FR2954277B1 - Suspension d'un turboreacteur a un aeronef - Google Patents

Suspension d'un turboreacteur a un aeronef

Info

Publication number
FR2954277B1
FR2954277B1 FR0959150A FR0959150A FR2954277B1 FR 2954277 B1 FR2954277 B1 FR 2954277B1 FR 0959150 A FR0959150 A FR 0959150A FR 0959150 A FR0959150 A FR 0959150A FR 2954277 B1 FR2954277 B1 FR 2954277B1
Authority
FR
France
Prior art keywords
aircraft
suspension
turbojet engine
turbojet
engine
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
FR0959150A
Other languages
English (en)
Other versions
FR2954277A1 (fr
Inventor
Jeremy Fert
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.)
Safran Aircraft Engines SAS
Original Assignee
SNECMA 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 SNECMA SAS filed Critical SNECMA SAS
Priority to FR0959150A priority Critical patent/FR2954277B1/fr
Publication of FR2954277A1 publication Critical patent/FR2954277A1/fr
Application granted granted Critical
Publication of FR2954277B1 publication Critical patent/FR2954277B1/fr
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; 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links
    • 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR0959150A 2009-12-17 2009-12-17 Suspension d'un turboreacteur a un aeronef Active FR2954277B1 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
FR0959150A FR2954277B1 (fr) 2009-12-17 2009-12-17 Suspension d'un turboreacteur a un aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0959150A FR2954277B1 (fr) 2009-12-17 2009-12-17 Suspension d'un turboreacteur a un aeronef

Publications (2)

Publication Number Publication Date
FR2954277A1 FR2954277A1 (fr) 2011-06-24
FR2954277B1 true FR2954277B1 (fr) 2012-03-23

Family

ID=42315251

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0959150A Active FR2954277B1 (fr) 2009-12-17 2009-12-17 Suspension d'un turboreacteur a un aeronef

Country Status (1)

Country Link
FR (1) FR2954277B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20140084129A1 (en) 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon
CA2918320C (fr) 2013-07-26 2018-05-15 Mra Systems, Inc. Mat d'accrochage de moteur pour aeronef
FR3059298B1 (fr) * 2016-11-29 2019-05-17 Airbus Operations Ensemble pour aeronef comprenant un moteur de type " open rotor puller " et des moyens d'accrochage de celui-ci a la structure rigide d'un mat d'accrochage

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2903382B1 (fr) * 2006-07-10 2008-10-10 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal
FR2915177B1 (fr) * 2007-04-20 2009-07-10 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif
FR2931800B1 (fr) * 2008-05-29 2010-07-30 Airbus France Dispositif de reprise des efforts de poussee pour mat d'accrochage de moteur d'aeronef, comprenant des bielles laterales a butees de palonnier integrees

Also Published As

Publication number Publication date
FR2954277A1 (fr) 2011-06-24

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