BRPI0515409A - dispositivo de ponta, superfìce de sustentação aerodinámica, aeronave, e, helicóptero - Google Patents

dispositivo de ponta, superfìce de sustentação aerodinámica, aeronave, e, helicóptero

Info

Publication number
BRPI0515409A
BRPI0515409A BRPI0515409-0A BRPI0515409A BRPI0515409A BR PI0515409 A BRPI0515409 A BR PI0515409A BR PI0515409 A BRPI0515409 A BR PI0515409A BR PI0515409 A BRPI0515409 A BR PI0515409A
Authority
BR
Brazil
Prior art keywords
aircraft
helicopter
leading edge
end device
lifting surface
Prior art date
Application number
BRPI0515409-0A
Other languages
English (en)
Inventor
Kevin Christopher Hackett
Clive Robert Pyne
Original Assignee
Qinetiq Ltd
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 Qinetiq Ltd filed Critical Qinetiq Ltd
Publication of BRPI0515409A publication Critical patent/BRPI0515409A/pt

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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C27/00—Rotorcraft; Rotors peculiar thereto
    • B64C27/32—Rotors
    • B64C27/46—Blades
    • B64C27/463—Blade tips
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • 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)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Automatic Assembly (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Saccharide Compounds (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Bridges Or Land Bridges (AREA)

Abstract

DISPOSITIVO DE PONTA, SUPERFìCIE DE SUSTENTAçãO AERODINáMICA, AERONAVE, E, HELICóPTERO. Um dispositivo de ponta (10) para atuar como uma continuação exterior de uma asa de aeronave (2) ou outra superfície de sustentação aerodinâmica tem um ângulo de inclinação descendente, uma borda de avanço (3, 8,11) recuada em relação à borda de avanço da superfície de sustentação interna, e uma corda que se reduz na direção exterior do dispositivo. Um equilíbrio favorável entre redução de arraste induzido e momento de encurvamento na raiz de asa pode, deste modo, ser atingido. Preferivelmente, o dispositivo também tem uma porção inclinada para cima em suas extremidade de raiz de modo que a inclinação para baixo começa a partir de um local pela envergadura, relativamente elevado, deste modo atenuando quaisquer problemas de vão livre com respeito ao solo.
BRPI0515409-0A 2004-09-16 2005-09-15 dispositivo de ponta, superfìce de sustentação aerodinámica, aeronave, e, helicóptero BRPI0515409A (pt)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB0420601A GB0420601D0 (en) 2004-09-16 2004-09-16 Wing tip devices
PCT/GB2005/003553 WO2006030213A1 (en) 2004-09-16 2005-09-15 Wing tip devices

Publications (1)

Publication Number Publication Date
BRPI0515409A true BRPI0515409A (pt) 2008-07-22

Family

ID=33306681

Family Applications (1)

Application Number Title Priority Date Filing Date
BRPI0515409-0A BRPI0515409A (pt) 2004-09-16 2005-09-15 dispositivo de ponta, superfìce de sustentação aerodinámica, aeronave, e, helicóptero

Country Status (9)

Country Link
US (1) US7971832B2 (pt)
EP (1) EP1789316B1 (pt)
AT (1) ATE434560T1 (pt)
BR (1) BRPI0515409A (pt)
CA (1) CA2577602A1 (pt)
DE (1) DE602005015123D1 (pt)
ES (1) ES2329064T3 (pt)
GB (1) GB0420601D0 (pt)
WO (1) WO2006030213A1 (pt)

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GB0518755D0 (en) * 2005-09-14 2005-10-19 Airbus Uk Ltd Wing tip device
GB0711942D0 (en) * 2007-06-21 2007-08-01 Airbus Uk Ltd Winglet
DE102007059455A1 (de) 2007-12-10 2009-06-25 Airbus Deutschland Gmbh Flügelspitzenverlängerung zur Reduktion von Wirbelschleppen bei Flugzeugen
ES3040742T3 (en) 2008-06-20 2025-11-04 Aviation Partners Inc Curved wing tip
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
CA2761317A1 (en) * 2009-05-05 2010-11-11 Aerostar Aircraft Corporation Aircraft winglet design having a compound curve profile
GB0913602D0 (en) 2009-08-05 2009-09-16 Qinetiq Ltd Aircraft
GB201011843D0 (en) * 2010-07-14 2010-09-01 Airbus Operations Ltd Wing tip device
US7946826B1 (en) * 2010-07-16 2011-05-24 General Electric Company Wind turbine rotor blade with a suction side winglet
US8382041B1 (en) 2010-08-04 2013-02-26 The United States Of America As Represented By The Secretary Of The Air Force Rakelet
US8317483B2 (en) 2010-12-15 2012-11-27 General Electric Company Wind turbine rotor blade
DE102012103704B4 (de) 2011-04-30 2025-11-06 General Electric Renovables España, S.L. Winglet für einen Rotorflügel einer Windkraftanlage
DK3650337T3 (da) 2011-06-09 2021-02-22 Aviation Partners Inc Delt "blended" winglet
US9103325B2 (en) 2012-03-20 2015-08-11 General Electric Company Winglet for a wind turbine rotor blade
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
US9778457B2 (en) * 2014-02-12 2017-10-03 Brother Kogyo Kabushiki Kaisha Light deflector and polygon mirror
US11148788B2 (en) * 2016-02-12 2021-10-19 Textron Innovation, Inc. Curved wingtip for aircraft
EP3269635A1 (en) * 2016-07-12 2018-01-17 The Aircraft Performance Company UG Airplane wing
USD834491S1 (en) 2016-10-27 2018-11-27 Ge Aviation Systems Llc Propeller blade
ES2905192T3 (es) * 2018-01-15 2022-04-07 The Aircraft Performance Company Gmbh Ala de avión
GB201805279D0 (en) 2018-03-29 2018-05-16 Archangel Lightworks Ltd Wing tips and wing tips construction design methods
EP3774527A1 (en) * 2018-04-02 2021-02-17 Aero Design Labs, Inc. Elliptical wing tip and method of fabricating same
GB2576929A (en) * 2018-09-07 2020-03-11 Airbus Operations Ltd A wing tip device
US12162588B2 (en) 2019-01-07 2024-12-10 Aviation Partners, Inc. High performance winglet
WO2021073706A1 (en) 2019-10-19 2021-04-22 Oddershede Magnus Wingtip
USD930549S1 (en) * 2019-12-30 2021-09-14 Bombardier Inc. Aircraft winglet
CN111114751B (zh) * 2020-01-14 2023-10-27 吴海军 一种用于飞行器的叠翼结构
US11440644B2 (en) * 2020-02-21 2022-09-13 Textron Innovations Inc. Download reducing winglets for aircraft having a rotor producing downwash and method of operating the same
US12017754B2 (en) 2020-03-12 2024-06-25 Textron Innovations Inc. Download reducing wingtips
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
GB2628523B (en) * 2022-11-16 2025-07-09 Airbus Operations Ltd Aircraft wing

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US1275251A (en) * 1917-10-11 1918-08-13 Louisa Harb Automatic flying-machine.
US3411738A (en) * 1966-10-27 1968-11-19 William E. Sargent Airfoil tip
US3974986A (en) * 1973-05-29 1976-08-17 Johnstone Edmund H Aircraft wing vortex deflector
US4108403A (en) * 1977-08-05 1978-08-22 Reginald Vernon Finch Vortex reducing wing tip
US4595160A (en) * 1983-05-18 1986-06-17 Jonathan Santos Wing tip airfoils
US4674709A (en) * 1983-06-20 1987-06-23 Welles Stanley W Airframe design
GB8815955D0 (en) * 1988-07-05 1988-11-16 Westland Helicopters Helicopter rotor blades
US5039032A (en) * 1988-11-07 1991-08-13 The Boeing Company High taper wing tip extension
FR2689852B1 (fr) * 1992-04-09 1994-06-17 Eurocopter France Pale pour voilure tournante d'aeronef, a extremite en fleche.
US5348253A (en) * 1993-02-01 1994-09-20 Gratzer Louis B Blended winglet
US5634613A (en) * 1994-07-18 1997-06-03 Mccarthy; Peter T. Tip vortex generation technology for creating a lift enhancing and drag reducing upwash effect
FR2755941B1 (fr) * 1996-11-19 1999-01-15 Eurocopter France Pale a extremite en fleche pour voilure tournante d'aeronef
US6089502A (en) * 1997-06-13 2000-07-18 The Boeing Company Blunt-leading-edge raked wingtips
US6474604B1 (en) * 1999-04-12 2002-11-05 Jerry E. Carlow Mobius-like joining structure for fluid dynamic foils
US6484968B2 (en) * 2000-12-11 2002-11-26 Fort F. Felker Aircraft with elliptical winglets
DE10117721B4 (de) * 2001-04-09 2007-09-27 Gerd Heller Flügelspitzenverlängerung für einen Flügel
US6772615B2 (en) * 2001-09-20 2004-08-10 Nsk Ltd. Method of manufacturing hub unit for supporting wheel and die for manufacturing the same
US6578798B1 (en) * 2002-04-08 2003-06-17 Faruk Dizdarevic Airlifting surface division
US6547181B1 (en) * 2002-05-29 2003-04-15 The Boeing Company Ground effect wing having a variable sweep winglet
US7207526B2 (en) * 2002-06-26 2007-04-24 Mccarthy Peter T High efficiency tip vortex reversal and induced drag reduction

Also Published As

Publication number Publication date
EP1789316B1 (en) 2009-06-24
WO2006030213A1 (en) 2006-03-23
CA2577602A1 (en) 2006-03-23
US20070252031A1 (en) 2007-11-01
ES2329064T3 (es) 2009-11-20
GB0420601D0 (en) 2004-10-20
US7971832B2 (en) 2011-07-05
EP1789316A1 (en) 2007-05-30
ATE434560T1 (de) 2009-07-15
DE602005015123D1 (de) 2009-08-06

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Legal Events

Date Code Title Description
B08F Application dismissed because of non-payment of annual fees [chapter 8.6 patent gazette]

Free format text: REFERENTE A 6A ANUIDADE.

B08K Patent lapsed as no evidence of payment of the annual fee has been furnished to inpi [chapter 8.11 patent gazette]

Free format text: REFERENTE AO DESPACHO 8.6 PUBLICADO NA RPI 2160 DE 29/05/2012.