DE602006006865D1 - 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
DE602006006865D1
DE602006006865D1 DE602006006865T DE602006006865T DE602006006865D1 DE 602006006865 D1 DE602006006865 D1 DE 602006006865D1 DE 602006006865 T DE602006006865 T DE 602006006865T DE 602006006865 T DE602006006865 T DE 602006006865T DE 602006006865 D1 DE602006006865 D1 DE 602006006865D1
Authority
DE
Germany
Prior art keywords
wing
central
pressure
geometric deformation
powerline
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
DE602006006865T
Other languages
English (en)
Inventor
Thierry Fol
Philippe Jimenez
Arnaud Namer
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.)
Airbus Operations SAS
Original Assignee
Airbus Operations SAS
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 Operations SAS filed Critical Airbus Operations SAS
Publication of DE602006006865D1 publication Critical patent/DE602006006865D1/de
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
DE602006006865T 2005-11-08 2006-11-06 Flugzeug mit zentraler stromlinienverkleidung, die den druck auf die flügelstrukturen mittels lokaler geometrischer verformungen einstellt Active DE602006006865D1 (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
DE602006006865D1 true DE602006006865D1 (de) 2009-06-25

Family

ID=36724619

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006006865T Active DE602006006865D1 (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)

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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
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
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

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Also Published As

Publication number Publication date
CA2626098C (en) 2014-08-12
BRPI0619664A2 (pt) 2011-10-11
CA2626098A1 (en) 2007-05-18
JP5431728B2 (ja) 2014-03-05
JP2009514725A (ja) 2009-04-09
US8177170B2 (en) 2012-05-15
WO2007054635A1 (fr) 2007-05-18
EP1945502B1 (de) 2009-05-13
CN101304918B (zh) 2010-05-19
CN101304918A (zh) 2008-11-12
FR2892999A1 (fr) 2007-05-11
US20090078830A1 (en) 2009-03-26
RU2008123002A (ru) 2009-12-20
EP1945502A1 (de) 2008-07-23
RU2424157C2 (ru) 2011-07-20
ATE431287T1 (de) 2009-05-15
FR2892999B1 (fr) 2008-02-01
BRPI0619664B1 (pt) 2018-06-12

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