FR2931799B1 - Avion a reacteurs arrieres. - Google Patents

Avion a reacteurs arrieres.

Info

Publication number
FR2931799B1
FR2931799B1 FR0853591A FR0853591A FR2931799B1 FR 2931799 B1 FR2931799 B1 FR 2931799B1 FR 0853591 A FR0853591 A FR 0853591A FR 0853591 A FR0853591 A FR 0853591A FR 2931799 B1 FR2931799 B1 FR 2931799B1
Authority
FR
France
Prior art keywords
airplane
reactors
rear reactors
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.)
Expired - Fee Related
Application number
FR0853591A
Other languages
English (en)
Other versions
FR2931799A1 (fr
Inventor
Olivier Cazals
Alexis Manneville
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
Priority to FR0853591A priority Critical patent/FR2931799B1/fr
Priority to US12/473,338 priority patent/US8573531B2/en
Publication of FR2931799A1 publication Critical patent/FR2931799A1/fr
Application granted granted Critical
Publication of FR2931799B1 publication Critical patent/FR2931799B1/fr
Expired - Fee Related 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; 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
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
FR0853591A 2008-05-30 2008-05-30 Avion a reacteurs arrieres. Expired - Fee Related FR2931799B1 (fr)

Priority Applications (2)

Application Number Priority Date Filing Date Title
FR0853591A FR2931799B1 (fr) 2008-05-30 2008-05-30 Avion a reacteurs arrieres.
US12/473,338 US8573531B2 (en) 2008-05-30 2009-05-28 Airplane with rear engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0853591A FR2931799B1 (fr) 2008-05-30 2008-05-30 Avion a reacteurs arrieres.

Publications (2)

Publication Number Publication Date
FR2931799A1 FR2931799A1 (fr) 2009-12-04
FR2931799B1 true FR2931799B1 (fr) 2010-12-24

Family

ID=40223241

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0853591A Expired - Fee Related FR2931799B1 (fr) 2008-05-30 2008-05-30 Avion a reacteurs arrieres.

Country Status (2)

Country Link
US (1) US8573531B2 (fr)
FR (1) FR2931799B1 (fr)

Families Citing this family (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2937952B1 (fr) * 2008-10-30 2010-12-17 Snecma Avion a moteurs partiellement encastres dans le fuselage
FR2943623B1 (fr) * 2009-03-30 2011-04-29 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs montee oscillante sur le fuselage
FR2997681B1 (fr) * 2012-11-08 2015-05-15 Snecma Avion propulse par un turboreacteur a soufflantes contrarotatives
WO2014074144A1 (fr) 2012-11-12 2014-05-15 United Technologies Corporation Inverseurs de poussée cadencés
WO2014092757A1 (fr) 2012-12-11 2014-06-19 United Technologies Corporation Inverseurs de poussée asymétriques
US9845159B2 (en) * 2013-03-07 2017-12-19 United Technologies Corporation Conjoined reverse core flow engine arrangement
WO2014193515A2 (fr) * 2013-03-14 2014-12-04 United Technologies Corporation Bloc réacteur inverse à inverseur de poussée
FR3020347B1 (fr) * 2014-04-28 2016-05-20 Airbus Operations Sas Procede d'assemblage d'une partie arriere d'aeronef
FR3052743B1 (fr) * 2016-06-20 2018-07-06 Airbus Operations Ensemble pour aeronef comprenant des moteurs a propulsion par ingestion de la couche limite
US10538335B2 (en) * 2016-12-19 2020-01-21 The Boeing Company Boundary layer ingestion integration into aft fuselage
FR3060531B1 (fr) * 2016-12-20 2019-05-31 Airbus Operations Partie arriere d'aeronef comprenant un cadre de fuselage supportant deux moteurs partiellement enterres
FR3063771B1 (fr) * 2017-03-07 2021-04-02 Safran Aircraft Engines Inverseur de poussee pour appareil a turboreacteur enterre
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
FR3101853B1 (fr) * 2019-10-15 2022-04-29 Safran Nacelles Avion à nacelle déportée affleurant le sillage de l’aile
CN111846251B (zh) * 2020-07-10 2024-03-19 山东太古飞机工程有限公司 一种用于发动机进气口、排气及尾喷嘴的防沙保护装置

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR1271797A (fr) * 1960-09-17 1961-09-15 Hamburger Flugzeugbau Gmbh Installation de moteurs à réaction sur avion
US3085770A (en) * 1960-09-22 1963-04-16 Lockheed Aircraft Corp Aircraft propulsion system
FR1314597A (fr) * 1961-12-16 1963-01-11 Hamburger Flugzeugbau Gmbh Installation de moteurs à réaction dans la queue des avions
FR1443200A (fr) * 1965-04-21 1966-06-24 Bristol Siddeley Engines Ltd Groupe propulseur utilisant une turbine à gaz, pour aéronefs
GB1252759A (fr) * 1968-05-14 1971-11-10
FR2041146A1 (fr) * 1969-04-09 1971-01-29 British Aircraft Corp Ltd
DE3219159A1 (de) * 1982-05-21 1983-11-24 Dornier Gmbh Anordnung von mit propellern arbeitenden antriebsanlagen an luftfahrzeugen
US4549708A (en) * 1982-08-31 1985-10-29 United Technologies Corporation Cowling latch system
US5046689A (en) * 1989-04-19 1991-09-10 The Boeing Company Cowling interlock system
US5350136A (en) * 1993-05-14 1994-09-27 United Technologies Corporation Nacelle arrangement
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
FR2811716B1 (fr) * 2000-07-17 2002-10-04 Hurel Dubois Avions Perfectionnements aux arriere-corps de nacelle, a tuyere commune, de reacteur d'avion
US6651928B1 (en) * 2002-09-05 2003-11-25 The Boeing Company Aircraft engine nacelles and methods for their manufacture
GB0320371D0 (en) * 2003-08-29 2003-10-01 Rolls Royce Plc A closure panel arrangement
FR2937301B1 (fr) * 2008-10-22 2010-12-10 Snecma Avion a groupes motopropulseurs partiellement encastres dans le fuselage

Also Published As

Publication number Publication date
US8573531B2 (en) 2013-11-05
US20100038472A1 (en) 2010-02-18
FR2931799A1 (fr) 2009-12-04

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Legal Events

Date Code Title Description
CA Change of address

Effective date: 20110916

CD Change of name or company name

Owner name: AIRBUS HOLDING, FR

Effective date: 20110916

CJ Change in legal form

Effective date: 20110916

TP Transmission of property

Owner name: AIRBUS HOLDING, FR

Effective date: 20110913

PLFP Fee payment

Year of fee payment: 9

PLFP Fee payment

Year of fee payment: 10

PLFP Fee payment

Year of fee payment: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

ST Notification of lapse

Effective date: 20220105