seitenleitwerk mit variabler Flügelgeometrie
US4205810A (en) 1977-12-19 1980-06-03 The Boeing Company Minimum drag wing configuration for aircraft operating at transonic speeds
US4245804B1 (en) 1977-12-19 1993-12-14 K. Ishimitsu Kichio Minimum drag wing configuration for aircraft operating at transonic speeds
US4247063A (en) 1978-08-07 1981-01-27 Lockheed Corporation Flight control mechanism for airplanes
US4240597A (en) 1978-08-28 1980-12-23 Gates Learjet Corporation Wing with improved leading edge for aircraft
US4365773A (en) 1979-04-11 1982-12-28 Julian Wolkovitch Joined wing aircraft
US4382569A (en) * 1979-12-26 1983-05-10 Grumman Aerospace Corporation Wing tip flow control
US4725020A (en) 1980-12-09 1988-02-16 The Boeing Company Control system incorporating structural feedback
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
FR2540824A1 (fr) 1983-02-10 1984-08-17 Daude Martine Avion muni d'ailettes marginales mobiles synchronisees
GB8314656D0 (en) * 1983-05-26 1983-06-29 Secr Defence Aircraft control
US4545552A (en) * 1983-06-20 1985-10-08 Welles Stanley W Airframe design
US4674709A (en) * 1983-06-20 1987-06-23 Welles Stanley W Airframe design
US4671473A (en) * 1984-11-08 1987-06-09 Goodson Kenneth W Airfoil
NL8500950A (nl) * 1985-03-29 1986-10-16 Fokker Bv Rolroer van een vliegtuigvleugel.
DE3634250C1 (de) * 1986-10-08 1988-03-03 Dornier Gmbh Fluggeraetesteuerung
JPH01254491A (ja) 1988-04-04 1989-10-11 Mitsubishi Heavy Ind Ltd 前縁フラップ装置
FR2636592B1 (fr) * 1988-09-20 1990-11-23 Aerospatiale Surface aerodynamique orientable pour un aeronef
US5039032A (en) 1988-11-07 1991-08-13 The Boeing Company High taper wing tip extension
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
JPH06502364A (ja) 1990-07-25 1994-03-17 サドレアー・ヴィートール・エアクラフト・カンパニー・プロプライエタリー・リミテッド Vtol航空機のための推進ユニット
US5156358A (en) 1991-04-11 1992-10-20 Northrop Corporation Aircraft outboard control
US5348253A (en) 1993-02-01 1994-09-20 Gratzer Louis B Blended winglet
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
DE69430198T2 (de) * 1994-12-16 2003-07-10 Aldo Frediani Grossraumflugzeug
IL119392A (en) * 1996-10-09 2004-01-04 Rafael Armament Dev Authority Device for reducing the drag at the base of a body
US6095459A (en) * 1997-06-16 2000-08-01 Codina; George Method and apparatus for countering asymmetrical aerodynamic process subjected onto multi engine aircraft
US5988563A (en) * 1997-12-30 1999-11-23 Mcdonnell Douglas Corporation Articulating winglets
DE19819341C2 (de) * 1998-04-30 2000-06-15 Daimler Chrysler Aerospace Verfahren zur Reduktion von an einem Flugzeug auftretenden Böenlasten unterhalb der Reiseflughöhe
US6227487B1 (en) * 1999-05-05 2001-05-08 Northrop Grumman Corporation Augmented wing tip drag flap
DE19926832B4 (de) 1999-06-12 2005-09-15 Airbus Deutschland Gmbh Unterschallflugzeug vorzugsweise mit gepfeilten Tragflügeln
DE19950403C2 (de) * 1999-10-20 2002-02-07 Deutsch Zentr Luft & Raumfahrt Flugzeug mit Mitteln zum Reduzieren der Wirbelstärke des Flügelhauptwirbelpaars
US6394397B1 (en) 2000-12-06 2002-05-28 The Boeing Company Lifting surface with active variable tip member and method for influencing lifting surface behavior therewith
US6484968B2 (en) * 2000-12-11 2002-11-26 Fort F. Felker Aircraft with elliptical winglets
GB0115130D0 (en) 2001-06-21 2001-08-15 Bae Systems Plc A winglet
US6666666B1 (en) 2002-05-28 2003-12-23 Denis Gilbert Multi-chamber positive displacement fluid device
US6766981B2 (en) 2002-10-25 2004-07-27 Northrop Grumman Corporation Control system for alleviating a gust load on an aircraft wing
US6923404B1 (en) 2003-01-10 2005-08-02 Zona Technology, Inc. Apparatus and methods for variable sweep body conformal wing with application to projectiles, missiles, and unmanned air vehicles
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
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
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
US8544800B2 (en) * 2005-07-21 2013-10-01 The Boeing Company Integrated wingtip extensions for jet transport aircraft and other types of aircraft
US20070114327A1 (en) * 2005-11-18 2007-05-24 The Boeing Company Wing load alleviation apparatus and method
US7922115B2 (en) * 2006-04-21 2011-04-12 Colgren Richard D Modular unmanned air-vehicle
US8387922B2 (en) * 2006-09-15 2013-03-05 Airbus Operations Gmbh Aerodynamic element and wing with aerodynamic element, actuator-activation module, computer, computer program and method of influencing wake eddies
US7744038B2 (en) * 2007-06-15 2010-06-29 The Boeing Company Controllable winglets
US8083185B2 (en) * 2007-11-07 2011-12-27 The Boeing Company Aircraft wing tip having a variable incidence angle
FR2929241B1 (fr) * 2008-03-31 2010-06-04 Airbus France Procede et dispositif de reduction du tremblement d'un avion.
US8128035B2 (en) * 2008-04-15 2012-03-06 The Boeing Company Winglets with recessed surfaces, and associated systems and methods
US8024079B2 (en) * 2008-05-20 2011-09-20 The Boeing Company Wing-body load alleviation for aircraft
US20100163669A1 (en) * 2008-12-29 2010-07-01 Im Sunstar Super aircraft structrue
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
US8651431B1 (en) 2011-08-09 2014-02-18 The Boeing Company Aircraft with movable winglets and method of control
ES2964283T3 (es) 2012-04-03 2024-04-05 Tamarack Aerospace Group Inc Dispositivos múltiples de modificación de flujo de aire controlables
EP3594115B1 (en) 2013-02-05 2023-08-23 Tamarack Aerospace Group, Inc. Controllable airflow modification device periodic load control
US9469391B1 (en) * 2013-04-26 2016-10-18 The Boeing Company Adaptive wing for an aircraft
US10562613B2 (en) * 2013-12-04 2020-02-18 Tamarack Aerospace Group, Inc. Adjustable lift modification wingtip
US10710702B2 (en) * 2016-08-12 2020-07-14 Aviation Partners, Inc. Shape adaptive airfoil

Also Published As

Publication number Publication date
EP2346734A4 (en) 2013-01-02
US20180029696A1 (en) 2018-02-01
US11884383B2 (en) 2024-01-30
JP5542955B2 (ja) 2014-07-09
US20110127383A1 (en) 2011-06-02
JP2013512153A (ja) 2013-04-11
WO2011068659A2 (en) 2011-06-09
EP2346734B1 (en) 2015-01-07
US20110186689A1 (en) 2011-08-04
EP2346734A1 (en) 2011-07-27
US9764825B2 (en) 2017-09-19
US8684315B2 (en) 2014-04-01
US20150008291A1 (en) 2015-01-08
US20200283130A1 (en) 2020-09-10
AU2010326260A1 (en) 2012-06-14
AU2010326260B2 (en) 2012-11-08
WO2011068659A3 (en) 2011-10-20
US7900877B1 (en) 2011-03-08
JP6854667B2 (ja) 2021-04-07
US20240409204A1 (en) 2024-12-12
US10486797B2 (en) 2019-11-26
JP2014193717A (ja) 2014-10-09
JP2017109742A (ja) 2017-06-22

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