ATE288384T1 - Schubbefestigung eines triebwerkes an einem luftfahrzeug - Google Patents

Schubbefestigung eines triebwerkes an einem luftfahrzeug

Info

Publication number
ATE288384T1
ATE288384T1 AT02291443T AT02291443T ATE288384T1 AT E288384 T1 ATE288384 T1 AT E288384T1 AT 02291443 T AT02291443 T AT 02291443T AT 02291443 T AT02291443 T AT 02291443T AT E288384 T1 ATE288384 T1 AT E288384T1
Authority
AT
Austria
Prior art keywords
strut
engine
fittings
aircraft
bolts
Prior art date
Application number
AT02291443T
Other languages
English (en)
Inventor
Stephane Levert
Sebastien Roszak
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 ATE288384T1 publication Critical patent/ATE288384T1/de

Links

Classifications

    • B64D27/40—
    • B64D27/404—
AT02291443T 2001-06-13 2002-06-11 Schubbefestigung eines triebwerkes an einem luftfahrzeug ATE288384T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0107728A FR2825976B1 (fr) 2001-06-13 2001-06-13 Dispositif de reprise d'efforts generes par un moteur d'aeronef

Publications (1)

Publication Number Publication Date
ATE288384T1 true ATE288384T1 (de) 2005-02-15

Family

ID=8864260

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02291443T ATE288384T1 (de) 2001-06-13 2002-06-11 Schubbefestigung eines triebwerkes an einem luftfahrzeug

Country Status (7)

Country Link
US (1) US6648271B2 (de)
EP (1) EP1266826B1 (de)
AT (1) ATE288384T1 (de)
CA (1) CA2389881C (de)
DE (1) DE60202813T2 (de)
ES (1) ES2236460T3 (de)
FR (1) FR2825976B1 (de)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2887851B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891248B1 (fr) 2005-09-28 2009-05-01 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2891249B1 (fr) * 2005-09-28 2009-05-01 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891255B1 (fr) * 2006-07-07 2007-10-26 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un mat d'accrochage d'un tel moteur
FR2915176B1 (fr) * 2007-04-20 2009-07-10 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une attache moteur arriere pourvue d'un ecrou a barillet
FR2926788B1 (fr) * 2008-01-25 2010-04-02 Snecma Fixation d'un turboreacteur multiflux a un aeronef
FR2929245B1 (fr) * 2008-03-28 2010-05-14 Aircelle Sa Structure primaire d'un mat d'accrochage.
GB0810589D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
CN105392700B (zh) 2013-07-26 2018-12-18 Mra系统有限责任公司 飞行器发动机吊架
GB201315968D0 (en) * 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
FR3059982B1 (fr) * 2016-12-14 2022-07-29 Airbus Operations Sas Ensemble support pour un moteur d'aeronef

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2291091A1 (fr) * 1974-11-13 1976-06-11 Snecma Dispositif de montage sur avion d'un turboreacteur
GB2061389B (en) * 1979-10-23 1983-05-18 Rolls Royce Rod installation for a gas turbine engine
US4725019A (en) * 1986-08-11 1988-02-16 The Boeing Company Aircraft engine mount with vertical vibration isolation
FR2622930B1 (fr) * 1987-11-06 1990-03-23 Aerospatiale Capotage pour turboreacteur a double flux
US5275357A (en) 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
US5620154A (en) 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US5927644A (en) * 1997-10-08 1999-07-27 General Electric Company Double failsafe engine mount
US5921500A (en) * 1997-10-08 1999-07-13 General Electric Company Integrated failsafe engine mount
FR2770486B1 (fr) 1997-11-06 2000-01-28 Aerospatiale Dispositif d'accrochage d'un moteur sur un aeronef
US6189830B1 (en) * 1999-02-26 2001-02-20 The Boeing Company Tuned engine mounting system for jet aircraft
GB9927425D0 (en) * 1999-11-20 2000-01-19 Rolls Royce Plc A gas turbine engine mounting arrangement

Also Published As

Publication number Publication date
CA2389881A1 (en) 2002-12-13
DE60202813T2 (de) 2006-05-04
FR2825976A1 (fr) 2002-12-20
EP1266826A1 (de) 2002-12-18
EP1266826B1 (de) 2005-02-02
CA2389881C (en) 2010-04-27
FR2825976B1 (fr) 2003-09-05
DE60202813D1 (de) 2005-03-10
US20030173456A1 (en) 2003-09-18
US6648271B2 (en) 2003-11-18
ES2236460T3 (es) 2005-07-16

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Legal Events

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