DE602004000283D1 - Vorrichtung für die Hinteraufhängung eines Flugzeugtriebwerkes mit Verbindungsstangen und Hebel mit Bumerangform - Google Patents

Vorrichtung für die Hinteraufhängung eines Flugzeugtriebwerkes mit Verbindungsstangen und Hebel mit Bumerangform

Info

Publication number
DE602004000283D1
DE602004000283D1 DE602004000283T DE602004000283T DE602004000283D1 DE 602004000283 D1 DE602004000283 D1 DE 602004000283D1 DE 602004000283 T DE602004000283 T DE 602004000283T DE 602004000283 T DE602004000283 T DE 602004000283T DE 602004000283 D1 DE602004000283 D1 DE 602004000283D1
Authority
DE
Germany
Prior art keywords
lever
connecting rods
rear suspension
aircraft engine
boomerang shape
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.)
Expired - Fee Related
Application number
DE602004000283T
Other languages
English (en)
Other versions
DE602004000283T2 (de
Inventor
Philippe Loewenstein
Frederic Jean-Marc Darcy
Marc Tesniere
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
Application filed by SNECMA SAS filed Critical SNECMA SAS
Publication of DE602004000283D1 publication Critical patent/DE602004000283D1/de
Application granted granted Critical
Publication of DE602004000283T2 publication Critical patent/DE602004000283T2/de
Expired - Fee Related 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
    • 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
    • B64D27/406—Suspension arrangements specially adapted for supporting thrust loads, e.g. thrust links

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Pivots And Pivotal Connections (AREA)
  • Transmission Devices (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Clamps And Clips (AREA)
  • Load-Engaging Elements For Cranes (AREA)
  • Supercharger (AREA)
DE602004000283T 2003-06-30 2004-06-25 Vorrichtung für die Hinteraufhängung eines Flugzeugtriebwerkes mit Verbindungsstangen und Hebel mit Bumerangform Expired - Fee Related DE602004000283T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
FR0307893 2003-06-30
FR0307893A FR2856656B1 (fr) 2003-06-30 2003-06-30 Suspension arriere de moteur d'avion avec bielles de reprise de poussee et palonnier en forme de boomerang

Publications (2)

Publication Number Publication Date
DE602004000283D1 true DE602004000283D1 (de) 2006-02-02
DE602004000283T2 DE602004000283T2 (de) 2006-08-31

Family

ID=33427637

Family Applications (1)

Application Number Title Priority Date Filing Date
DE602004000283T Expired - Fee Related DE602004000283T2 (de) 2003-06-30 2004-06-25 Vorrichtung für die Hinteraufhängung eines Flugzeugtriebwerkes mit Verbindungsstangen und Hebel mit Bumerangform

Country Status (9)

Country Link
US (1) US7021585B2 (de)
EP (1) EP1493663B1 (de)
JP (1) JP2005022641A (de)
BR (1) BRPI0402464A (de)
CA (1) CA2472312A1 (de)
DE (1) DE602004000283T2 (de)
ES (1) ES2253728T3 (de)
FR (1) FR2856656B1 (de)
RU (1) RU2004119904A (de)

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FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
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
FR2891804B1 (fr) * 2005-10-12 2009-05-01 Airbus France Sas Systeme d'ecrou et mat d'accrochage de moteur d'aeronef comprenant un tel systeme
FR2892706B1 (fr) * 2005-10-31 2009-04-24 Airbus France Sas Dispositif d'attache avant d'un turboreacteur a un mat de fixation d'un aeronef
FR2900906B1 (fr) * 2006-05-09 2009-01-09 Airbus France Sas Systeme de fixation tolerant aux dommages pour moteur d'aeronef
FR2903382B1 (fr) * 2006-07-10 2008-10-10 Airbus France Sas Dispositif d'accrochage d'un moteur d'aeronef comportant deux bielles de reprise de poussee a emboitement transversal
FR2914907B1 (fr) * 2007-04-16 2009-10-30 Snecma Sa Suspension souple avec peigne pour turbomoteur
FR2915175B1 (fr) * 2007-04-20 2009-07-17 Airbus France Sa Mat d'accrochage de moteur pour aeronef disposant d'une poutre d'attache moteur arriere deportee du caisson
FR2917713B1 (fr) * 2007-06-21 2009-09-25 Airbus France Sas Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif.
FR2918644B1 (fr) * 2007-07-09 2009-10-23 Airbus France Sas Mat d'accrochage de moteur pour aeronef disposant d'un palonnier articule en quatre points.
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
US11486311B2 (en) 2007-08-01 2022-11-01 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11242805B2 (en) 2007-08-01 2022-02-08 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US8844265B2 (en) 2007-08-01 2014-09-30 United Technologies Corporation Turbine section of high bypass turbofan
US11149650B2 (en) 2007-08-01 2021-10-19 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US20150377123A1 (en) 2007-08-01 2015-12-31 United Technologies Corporation Turbine section of high bypass turbofan
FR2920138B1 (fr) * 2007-08-24 2010-03-12 Airbus France Dispositif d'accrochage de moteur d'aeronef comportant un dispositif de reprise des efforts de poussee a encombrement reduit
FR2924094B1 (fr) * 2007-11-23 2010-01-15 Snecma Turboreacteur suspendu a un pylone d'aeronef
FR2924684B1 (fr) * 2007-12-07 2010-01-01 Snecma Suspension d'un turboreacteur a un aeronef
FR2925016B1 (fr) * 2007-12-12 2010-06-18 Snecma Suspension d'un turboreacteur a un aeronef
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
FR2926536B1 (fr) * 2008-01-23 2010-07-30 Snecma Accrochage d'un systeme propulsif a un element de structure d'un aeronef
US8826641B2 (en) * 2008-01-28 2014-09-09 United Technologies Corporation Thermal management system integrated pylon
US9234481B2 (en) * 2008-01-25 2016-01-12 United Technologies Corporation Shared flow thermal management system
US8167237B2 (en) 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
DE102008021431A1 (de) * 2008-04-29 2009-11-12 Airbus Deutschland Gmbh Flugzeug mit einer Energie-Versorgungsvorrichtung
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8800914B2 (en) 2008-06-02 2014-08-12 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US20140174056A1 (en) 2008-06-02 2014-06-26 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
GB0810589D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
GB0810585D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
GB0810791D0 (en) * 2008-06-13 2008-07-23 Rolls Royce Plc Thrust mounting arrangement
GB0902909D0 (en) * 2009-02-23 2009-04-08 Rolls Royce Plc A thrust mount arrangement for an aircraft engine
FR2952150B1 (fr) * 2009-11-02 2012-02-24 Airbus Operations Sas Bielle structurale comportant un mode filtrant des vibrations
FR2959210B1 (fr) * 2010-04-21 2013-08-23 Snecma Palonnier de suspension de turboreacteur d'aeronef et suspension avec accroche-soufflante ainsi equipee
KR101767071B1 (ko) * 2010-06-14 2017-08-10 로오드 코포레이션 헬리콥터 엔진 장착 시스템 및 방법
FR2965549B1 (fr) * 2010-10-01 2013-07-05 Airbus Operations Sas Dispositif de reprise de poussee a bielles pour mat d'accrochage d'un moteur d'aeronef, integrant trois rotules alignees
FR2965796B1 (fr) * 2010-10-07 2013-06-07 Snecma Suspension d'un moteur a un mat d'aeronef comportant un arceau de suspension
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
FR2981047B1 (fr) * 2011-10-06 2013-10-25 Aircelle Sa Ensemble propulsif d'aeronef
US9016623B2 (en) * 2011-11-30 2015-04-28 The Boeing Company Jam protection and alleviation for control surface linkage mechanisms
US20140084129A1 (en) * 2012-09-27 2014-03-27 United Technologies Corporation Assembly for mounting a turbine engine case to a pylon
US8979020B2 (en) * 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
CA2918320C (en) 2013-07-26 2018-05-15 Mra Systems, Inc. Aircraft engine pylon
EP3058202A4 (de) 2013-10-16 2017-06-28 United Technologies Corporation Turbogebläsemotor mit gezielter modularer wirkung
CN103587709B (zh) * 2013-10-30 2016-06-01 中国运载火箭技术研究院 一种用于直升机挂载飞行器的挂架系统
GB201417202D0 (en) * 2014-09-30 2014-11-12 Rolls Royce Plc Gas Turbine Engine Mounting Arrangement
FR3032180B1 (fr) * 2015-01-30 2018-05-18 Airbus Operations Ensemble propulsif comportant un turboreacteur et un mat d'accrochage permettant une nouvelle distribution des efforts entre le turboreacteur et la voilure
FR3041996B1 (fr) * 2015-10-05 2017-10-27 Snecma Systeme de suspension de deux modules d'un ensemble propulsif
WO2018031548A1 (en) 2016-08-08 2018-02-15 Lord Corporation Mounting systems, devices, and methods for aircraft engines
FR3058986B1 (fr) * 2016-11-21 2021-04-16 Airbus Operations Sas Attache arriere d'un moteur d'aeronef comportant des temoins de rupture
FR3060069B1 (fr) * 2016-12-13 2019-05-24 Airbus Operations Sas Bielle amortissante convertible en bielle rigide
FR3086924B1 (fr) * 2018-10-08 2021-02-12 Safran Aircraft Engines Turbomachine comportant des moyens de suspension
EP3663206B1 (de) * 2018-12-06 2023-09-06 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Befestigung zum aufhängen eines flugzeugtriebwerks
US11970279B2 (en) 2020-02-21 2024-04-30 General Electric Company Control system and methods of controlling an engine-mounting link system
US11939070B2 (en) 2020-02-21 2024-03-26 General Electric Company Engine-mounting links that have an adjustable inclination angle
US11970278B2 (en) 2020-07-14 2024-04-30 General Electric Company Thrust mounts with load-balancing thrust link-lever
FR3114300A1 (fr) * 2020-09-21 2022-03-25 Airbus Operations (S.A.S.) Assemblage d’un moteur avec un mat d’aeronef
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
FR3127202A1 (fr) * 2021-09-20 2023-03-24 Airbus Operations (S.A.S.) Ensemble de motorisation d’aéronef comprenant un dispositif de reprise d’efforts de poussée

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US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
US5873547A (en) * 1997-05-20 1999-02-23 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
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
FR2830516B1 (fr) * 2001-10-04 2004-01-02 Snecma Moteurs Suspension de turboreacteur
FR2830515B1 (fr) * 2001-10-04 2004-01-30 Snecma Moteurs Suspension de turboreacteur

Also Published As

Publication number Publication date
BRPI0402464A (pt) 2005-05-24
FR2856656A1 (fr) 2004-12-31
ES2253728T3 (es) 2006-06-01
JP2005022641A (ja) 2005-01-27
US20050067528A1 (en) 2005-03-31
US7021585B2 (en) 2006-04-04
EP1493663B1 (de) 2005-12-28
FR2856656B1 (fr) 2006-12-01
DE602004000283T2 (de) 2006-08-31
CA2472312A1 (fr) 2004-12-30
RU2004119904A (ru) 2005-12-10
EP1493663A1 (de) 2005-01-05

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee