ATE431287T1 - Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt - Google Patents

Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt

Info

Publication number
ATE431287T1
ATE431287T1 AT06831066T AT06831066T ATE431287T1 AT E431287 T1 ATE431287 T1 AT E431287T1 AT 06831066 T AT06831066 T AT 06831066T AT 06831066 T AT06831066 T AT 06831066T AT E431287 T1 ATE431287 T1 AT E431287T1
Authority
AT
Austria
Prior art keywords
wing
aircraft
pressure
adjusts
local geometric
Prior art date
Application number
AT06831066T
Other languages
English (en)
Inventor
Thierry Fol
Philippe Jimenez
Arnaud Namer
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE431287T1 publication Critical patent/ATE431287T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D29/00—Power-plant nacelles, fairings or cowlings
    • B64D29/02—Power-plant nacelles, fairings or cowlings associated with wings
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • 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)
  • Tires In General (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
  • Pressure Welding/Diffusion-Bonding (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Hydraulic Turbines (AREA)
  • Measuring Fluid Pressure (AREA)
  • Toys (AREA)
AT06831066T 2005-11-08 2006-11-06 Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt ATE431287T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0511337A FR2892999B1 (fr) 2005-11-08 2005-11-08 Aeronef comportant un carenage central ajusteur de pression voilure par deformations geometriques locales
PCT/FR2006/002464 WO2007054635A1 (fr) 2005-11-08 2006-11-06 Aeronef comportant un carenage central ajusteur de pression voilure par déformations geometriques locales

Publications (1)

Publication Number Publication Date
ATE431287T1 true ATE431287T1 (de) 2009-05-15

Family

ID=36724619

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06831066T ATE431287T1 (de) 2005-11-08 2006-11-06 Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt

Country Status (11)

Country Link
US (1) US8177170B2 (de)
EP (1) EP1945502B1 (de)
JP (1) JP5431728B2 (de)
CN (1) CN101304918B (de)
AT (1) ATE431287T1 (de)
BR (1) BRPI0619664B1 (de)
CA (1) CA2626098C (de)
DE (1) DE602006006865D1 (de)
FR (1) FR2892999B1 (de)
RU (1) RU2424157C2 (de)
WO (1) WO2007054635A1 (de)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CA2716169C (en) * 2008-05-09 2013-12-17 The Boeing Company Aircraft fillet fairings with fixed and moveable portions, and associated systems and methods
US9027883B2 (en) 2008-11-05 2015-05-12 Airbus Operations Limited Aircraft fairing
CN101560929B (zh) * 2009-05-22 2010-08-25 中国科学院力学研究所 一种可变倾角超燃冲压发动机外整流罩
EP2338787B1 (de) * 2009-12-21 2011-12-14 Eurocopter Deutschland GmbH Abdichtung des Luftstroms zwischen einer Tragfläche und einem Rumpf
ES2399262B1 (es) * 2010-12-31 2014-04-29 Airbus Operations, S.L. Herraje regulable para la instalación y ajuste de carenas en aeronaves.
CN102642613B (zh) * 2012-05-11 2014-12-10 中国航空工业集团公司西安飞机设计研究所 波纹套低阻整流罩
EP2690008B1 (de) 2012-07-26 2015-06-10 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Hubschrauber mit aerodynamischem, abgerundetem Heckkörper
FR3000020B1 (fr) * 2012-12-26 2015-01-30 Airbus Operations Sas Avion a fuselage pourvu d'excroissances laterales delimitant des espaces de stockage
ES2578427T3 (es) 2012-12-27 2016-07-26 Airbus Operations S.L. Una carena ventral de una aeronave con una capacidad de almacenamiento mejorada
USD754053S1 (en) * 2014-02-19 2016-04-19 Aeronautical Testing Service, Inc. Wing root leading edge extension
US9725155B2 (en) 2015-12-30 2017-08-08 General Electric Company Method and system for open rotor engine fuselage protection
EP3348470B1 (de) 2017-01-16 2019-03-06 Deutsches Zentrum für Luft- und Raumfahrt e.V. Flugzeug oder fahrzeug mit konfiguration einer t-verbindung eines strömungshindernisses an einer wand zur begrenzung einer strömung
FR3077801B1 (fr) * 2018-02-14 2022-04-22 Dassault Aviat Portion d'aeronef a trainee d'onde reduite
WO2019178064A1 (en) * 2018-03-12 2019-09-19 Aero Design Labs, Inc. Wing-to-body trailing edge fairing and method of fabricating same
CN108860571B (zh) * 2018-07-26 2023-09-29 成都飞机工业（集团）有限责任公司 一种飞机翼身整流罩及其构建方法
CA3084642A1 (en) * 2019-06-24 2020-12-24 Bombardier Inc. Wing to fuse junction shaping, and associated systems and methods
US20210221491A1 (en) * 2019-10-15 2021-07-22 General Electric Company Fuselage shield for an aircraft with an unducted engine
US11814174B2 (en) * 2019-10-15 2023-11-14 General Electric Company Layered fuselage shield

Family Cites Families (36)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2800291A (en) * 1950-10-24 1957-07-23 Stephens Arthur Veryan Solid boundary surface for contact with a relatively moving fluid medium
US2927749A (en) * 1956-11-02 1960-03-08 Walter T Brownell Airfoil wing root fillet
JPS4840238B1 (de) * 1966-04-25 1973-11-29
GB1307990A (en) * 1969-05-27 1973-02-21 British Aircraft Corp Ltd Variable-geometry aircraft
US3578265A (en) * 1969-10-06 1971-05-11 Northrop Corp Aerodynamic structures
US4314681A (en) * 1979-08-31 1982-02-09 General Electric Company Drag-reducing component
FR2492337A1 (fr) * 1980-10-16 1982-04-23 Aerospatiale Aile d'aeronef pourvue d'un systeme hypersustentateur dans son bord d'attaque et aeronef comportant une telle aile
US4478377A (en) * 1980-12-22 1984-10-23 British Aerospace Public Limited Company Aircraft
US4506848A (en) * 1980-12-22 1985-03-26 British Aerospace Public Limited Company Aircraft configuration and control arrangement therefor
DE3149629C1 (de) * 1981-12-15 1983-04-21 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Einrichtung zum Abdichten eines Luftspaltes an einer Flugzeugklappe
US4624425A (en) * 1984-05-23 1986-11-25 Michael Austin Fixed wing light aircraft
DE214767T1 (de) * 1985-08-08 1987-07-02 British Aerospace Plc, London Kraftstoffladungsmittel.
US4801058A (en) * 1987-02-05 1989-01-31 Rolls-Royce Plc Aircraft and powerplant combinations
US6149101A (en) * 1991-07-08 2000-11-21 Tracy; Richard R. Aircraft wing and fuselage contours
US5282591A (en) * 1992-12-21 1994-02-01 The United States Of America As Represented By The Secretary Of The Navy Active vortex control for a high performance wing
US5779189A (en) * 1996-03-19 1998-07-14 Lockheed Martin Corporation System and method for diverting boundary layer air
JP3714722B2 (ja) * 1996-05-09 2005-11-09 本田技研工業株式会社 剥離抑制装置
DE19719922C1 (de) * 1997-05-13 1998-11-12 Daimler Benz Aerospace Airbus Einrichtung zur Beeinflussung einer Wurzelströmung
US5899413A (en) * 1997-12-01 1999-05-04 Mcdonnell Douglas Corporation Non-waisted fuselage design for supersonic aircraft
JP3980775B2 (ja) * 1998-10-28 2007-09-26 本田技研工業株式会社 飛行機の造波抵抗低減方法
US6409126B1 (en) * 2000-11-01 2002-06-25 Lockhead Martin Corporation Passive flow control of bluff body wake turbulence
RU2173658C1 (ru) * 2000-12-18 2001-09-20 Немыкин Артур Степанович Способ уменьшения лобового сопротивления движущегося объекта и устройство для его осуществления
FR2827028B1 (fr) * 2001-07-06 2003-09-26 Airbus France Aeronef a carenage ventral et joint pour un tel aeronef
FR2827029B1 (fr) * 2001-07-06 2003-10-17 Airbus France Aeronef a carenage ventral et joint pour un tel aeronef
EP1300335B1 (de) * 2001-10-05 2005-03-02 Airbus France Flugzeug mit Flügel-Rumpf-Verkleidungsdichtung
US6964397B2 (en) * 2003-07-18 2005-11-15 The Boeing Company Nacelle chine installation for drag reduction
US20050116107A1 (en) * 2003-11-11 2005-06-02 Supersonic Aerospace International, Llc Area ruling for vertical stabilizers
US20060006287A1 (en) * 2004-01-16 2006-01-12 Ferguson Stanley D Fairing and airfoil apparatus and method
FR2869872B1 (fr) * 2004-05-04 2007-07-20 Airbus France Sas Cale de transition entre un moyen de fixation d'une aile sur un fuselage d'un aeronef et ladite aile, et aeronef comportant une telle cale.
FR2871436B1 (fr) * 2004-06-11 2007-09-07 Airbus France Sas Aeronef muni d'un carenage ventral, et carenage ventral.
US7614588B2 (en) * 2004-12-23 2009-11-10 David Birkenstock Apparatus system and method for drag reduction
DE602006005221D1 (de) * 2006-03-16 2009-04-02 Eads Constr Aeronauticas Sa Elastisch vorgeformte Verkleidung für Flugzeuge und Verfahren zur ihrer Herstellung
FR2899201B1 (fr) * 2006-03-31 2009-02-13 Airbus France Sas Agencement d'aile d'aeronef comportant un mat d'accrochage de moteur definissant en zone avant un canal lateral d'ecoulement d'air
ES2301360B1 (es) * 2006-05-16 2009-05-01 Airbus España, S.L. Sistema de sellado del hueco existente entre el fuselaje y el timon de altura del estabilizador horizontal orientable de un avion, extendido con una carena aerodinamica de sellado de la abertura existente entre el fuselaje y el estabilizador horizontal orientable.
FR2901538B1 (fr) * 2006-05-23 2008-07-18 Airbus France Sas Aeronef comportant un dispositif de reduction de la trainee induite
FR2928622B1 (fr) * 2008-03-14 2011-12-02 Airbus France Mat de suspension d'avion comportant au moins un element pour former des tourbillons d'air

Also Published As

Publication number Publication date
RU2424157C2 (ru) 2011-07-20
CN101304918B (zh) 2010-05-19
CN101304918A (zh) 2008-11-12
US8177170B2 (en) 2012-05-15
RU2008123002A (ru) 2009-12-20
CA2626098C (en) 2014-08-12
BRPI0619664A2 (pt) 2011-10-11
EP1945502A1 (de) 2008-07-23
WO2007054635A1 (fr) 2007-05-18
JP5431728B2 (ja) 2014-03-05
DE602006006865D1 (de) 2009-06-25
JP2009514725A (ja) 2009-04-09
EP1945502B1 (de) 2009-05-13
CA2626098A1 (en) 2007-05-18
BRPI0619664B1 (pt) 2018-06-12
FR2892999B1 (fr) 2008-02-01
US20090078830A1 (en) 2009-03-26
FR2892999A1 (fr) 2007-05-11

Similar Documents

Publication Publication Date Title
ATE431287T1 (de) Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt
WO2020003239A3 (en) Tail sitter
MX378338B (es) Una aeronave multirrotor con un fuselaje y al menos un ala.
ATE512049T1 (de) Flugzeug mit ringförmigem heck
US10005545B2 (en) Aircraft wing rib
UA106677C2 (uk) Літак інтегрального аеродинамічного компонування
ATE490912T1 (de) Steuersystem für einlassverzerrung und wiederherstellung
WO2013064768A3 (fr) Pylone d'accrochage pour turbomachine
WO2008154066A3 (en) Methods and apparatus for aircraft
US20160280358A1 (en) Hybrid Flow Control Method for Simple Hinged Flap High-Lift System
EP2452873A3 (de) Flugzeugflügelverlängerung und Düsensystem
RU2015108033A (ru) Крыло самолета с системой образования ламинарного потока в пограничном слое
DE602007009390D1 (de) Flugzeug mit konvertierbarem flugsystem
WO2020226708A3 (en) Fluidic propulsive system
WO2012028467A8 (en) Air sucking vehicle fuselage component, method for producing an air sucking vehicle fuselage component and a vehicle, especially an aircraft, with an air sucking vehicle fuselage component
BRPI0911484A2 (pt) asa de sustentação para uma aeronave
WO2009133217A8 (es) Conjunto soporte-maqueta de mínima interferencia aerodinámica para ensayos en régimen transónico en túnel de viento
ATE446245T1 (de) Flugzeugflügelanordnung mit einer triebwerksbefestigungsgondel, die im vorderen bereich einen lateralen luftstromkanal definiert
JP2015533111A5 (de)
EP2700573A3 (de) Druckfester Flugzeugrumpf mit einem Druckschott
FR2938504B1 (fr) Entree d'air d'un moteur d'avion a helices propulsives non carenees
US20160068270A1 (en) Air generation unit for an aircraft
MX2007015026A (es) Avion de juguete.
ATE542739T1 (de) Flugzeugflügel
DE602007010125D1 (de) Luftfahrzeug mit einer vorrichtung zur verringerung des luftwiderstands

Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties