ATE312017T1 - Triebwerkaufhängungsvorrichtung an einem luftfahrzeug - Google Patents

Triebwerkaufhängungsvorrichtung an einem luftfahrzeug

Info

Publication number
ATE312017T1
ATE312017T1 AT02290284T AT02290284T ATE312017T1 AT E312017 T1 ATE312017 T1 AT E312017T1 AT 02290284 T AT02290284 T AT 02290284T AT 02290284 T AT02290284 T AT 02290284T AT E312017 T1 ATE312017 T1 AT E312017T1
Authority
AT
Austria
Prior art keywords
fittings
attachment structure
nacelle stub
engine
aircraft
Prior art date
Application number
AT02290284T
Other languages
English (en)
Inventor
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 ATE312017T1 publication Critical patent/ATE312017T1/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
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Connection Of Plates (AREA)
  • Vibration Prevention Devices (AREA)
  • Agricultural Machines (AREA)
  • Snaps, Bayonet Connections, Set Pins, And Snap Rings (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Vehicle Body Suspensions (AREA)
AT02290284T 2001-02-08 2002-02-06 Triebwerkaufhängungsvorrichtung an einem luftfahrzeug ATE312017T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR0101701A FR2820402B1 (fr) 2001-02-08 2001-02-08 Dispositif d'accrochage d'un moteur sur un aeronef

Publications (1)

Publication Number Publication Date
ATE312017T1 true ATE312017T1 (de) 2005-12-15

Family

ID=8859767

Family Applications (1)

Application Number Title Priority Date Filing Date
AT02290284T ATE312017T1 (de) 2001-02-08 2002-02-06 Triebwerkaufhängungsvorrichtung an einem luftfahrzeug

Country Status (7)

Country Link
US (1) US6601796B2 (de)
EP (1) EP1231138B1 (de)
AT (1) ATE312017T1 (de)
CA (1) CA2369206C (de)
DE (1) DE60207765T2 (de)
ES (1) ES2254616T3 (de)
FR (1) FR2820402B1 (de)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2830516B1 (fr) * 2001-10-04 2004-01-02 Snecma Moteurs Suspension de turboreacteur
US6607165B1 (en) * 2002-06-28 2003-08-19 General Electric Company Aircraft engine mount with single thrust link
FR2855494B1 (fr) * 2003-05-27 2006-09-22 Snecma Moteurs Dispositif d'accrocharge arriere de moteur d'avion
US6843449B1 (en) * 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system
FR2867155B1 (fr) 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2873986B1 (fr) * 2004-08-04 2007-12-21 Airbus France Sas Ensemble moteur pour aeronef
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
GB0507721D0 (en) * 2005-04-16 2005-05-25 Rolls Royce Plc Gas turbine engine mounting arrangement
FR2887521B1 (fr) * 2005-06-28 2007-08-17 Airbus France Sas Ensemble moteur pour aeronef comprenant un moteur ainsi qu'un dispositif d'accrochage d'un tel moteur
FR2887853B1 (fr) * 2005-06-29 2007-08-17 Airbus France Sas Attache moteur pour aeronef destinee a etre interposee entre un moteur et un mat d'accrochage
US20070057128A1 (en) * 2005-09-14 2007-03-15 Honeywell International, Inc. Auxiliary power unit case flange to plate adapter
FR2891253B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
FR2900906B1 (fr) * 2006-05-09 2009-01-09 Airbus France Sas Systeme de fixation tolerant aux dommages pour moteur d'aeronef
ATE430691T1 (de) * 2006-10-24 2009-05-15 Eads Constr Aeronauticas Sa Luftbetankungssonde mit ausfallsicherem roll- und nickscharnier
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
FR2916424B1 (fr) * 2007-05-23 2009-08-21 Airbus France Sa Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant
WO2008150202A1 (en) * 2007-06-08 2008-12-11 Volvo Aero Corporation A structure for transferring loads at a gas turbine engine, and an engine and an aircraft with such a structure
US8950702B2 (en) * 2008-01-18 2015-02-10 United Technologies Corporation Pylon and engine mount configuration
US8047469B2 (en) * 2008-03-01 2011-11-01 The Boeing Company Airframe attachment fitting
GB0810589D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
CN103318415B (zh) * 2012-03-21 2015-10-14 中国航空工业集团公司沈阳发动机设计研究所 一种航空发动机安装维护用升降装置
US20140084129A1 (en) * 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon
GB201315968D0 (en) * 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
FR3027873B1 (fr) * 2014-11-03 2016-12-23 Airbus Operations Sas Attache moteur avant pour un moteur d'aeronef
FR3096353B1 (fr) * 2019-05-21 2022-02-11 Airbus Operations Sas Systeme d’attache moteur avant pour un moteur d’aeronef comportant une poutre realisee en deux parties
CN113237403A (zh) * 2021-03-26 2021-08-10 陕西飞机工业有限责任公司 发动机发房下盖支架检测装置及方法
FR3128205A1 (fr) * 2021-10-14 2023-04-21 Airbus Operations Assemblage d’un mat avec un moteur d’un aéronef

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5275357A (en) 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
US5620154A (en) 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
FR2770486B1 (fr) 1997-11-06 2000-01-28 Aerospatiale Dispositif d'accrochage d'un moteur sur un aeronef
FR2774358B1 (fr) * 1998-02-04 2000-04-21 Aerospatiale Dispositif d'accrochage d'un moteur d'aeronef
FR2793767B1 (fr) * 1999-05-17 2001-09-21 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef
FR2793769B1 (fr) * 1999-05-19 2001-09-07 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef a un mat
FR2806699B1 (fr) * 2000-03-22 2002-05-10 Aerospatiale Matra Airbus Dispositif de reprise de poussee apte a relier un turbomoteur et un mat d'aeronef
US6401448B1 (en) * 2000-08-31 2002-06-11 General Electric Company System for mounting aircraft engines

Also Published As

Publication number Publication date
EP1231138A1 (de) 2002-08-14
FR2820402B1 (fr) 2003-05-02
US6601796B2 (en) 2003-08-05
CA2369206C (en) 2010-06-01
CA2369206A1 (en) 2002-08-08
EP1231138B1 (de) 2005-12-07
FR2820402A1 (fr) 2002-08-09
ES2254616T3 (es) 2006-06-16
DE60207765D1 (de) 2006-01-12
US20020104924A1 (en) 2002-08-08
DE60207765T2 (de) 2006-09-07

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Legal Events

Date Code Title Description
RER Ceased as to paragraph 5 lit. 3 law introducing patent treaties