FR2952614B1 - Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef - Google Patents

Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef

Info

Publication number
FR2952614B1
FR2952614B1 FR0958124A FR0958124A FR2952614B1 FR 2952614 B1 FR2952614 B1 FR 2952614B1 FR 0958124 A FR0958124 A FR 0958124A FR 0958124 A FR0958124 A FR 0958124A FR 2952614 B1 FR2952614 B1 FR 2952614B1
Authority
FR
France
Prior art keywords
aircraft
turbomoteur
suspension
suspension beam
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
FR0958124A
Other languages
English (en)
Other versions
FR2952614A1 (fr
Inventor
Patrick Dunleavy
Richard Masson
Guilhem Seize
Guillaume Lefort
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
Safran Landing Systems SAS
Original Assignee
Messier Dowty SA
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
Priority to FR0958124A priority Critical patent/FR2952614B1/fr
Application filed by Messier Dowty SA, SNECMA SAS filed Critical Messier Dowty SA
Priority to CA2768085A priority patent/CA2768085C/fr
Priority to EP10737561.0A priority patent/EP2459446B1/fr
Priority to PCT/EP2010/060856 priority patent/WO2011012603A2/fr
Priority to RU2012107090/11A priority patent/RU2571680C2/ru
Priority to BR112012001965A priority patent/BR112012001965B8/pt
Priority to US13/387,534 priority patent/US9321537B2/en
Priority to CN2010800340198A priority patent/CN102470928A/zh
Publication of FR2952614A1 publication Critical patent/FR2952614A1/fr
Application granted granted Critical
Publication of FR2952614B1 publication Critical patent/FR2952614B1/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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • 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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
FR0958124A 2009-07-28 2009-11-17 Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef Active FR2952614B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0958124A FR2952614B1 (fr) 2009-11-17 2009-11-17 Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef
EP10737561.0A EP2459446B1 (fr) 2009-07-28 2010-07-27 Poutre de suspension de turbomoteur a la structure d'un aeronef
PCT/EP2010/060856 WO2011012603A2 (fr) 2009-07-28 2010-07-27 Poutre de suspension de turbomoteur a la structure d'un aeronef
RU2012107090/11A RU2571680C2 (ru) 2009-07-28 2010-07-27 Балка подвески турбинного двигателя к конструкции летательного аппарата
CA2768085A CA2768085C (fr) 2009-07-28 2010-07-27 Poutre de suspension de turbomoteur a la structure d'un aeronef
BR112012001965A BR112012001965B8 (pt) 2009-07-28 2010-07-27 viga para a suspensão de um turbomotor na estrutura de uma aeronave, utilização de uma viga, e, aeronave
US13/387,534 US9321537B2 (en) 2009-07-28 2010-07-27 Beam for suspending a turboshaft engine from an aircraft structure
CN2010800340198A CN102470928A (zh) 2009-07-28 2010-07-27 用于从飞机结构悬置涡轮轴引擎的梁

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0958124A FR2952614B1 (fr) 2009-11-17 2009-11-17 Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef

Publications (2)

Publication Number Publication Date
FR2952614A1 FR2952614A1 (fr) 2011-05-20
FR2952614B1 true FR2952614B1 (fr) 2012-02-03

Family

ID=42199997

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0958124A Active FR2952614B1 (fr) 2009-07-28 2009-11-17 Poutre de suspension d'un turbomoteur a la structure d'un aeronef, utilisation de la poutre et aeronef

Country Status (1)

Country Link
FR (1) FR2952614B1 (fr)

Families Citing this family (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3026137B1 (fr) 2014-09-22 2019-03-15 Safran Aircraft Engines Element pour une turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur d'avion
FR3039204B1 (fr) * 2015-07-24 2017-07-21 Snecma Ensemble de montage d'une turbomachine
FR3049582B1 (fr) * 2016-03-31 2023-01-13 Snecma Turbomachine, telle par exemple qu'un turboreacteur ou un turbopropulseur

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2919284B1 (fr) * 2007-07-26 2010-09-24 Snecma Piece mecanique comportant un insert en materiau composite.
FR2925016B1 (fr) * 2007-12-12 2010-06-18 Snecma Suspension d'un turboreacteur a un aeronef

Also Published As

Publication number Publication date
FR2952614A1 (fr) 2011-05-20

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Owner name: SAFRAN LANDING SYSTEMS, FR

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