ATE423061T1 - Befestigungsvorrichtung für einen turbostrahlmotor mit einer strebe zur befestigung an einem flugzeug - Google Patents

Befestigungsvorrichtung für einen turbostrahlmotor mit einer strebe zur befestigung an einem flugzeug

Info

Publication number
ATE423061T1
ATE423061T1 AT06831287T AT06831287T ATE423061T1 AT E423061 T1 ATE423061 T1 AT E423061T1 AT 06831287 T AT06831287 T AT 06831287T AT 06831287 T AT06831287 T AT 06831287T AT E423061 T1 ATE423061 T1 AT E423061T1
Authority
AT
Austria
Prior art keywords
turbojet engine
bracket
fixing points
aircraft
fastening
Prior art date
Application number
AT06831287T
Other languages
English (en)
Inventor
Herve Marche
Original Assignee
Airbus France
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 France filed Critical Airbus France
Application granted granted Critical
Publication of ATE423061T1 publication Critical patent/ATE423061T1/de

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
    • 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)
  • Clamps And Clips (AREA)
  • Connection Of Plates (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Supercharger (AREA)
AT06831287T 2005-10-31 2006-10-24 Befestigungsvorrichtung für einen turbostrahlmotor mit einer strebe zur befestigung an einem flugzeug ATE423061T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0553304A FR2892706B1 (fr) 2005-10-31 2005-10-31 Dispositif d'attache avant d'un turboreacteur a un mat de fixation d'un aeronef

Publications (1)

Publication Number Publication Date
ATE423061T1 true ATE423061T1 (de) 2009-03-15

Family

ID=36658609

Family Applications (1)

Application Number Title Priority Date Filing Date
AT06831287T ATE423061T1 (de) 2005-10-31 2006-10-24 Befestigungsvorrichtung für einen turbostrahlmotor mit einer strebe zur befestigung an einem flugzeug

Country Status (11)

Country Link
US (1) US8366038B2 (de)
EP (1) EP1943145B1 (de)
JP (1) JP5227798B2 (de)
CN (1) CN101300172A (de)
AT (1) ATE423061T1 (de)
BR (1) BRPI0618083A2 (de)
CA (1) CA2625800C (de)
DE (1) DE602006005263D1 (de)
FR (1) FR2892706B1 (de)
RU (1) RU2398715C2 (de)
WO (1) WO2007051938A2 (de)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2924684B1 (fr) * 2007-12-07 2010-01-01 Snecma Suspension d'un turboreacteur a un aeronef
FR2981046B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
FR2989952B1 (fr) 2012-04-27 2014-04-18 Aircelle Sa Nacelle de turboreacteur a section aval
US10266273B2 (en) 2013-07-26 2019-04-23 Mra Systems, Llc Aircraft engine pylon
FR3027873B1 (fr) * 2014-11-03 2016-12-23 Airbus Operations Sas Attache moteur avant pour un moteur d'aeronef
GB201804962D0 (en) * 2018-03-28 2018-05-09 Rolls Royce Plc A geared turbofan engine mount arrangement
FR3086924B1 (fr) 2018-10-08 2021-02-12 Safran Aircraft Engines Turbomachine comportant des moyens de suspension
FR3123323B1 (fr) 2021-05-27 2024-05-03 Safran Aircraft Engines Structure de liaison et de support d’une turbomachine a un pylone d’aeronef

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4555078A (en) 1983-12-27 1985-11-26 Societe Belge D'exploitation De La Navigation Aerienne (Sabena) Apparatus for the suspension of an aircraft engine cowling
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
JPH07277290A (ja) 1994-04-11 1995-10-24 Toyota Motor Corp 航空機エンジンのマウント装置
FR2755943B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
FR2793769B1 (fr) * 1999-05-19 2001-09-07 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef a un mat
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
FR2856656B1 (fr) * 2003-06-30 2006-12-01 Snecma Moteurs Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang
FR2867156B1 (fr) * 2004-03-04 2006-06-02 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.
FR2867158B1 (fr) * 2004-03-04 2007-06-08 Airbus France Systeme de montage interpose entre un moteur d'aeronef et une structure rigide d'un mat d'accrochage fixe sous une voilure de cet aeronef.

Also Published As

Publication number Publication date
CA2625800C (fr) 2013-06-11
EP1943145A2 (de) 2008-07-16
CA2625800A1 (fr) 2007-05-10
DE602006005263D1 (de) 2009-04-02
BRPI0618083A2 (pt) 2011-08-16
US8366038B2 (en) 2013-02-05
US20090218441A1 (en) 2009-09-03
CN101300172A (zh) 2008-11-05
WO2007051938A3 (fr) 2007-07-19
RU2008121952A (ru) 2009-12-10
JP5227798B2 (ja) 2013-07-03
FR2892706A1 (fr) 2007-05-04
WO2007051938A2 (fr) 2007-05-10
JP2009513434A (ja) 2009-04-02
RU2398715C2 (ru) 2010-09-10
EP1943145B1 (de) 2009-02-18
FR2892706B1 (fr) 2009-04-24

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Legal Events

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