DE602006013338D1 - Flugzeug mit reduzierten umweltauswirkungen - Google Patents

Flugzeug mit reduzierten umweltauswirkungen

Info

Publication number
DE602006013338D1
DE602006013338D1 DE602006013338T DE602006013338T DE602006013338D1 DE 602006013338 D1 DE602006013338 D1 DE 602006013338D1 DE 602006013338 T DE602006013338 T DE 602006013338T DE 602006013338 T DE602006013338 T DE 602006013338T DE 602006013338 D1 DE602006013338 D1 DE 602006013338D1
Authority
DE
Germany
Prior art keywords
aircraft
engines
turboprop
plane
environmental impact
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
DE602006013338T
Other languages
English (en)
Inventor
Pierre-Emmanuel Gall
Christophe Cros
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 DE602006013338D1 publication Critical patent/DE602006013338D1/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
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/10—Aircraft characterised by the type or position of power plant of gas-turbine type
    • B64D27/14—Aircraft characterised by the type or position of power plant of gas-turbine type within or attached to fuselage
    • 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
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • 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
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D2027/005—Aircraft with an unducted turbofan comprising contra-rotating rotors, e.g. contra-rotating open rotors [CROR]
    • 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
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
DE602006013338T 2005-11-03 2006-10-23 Flugzeug mit reduzierten umweltauswirkungen Active DE602006013338D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0511176A FR2892705B1 (fr) 2005-11-03 2005-11-03 Aeronef a impact environnemental reduit.
PCT/FR2006/002372 WO2007051914A1 (fr) 2005-11-03 2006-10-23 Aéronef à impact environnemental réduit.

Publications (1)

Publication Number Publication Date
DE602006013338D1 true DE602006013338D1 (de) 2010-05-12

Family

ID=36570590

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602006013338T Active DE602006013338D1 (de) 2005-11-03 2006-10-23 Flugzeug mit reduzierten umweltauswirkungen

Country Status (11)

Country Link
US (1) US8313055B2 (de)
EP (1) EP1943144B1 (de)
JP (1) JP2009514724A (de)
CN (1) CN101300171B (de)
AT (1) ATE462645T1 (de)
BR (1) BRPI0617999A2 (de)
CA (1) CA2626201C (de)
DE (1) DE602006013338D1 (de)
FR (1) FR2892705B1 (de)
RU (1) RU2384479C2 (de)
WO (1) WO2007051914A1 (de)

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US7900865B2 (en) * 2006-12-19 2011-03-08 The Boeing Company Airplane configuration
FR2938504B1 (fr) * 2008-11-14 2010-12-10 Snecma Entree d'air d'un moteur d'avion a helices propulsives non carenees
FR2942513B1 (fr) * 2009-02-20 2011-05-27 Airbus France Aube pour recepteur de turbomachine, comprenant une partie pale integrant un fusible mecanique
DE102009010524A1 (de) 2009-02-25 2010-09-02 Rolls-Royce Deutschland Ltd & Co Kg Turbopropantrieb mit Druckpropeller
FR2943039B1 (fr) * 2009-03-12 2012-09-28 Airbus France Avion a empennage queue-de-morue et moteur arriere.
FR2964362B1 (fr) * 2010-09-03 2013-06-28 Airbus Operations Sas Avion a turbopropulseurs et empennage en croix.
US8393567B2 (en) * 2010-11-15 2013-03-12 The Boeing Company Method and apparatus for reducing aircraft noise
FR2971993B1 (fr) * 2011-02-25 2013-12-27 Airbus Operations Sas Aeronef a impact environnemental reduit
EP2610164B1 (de) * 2011-12-28 2015-10-28 Airbus Operations S.L. Rumpfheck mit einem Schild für ein Flugzeug mit rumpfmontierten Motoren und Verfahren zur Bestimmung der Fläche des Schildes
US9845159B2 (en) * 2013-03-07 2017-12-19 United Technologies Corporation Conjoined reverse core flow engine arrangement
USD735633S1 (en) * 2013-06-14 2015-08-04 Airbus Sas Aircraft
US9701395B2 (en) 2014-01-06 2017-07-11 United Technologies Corporation Contra-rotating open rotor distributed propulsion system
FR3030446B1 (fr) * 2014-12-17 2018-06-01 Safran Aircraft Engines Turbomachine a helice multi-diametres
FR3043984B1 (fr) * 2015-11-25 2017-12-22 Snecma Avion propulse par une turbomachine muni d'un ecran acoustique
USD797641S1 (en) * 2016-01-19 2017-09-19 Darold B Cummings Aircraft with slotted inboard wings
FR3050721B1 (fr) * 2016-04-28 2018-04-13 Airbus Operations Ensemble moteur pour aeronef comprenant un bord d'attaque de mat integre a une rangee annulaire d'aubes directrices de sortie non carenees
FR3052743B1 (fr) * 2016-06-20 2018-07-06 Airbus Operations Ensemble pour aeronef comprenant des moteurs a propulsion par ingestion de la couche limite
USD809993S1 (en) * 2016-12-22 2018-02-13 Toshikazu Tsukii Jet airplane
US11111029B2 (en) * 2017-07-28 2021-09-07 The Boeing Company System and method for operating a boundary layer ingestion fan
US10759545B2 (en) 2018-06-19 2020-09-01 Raytheon Technologies Corporation Hybrid electric aircraft system with distributed propulsion
US10906657B2 (en) * 2018-06-19 2021-02-02 Raytheon Technologies Corporation Aircraft system with distributed propulsion
USD922930S1 (en) * 2018-10-22 2021-06-22 Darold B. Cummings Aircraft
US11597501B2 (en) * 2018-12-31 2023-03-07 Blended Wing Aircraft, Inc. Deployable noise shield panels
US11267577B2 (en) 2019-12-06 2022-03-08 General Electric Company Aircraft having an engine wing assembly

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GB1364313A (en) * 1971-02-05 1974-08-21 Britten Norman Ltd Aircraft
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GB1480340A (en) * 1973-07-30 1977-07-20 Hawker Siddeley Aviation Ltd Aircraft
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US4149688A (en) * 1976-10-01 1979-04-17 Aereon Corporation Lifting body aircraft for V/STOL service
DE7808902U1 (de) * 1978-03-23 1978-11-16 Koehler, Klemens, 4400 Muenster Flugzeug mit propeller-manteltriebwerken
DE3219159A1 (de) * 1982-05-21 1983-11-24 Dornier Gmbh Anordnung von mit propellern arbeitenden antriebsanlagen an luftfahrzeugen
US4447022A (en) * 1982-05-21 1984-05-08 Lion Charles E Reduced noise monolithic wing-stabilizer aircraft
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US20030168552A1 (en) * 2002-03-05 2003-09-11 Brown Paul Anthony Aircraft propulsion system and method
FR2862045B1 (fr) * 2003-11-12 2006-05-05 Snecma Moteurs Turboreacteur destine a etre fixe sur le fuselage d'un avion et en particulier sur sa partie arriere
FR2873095B1 (fr) * 2004-07-15 2006-09-29 Airbus France Sas Avion multimoteur a puits de descente
FR2873096B1 (fr) * 2004-07-15 2007-11-23 Airbus France Sas Avion multimoteur
FR2884492B1 (fr) * 2005-04-13 2007-05-18 Airbus France Sas Aeronef a faible bruit, notamment lors des decollages et des atterrissages.
US20070023571A1 (en) * 2005-07-15 2007-02-01 Kawai Ronald T Quiet airplane configuration
USD622653S1 (en) * 2006-01-30 2010-08-31 The Boeing Company Aircraft
US8016233B2 (en) * 2006-01-30 2011-09-13 The Boeing Company Aircraft configuration
FR2898583B1 (fr) * 2006-03-20 2008-04-18 Airbus France Sas Aeronef a impact environnemental reduit
FR2905356B1 (fr) * 2006-09-05 2008-11-07 Airbus France Sas Procede pour la realisation d'un aeronef a impact environnemental reduit et aeronef obtenu
US7900865B2 (en) * 2006-12-19 2011-03-08 The Boeing Company Airplane configuration
USD607806S1 (en) * 2007-03-22 2010-01-12 Airbus Sas Aircraft tail
USD608720S1 (en) * 2007-03-22 2010-01-26 Airbus Sas Aircraft

Also Published As

Publication number Publication date
EP1943144A1 (de) 2008-07-16
FR2892705B1 (fr) 2009-04-24
CN101300171B (zh) 2012-07-04
US20080258005A1 (en) 2008-10-23
CA2626201C (fr) 2013-08-13
BRPI0617999A2 (pt) 2011-08-16
RU2384479C2 (ru) 2010-03-20
ATE462645T1 (de) 2010-04-15
CN101300171A (zh) 2008-11-05
EP1943144B1 (de) 2010-03-31
RU2008122042A (ru) 2009-12-20
FR2892705A1 (fr) 2007-05-04
JP2009514724A (ja) 2009-04-09
CA2626201A1 (fr) 2007-05-10
WO2007051914A1 (fr) 2007-05-10
US8313055B2 (en) 2012-11-20

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