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 einstelltInfo
- 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
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)
- Measuring Fluid Pressure (AREA)
- Toys (AREA)
- Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
- Hydraulic Turbines (AREA)
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 (17)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102015444B (zh) * | 2008-05-09 | 2014-02-19 | 波音公司 | 具有固定和可运动部分的航行器整流片整流装置和相关系统及方法 |
WO2010052446A1 (en) * | 2008-11-05 | 2010-05-14 | Airbus Uk 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 |
EP2749493B1 (de) | 2012-12-27 | 2016-03-23 | Airbus Operations, S.L. | Flugzeug-Bauchverkleidung mit verbesserter Ladekapazität |
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 |
BR112020018688A2 (pt) * | 2018-03-12 | 2020-12-29 | Aero Design Labs, Inc. | Método para fabricar uma carenagem de asa ao corpo e carenagem de asa ao corpo |
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 |
US20210221491A1 (en) * | 2019-10-15 | 2021-07-22 | General Electric Company | Fuselage shield for an aircraft with an unducted engine |
CN112660396A (zh) * | 2019-10-15 | 2021-04-16 | 通用电气公司 | 用于飞行器的可去除机身护罩 |
Family Cites Families (34)
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 |
US4776537A (en) * | 1985-08-08 | 1988-10-11 | British Aerospace Plc | Fuel storage means |
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 |
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 |
FR2827029B1 (fr) * | 2001-07-06 | 2003-10-17 | Airbus France | Aeronef a carenage ventral et joint pour un tel aeronef |
FR2827028B1 (fr) * | 2001-07-06 | 2003-09-26 | 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 |
-
2005
- 2005-11-08 FR FR0511337A patent/FR2892999B1/fr not_active Expired - Fee Related
-
2006
- 2006-11-06 CN CN2006800415944A patent/CN101304918B/zh active Active
- 2006-11-06 AT AT06831066T patent/ATE431287T1/de not_active IP Right Cessation
- 2006-11-06 WO PCT/FR2006/002464 patent/WO2007054635A1/fr active Application Filing
- 2006-11-06 JP JP2008538383A patent/JP5431728B2/ja active Active
- 2006-11-06 DE DE602006006865T patent/DE602006006865D1/de active Active
- 2006-11-06 CA CA2626098A patent/CA2626098C/en active Active
- 2006-11-06 EP EP06831066A patent/EP1945502B1/de active Active
- 2006-11-06 BR BRPI0619664-0A patent/BRPI0619664B1/pt not_active IP Right Cessation
- 2006-11-06 US US12/092,614 patent/US8177170B2/en active Active
- 2006-11-06 RU RU2008123002/11A patent/RU2424157C2/ru not_active IP Right Cessation
Also Published As
Publication number | Publication date |
---|---|
RU2424157C2 (ru) | 2011-07-20 |
BRPI0619664A2 (pt) | 2011-10-11 |
CA2626098C (en) | 2014-08-12 |
FR2892999B1 (fr) | 2008-02-01 |
RU2008123002A (ru) | 2009-12-20 |
CA2626098A1 (en) | 2007-05-18 |
US20090078830A1 (en) | 2009-03-26 |
WO2007054635A1 (fr) | 2007-05-18 |
US8177170B2 (en) | 2012-05-15 |
EP1945502A1 (de) | 2008-07-23 |
JP5431728B2 (ja) | 2014-03-05 |
BRPI0619664B1 (pt) | 2018-06-12 |
CN101304918A (zh) | 2008-11-12 |
CN101304918B (zh) | 2010-05-19 |
EP1945502B1 (de) | 2009-05-13 |
DE602006006865D1 (de) | 2009-06-25 |
JP2009514725A (ja) | 2009-04-09 |
FR2892999A1 (fr) | 2007-05-11 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
RER | Ceased as to paragraph 5 lit. 3 law introducing patent treaties |