ATE467560T1 - Flugzeug mit vermindertem lärmpegel - Google Patents

Flugzeug mit vermindertem lärmpegel

Info

Publication number
ATE467560T1
ATE467560T1 AT07731141T AT07731141T ATE467560T1 AT E467560 T1 ATE467560 T1 AT E467560T1 AT 07731141 T AT07731141 T AT 07731141T AT 07731141 T AT07731141 T AT 07731141T AT E467560 T1 ATE467560 T1 AT E467560T1
Authority
AT
Austria
Prior art keywords
airplane
noise level
reduced noise
aircraft
propeller
Prior art date
Application number
AT07731141T
Other languages
English (en)
Inventor
Pierre-Emmanuel Gall
Christophe Cros
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
Application granted granted Critical
Publication of ATE467560T1 publication Critical patent/ATE467560T1/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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/14—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, fuselages
    • 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
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Tires In General (AREA)
  • Toys (AREA)
  • Compositions Of Macromolecular Compounds (AREA)
  • Diaphragms For Electromechanical Transducers (AREA)
  • Waveguide Aerials (AREA)
  • Ignition Installations For Internal Combustion Engines (AREA)
  • Transmission Devices (AREA)
AT07731141T 2006-03-20 2007-03-15 Flugzeug mit vermindertem lärmpegel ATE467560T1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0602405A FR2898583B1 (fr) 2006-03-20 2006-03-20 Aeronef a impact environnemental reduit
PCT/FR2007/000447 WO2007107647A1 (fr) 2006-03-20 2007-03-15 Aeronef a impact environnemental reduit

Publications (1)

Publication Number Publication Date
ATE467560T1 true ATE467560T1 (de) 2010-05-15

Family

ID=37311929

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07731141T ATE467560T1 (de) 2006-03-20 2007-03-15 Flugzeug mit vermindertem lärmpegel

Country Status (11)

Country Link
US (1) US8196860B2 (de)
EP (1) EP1996464B1 (de)
JP (1) JP5070276B2 (de)
CN (1) CN101405185B (de)
AT (1) ATE467560T1 (de)
BR (1) BRPI0707010A2 (de)
CA (1) CA2641015A1 (de)
DE (1) DE602007006440D1 (de)
FR (1) FR2898583B1 (de)
RU (1) RU2388657C1 (de)
WO (1) WO2007107647A1 (de)

Families Citing this family (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2892705B1 (fr) * 2005-11-03 2009-04-24 Airbus France Sas Aeronef a impact environnemental reduit.
DE102008024463B4 (de) * 2008-05-21 2011-02-24 Bauhaus Luftfahrt E.V. Flugzeugantriebssystem
FR2938504B1 (fr) * 2008-11-14 2010-12-10 Snecma Entree d'air d'un moteur d'avion a helices propulsives non carenees
ES2373812B1 (es) * 2008-12-17 2012-12-18 Airbus Operations, S.L. Superficie estabilizadora horizontal de aeronave.
US8740139B1 (en) * 2012-04-23 2014-06-03 The Boeing Company Leading edge snag for exposed propeller engine installation
US9637218B2 (en) * 2012-11-12 2017-05-02 United Technologies Corporation Aircraft with forward sweeping T-tail
US10112696B2 (en) 2012-11-12 2018-10-30 United Technologies Corporation Stabilizer sacrificial surfaces
EP2920068B1 (de) * 2012-11-15 2017-11-29 United Technologies Corporation Stabilisator mit struktureller box und opferoberflächen
USD735633S1 (en) * 2013-06-14 2015-08-04 Airbus Sas Aircraft
FR3043984B1 (fr) 2015-11-25 2017-12-22 Snecma Avion propulse par une turbomachine muni d'un ecran acoustique
EP3187420B1 (de) * 2015-12-31 2018-05-23 Airbus Operations S.L. Flugzeug mit hinten montierten motoren
FR3077801B1 (fr) * 2018-02-14 2022-04-22 Dassault Aviat Portion d'aeronef a trainee d'onde reduite
US11597501B2 (en) * 2018-12-31 2023-03-07 Blended Wing Aircraft, Inc. Deployable noise shield panels
US11506067B2 (en) 2019-10-15 2022-11-22 General Electric Company Gas turbine engine with clutch assembly
US11286795B2 (en) 2019-10-15 2022-03-29 General Electric Company Mount for an airfoil
US11834196B2 (en) 2019-10-15 2023-12-05 General Electric Company System and method for control for unducted engine
US11814174B2 (en) 2019-10-15 2023-11-14 General Electric Company Layered fuselage shield
US11401824B2 (en) 2019-10-15 2022-08-02 General Electric Company Gas turbine engine outlet guide vane assembly
US12410758B2 (en) 2022-01-10 2025-09-09 General Electric Company Three-stream gas turbine engine control
JP7779789B2 (ja) * 2022-03-31 2025-12-03 本田技研工業株式会社 航空機
JP7783785B2 (ja) 2022-06-07 2025-12-10 本田技研工業株式会社 航空機
US12275532B2 (en) 2022-08-15 2025-04-15 General Electric Company Gas turbine engine noise reduction
US12480449B2 (en) 2022-08-22 2025-11-25 General Electric Company Propulsion system including an electric machine for starting a gas turbine engine
US12352181B2 (en) 2023-01-30 2025-07-08 General Electric Company Turbine airfoils

Family Cites Families (16)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3145954A (en) * 1962-03-07 1964-08-25 Robert W Jenny Vehicle for non-air, semi-air, and full-air supported travel
US3652035A (en) * 1969-06-12 1972-03-28 Charles G Fredericks Channel tail aircraft
US3684217A (en) * 1970-09-30 1972-08-15 Aereon Corp Aircraft
GB1480340A (en) * 1973-07-30 1977-07-20 Hawker Siddeley Aviation Ltd Aircraft
US4447022A (en) * 1982-05-21 1984-05-08 Lion Charles E Reduced noise monolithic wing-stabilizer aircraft
DE3219159A1 (de) * 1982-05-21 1983-11-24 Dornier Gmbh Anordnung von mit propellern arbeitenden antriebsanlagen an luftfahrzeugen
GB2188987B (en) * 1986-04-09 1990-02-14 Rolls Royce A turbofan gas turbine engine and mountings therefor
US4767083A (en) * 1986-11-24 1988-08-30 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration High performance forward swept wing aircraft
US4976396A (en) * 1987-11-13 1990-12-11 The Boeing Company Aircraft configuration with aft mounted engines
US4896160A (en) * 1988-02-19 1990-01-23 Aereon Corporation Airborne surveillance platform
US6113028A (en) * 1996-02-22 2000-09-05 Lohse; James R. Amphibious aircraft
RU2139812C1 (ru) * 1998-04-21 1999-10-20 Российский авиационный консорциум Самолет с тремя двигателями
RU2141433C1 (ru) * 1999-01-06 1999-11-20 Куваев Владимир Яковлевич Сверхзвуковой самолет
US6196498B1 (en) * 1999-12-21 2001-03-06 Lockheed Martin Corporation Semi-buoyant vehicle with aerodynamic lift capability
RU2252176C1 (ru) * 2003-11-27 2005-05-20 Открытое акционерное общество "Туполев" (ОАО "Туполев") Устройство крепления авиационного двигателя летательного аппарата
FR2873096B1 (fr) * 2004-07-15 2007-11-23 Airbus France Sas Avion multimoteur

Also Published As

Publication number Publication date
BRPI0707010A2 (pt) 2011-04-12
US8196860B2 (en) 2012-06-12
FR2898583B1 (fr) 2008-04-18
FR2898583A1 (fr) 2007-09-21
CA2641015A1 (fr) 2007-09-27
US20090020643A1 (en) 2009-01-22
CN101405185B (zh) 2011-03-23
RU2388657C1 (ru) 2010-05-10
JP2009530173A (ja) 2009-08-27
DE602007006440D1 (de) 2010-06-24
JP5070276B2 (ja) 2012-11-07
EP1996464A1 (de) 2008-12-03
EP1996464B1 (de) 2010-05-12
WO2007107647A1 (fr) 2007-09-27
CN101405185A (zh) 2009-04-08

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Legal Events

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