FR2900907B1 - Ensemble moteur pour aeronef a nacelle et mat integres - Google Patents

Ensemble moteur pour aeronef a nacelle et mat integres

Info

Publication number
FR2900907B1
FR2900907B1 FR0651652A FR0651652A FR2900907B1 FR 2900907 B1 FR2900907 B1 FR 2900907B1 FR 0651652 A FR0651652 A FR 0651652A FR 0651652 A FR0651652 A FR 0651652A FR 2900907 B1 FR2900907 B1 FR 2900907B1
Authority
FR
France
Prior art keywords
mat
aircraft
engine assembly
integrated boom
boom
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
FR0651652A
Other languages
English (en)
Other versions
FR2900907A1 (fr
Inventor
Laurent Lafont
Lionel Diochon
Frederic Journade
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 FR0651652A priority Critical patent/FR2900907B1/fr
Publication of FR2900907A1 publication Critical patent/FR2900907A1/fr
Application granted granted Critical
Publication of FR2900907B1 publication Critical patent/FR2900907B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/402Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/40Arrangements for mounting power plants in aircraft
    • B64D27/406Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0651652A 2006-05-09 2006-05-09 Ensemble moteur pour aeronef a nacelle et mat integres Expired - Fee Related FR2900907B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0651652A FR2900907B1 (fr) 2006-05-09 2006-05-09 Ensemble moteur pour aeronef a nacelle et mat integres

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0651652A FR2900907B1 (fr) 2006-05-09 2006-05-09 Ensemble moteur pour aeronef a nacelle et mat integres

Publications (2)

Publication Number Publication Date
FR2900907A1 FR2900907A1 (fr) 2007-11-16
FR2900907B1 true FR2900907B1 (fr) 2008-12-19

Family

ID=37574805

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0651652A Expired - Fee Related FR2900907B1 (fr) 2006-05-09 2006-05-09 Ensemble moteur pour aeronef a nacelle et mat integres

Country Status (1)

Country Link
FR (1) FR2900907B1 (fr)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20080258016A1 (en) * 2007-04-23 2008-10-23 Gukeisen Robert L Nacelle assembly without lower bi-fi splitter
US9126691B2 (en) 2007-05-30 2015-09-08 United Technologies Corporation Access door for gas turbine engine components
FR2928136B1 (fr) * 2008-02-28 2010-04-02 Airbus France Ensemble moteur pour aeronef comprenant des attaches moteur deportees vers le bas sur le carter de soufflante.
FR2950323B1 (fr) 2009-09-22 2011-11-04 Airbus Operations Sas Mat d'accrochage de moteur d'aeronef, ensemble comprenant ce mat et aeronef associe
FR2950322B1 (fr) 2009-09-22 2012-05-25 Airbus Operations Sas Element d'accrochage d'un moteur d'aeronef, ensemble d'aeronef comprenant cet element et aeronef associe
FR2950860B1 (fr) 2009-10-01 2011-12-09 Airbus Operations Sas Dispositif d'accrochage d'un moteur a un mat d'aeronef

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3952973A (en) * 1974-12-20 1976-04-27 The Boeing Company Engine mounting assembly
GB9116986D0 (en) * 1991-08-07 1991-10-09 Rolls Royce Plc Gas turbine engine nacelle assembly
US6126110A (en) * 1997-12-22 2000-10-03 Mcdonnell Douglas Corporation Horizontally opposed trunnion forward engine mount system supported beneath a wing pylon
FR2862611B1 (fr) * 2003-11-25 2007-03-09 Airbus France Dispositif d'accrochage d'un moteur sous une voilure d'aeronef
FR2862944B1 (fr) * 2003-12-01 2006-02-24 Airbus France Dispositif d'accrochage d'un turbopropulseur sous une voilure d'aeronef
FR2885877B1 (fr) * 2005-05-23 2008-12-12 Airbus France Sas Mat d'accrochage de turboreacteur pour aeronef

Also Published As

Publication number Publication date
FR2900907A1 (fr) 2007-11-16

Similar Documents

Publication Publication Date Title
FR2898641B1 (fr) Habillage de carter dans un turboreacteur
FR2896537B1 (fr) Turbomachine a generateur-demarreur integre
DE602005003759D1 (de) Gegenläufiges Turbinentriebwerk
FR2952922B1 (fr) Ensemble de manutention d'un module de moteur d'aeronef
DE602007006800D1 (de) Steuervorrichtung für einen verbrennungsmotor und steuerverfahren für einen verbrennungsmotor
BRPI0817123A2 (pt) Motor a diesel
FR2925607B1 (fr) Nacelle pour moteur d'aeronef a tuyere de section variable
EP2066004A4 (fr) Moteur et compresseur
ATE509197T1 (de) Verbrennungskraftmaschine
EP1879283A4 (fr) Moteur
PL1902953T3 (pl) Silnik śmigłowca z turbiną gazową
GB0622405D0 (en) A turbine engine mounting arrangement
DE602007002797D1 (de) Brennstoffzuführvorrichtung und brennstoffzuführverfahren für einen verbrennungsmotor
DE602007003320D1 (de) Verbrennungsmotor
DE602007012229D1 (de) Einlasssteuerungsvorrichtung für einen verbrennungsmotor
DE602007004968D1 (de) Steuervorrichtung und steuerverfahren für einen verbrennungsmotor mit zentrifugalkompressor
EP2039897A4 (fr) Unité de commande et procédé de commande pour moteur à combustion interne
EP2107667A4 (fr) Moteur et compresseur
DE502007003336D1 (de) Brennkraftmaschine
FR2943040B1 (fr) Ensemble moteur et nacelle pour aeronef, equipe d'un dispositif anti-glace
DE602007003477D1 (de) Ansaugvorrichtung für einen verbrennungsmotor
DE602006015519D1 (de) Verbrennungsmotor mit einem turbolader
FR2900907B1 (fr) Ensemble moteur pour aeronef a nacelle et mat integres
DE502005004226D1 (de) Anordnung aus einer welle mit darauf montierter gleitringdichtung
FR2885878B1 (fr) Ensemble moteur pour aeronef

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: 11

PLFP Fee payment

Year of fee payment: 12

PLFP Fee payment

Year of fee payment: 13

PLFP Fee payment

Year of fee payment: 14

ST Notification of lapse

Effective date: 20210105