FR2948633B1 - Poutre de suspension annulaire de turbomoteur a la structure d'un aeronef - Google Patents

Poutre de suspension annulaire de turbomoteur a la structure d'un aeronef

Info

Publication number
FR2948633B1
FR2948633B1 FR0903696A FR0903696A FR2948633B1 FR 2948633 B1 FR2948633 B1 FR 2948633B1 FR 0903696 A FR0903696 A FR 0903696A FR 0903696 A FR0903696 A FR 0903696A FR 2948633 B1 FR2948633 B1 FR 2948633B1
Authority
FR
France
Prior art keywords
turbomoteur
aircraft
annular
suspension beam
suspension
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
FR0903696A
Other languages
English (en)
Other versions
FR2948633A1 (fr
Inventor
Patrick Dunleavy
Richard Masson
Guilhem Seize
Guillaume Lefort
Thibaut Roux
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
Priority to FR0903696A priority Critical patent/FR2948633B1/fr
Application filed by SNECMA SAS filed Critical SNECMA SAS
Priority to CA2768085A priority patent/CA2768085C/fr
Priority to BR112012001965A priority patent/BR112012001965B8/pt
Priority to EP10737561.0A priority patent/EP2459446B1/fr
Priority to CN2010800340198A priority patent/CN102470928A/zh
Priority to RU2012107090/11A priority patent/RU2571680C2/ru
Priority to US13/387,534 priority patent/US9321537B2/en
Priority to PCT/EP2010/060856 priority patent/WO2011012603A2/fr
Publication of FR2948633A1 publication Critical patent/FR2948633A1/fr
Application granted granted Critical
Publication of FR2948633B1 publication Critical patent/FR2948633B1/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
    • B64D27/02—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
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • C—CHEMISTRY; METALLURGY
    • C22—METALLURGY; FERROUS OR NON-FERROUS ALLOYS; TREATMENT OF ALLOYS OR NON-FERROUS METALS
    • C22C—ALLOYS
    • C22C49/00—Alloys containing metallic or non-metallic fibres or filaments
    • C22C49/02—Alloys containing metallic or non-metallic fibres or filaments characterised by the matrix material
    • C22C49/10—Refractory metals
    • C22C49/11—Titanium
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B22—CASTING; POWDER METALLURGY
    • B22F—WORKING METALLIC POWDER; MANUFACTURE OF ARTICLES FROM METALLIC POWDER; MAKING METALLIC POWDER; APPARATUS OR DEVICES SPECIALLY ADAPTED FOR METALLIC POWDER
    • B22F2998/00—Supplementary information concerning processes or compositions relating to powder metallurgy
    • B22F2998/10—Processes characterised by the sequence of their steps

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Materials Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Metallurgy (AREA)
  • Organic Chemistry (AREA)
  • Manufacture Of Alloys Or Alloy Compounds (AREA)
FR0903696A 2009-07-28 2009-07-28 Poutre de suspension annulaire de turbomoteur a la structure d'un aeronef Active FR2948633B1 (fr)

Priority Applications (8)

Application Number Priority Date Filing Date Title
FR0903696A FR2948633B1 (fr) 2009-07-28 2009-07-28 Poutre de suspension annulaire 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
EP10737561.0A EP2459446B1 (fr) 2009-07-28 2010-07-27 Poutre de suspension de turbomoteur a la structure d'un aeronef
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
CA2768085A CA2768085C (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
US13/387,534 US9321537B2 (en) 2009-07-28 2010-07-27 Beam for suspending a turboshaft engine from an aircraft structure
PCT/EP2010/060856 WO2011012603A2 (fr) 2009-07-28 2010-07-27 Poutre de suspension de turbomoteur a la structure d'un aeronef

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0903696A FR2948633B1 (fr) 2009-07-28 2009-07-28 Poutre de suspension annulaire de turbomoteur a la structure d'un aeronef

Publications (2)

Publication Number Publication Date
FR2948633A1 FR2948633A1 (fr) 2011-02-04
FR2948633B1 true FR2948633B1 (fr) 2011-09-23

Family

ID=42060581

Family Applications (1)

Application Number Title Priority Date Filing Date
FR0903696A Active FR2948633B1 (fr) 2009-07-28 2009-07-28 Poutre de suspension annulaire de turbomoteur a la structure d'un aeronef

Country Status (1)

Country Link
FR (1) FR2948633B1 (fr)

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2753140A (en) * 1951-07-28 1956-07-03 United Aircraft Corp Engine mount
US3222017A (en) * 1964-03-30 1965-12-07 Gen Electric Engine mounting
US5501906A (en) * 1994-08-22 1996-03-26 Minnesota Mining And Manufacturing Company Ceramic fiber tow reinforced metal matrix composite
GB2303884B (en) * 1995-04-13 1999-07-14 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
US5660526A (en) * 1995-06-05 1997-08-26 Allison Engine Company, Inc. Gas turbine rotor with remote support rings
US6401448B1 (en) * 2000-08-31 2002-06-11 General Electric Company System for mounting aircraft engines
WO2002022296A2 (fr) * 2000-09-11 2002-03-21 Allison Advanced Development Company Tole rainuree mecaniquement et procede de production
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion

Also Published As

Publication number Publication date
FR2948633A1 (fr) 2011-02-04

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