DE60021046D1 - Aufhängevorrichtung eines Turbotriebwerks - Google Patents

Aufhängevorrichtung eines Turbotriebwerks

Info

Publication number
DE60021046D1
DE60021046D1 DE60021046T DE60021046T DE60021046D1 DE 60021046 D1 DE60021046 D1 DE 60021046D1 DE 60021046 T DE60021046 T DE 60021046T DE 60021046 T DE60021046 T DE 60021046T DE 60021046 D1 DE60021046 D1 DE 60021046D1
Authority
DE
Germany
Prior art keywords
suspension device
turbo engine
turbo
engine
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.)
Expired - Lifetime
Application number
DE60021046T
Other languages
English (en)
Other versions
DE60021046T2 (de
Inventor
Olivier Jean-Francois Cazenave
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of DE60021046D1 publication Critical patent/DE60021046D1/de
Publication of DE60021046T2 publication Critical patent/DE60021046T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B64D27/40—
    • B64D27/402—
    • B64D27/404—
    • B64D27/406—
DE60021046T 1999-11-20 2000-11-08 Aufhängevorrichtung eines Turbotriebwerks Expired - Lifetime DE60021046T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GBGB9927425.0A GB9927425D0 (en) 1999-11-20 1999-11-20 A gas turbine engine mounting arrangement
GB9927425 1999-11-20

Publications (2)

Publication Number Publication Date
DE60021046D1 true DE60021046D1 (de) 2005-08-04
DE60021046T2 DE60021046T2 (de) 2005-12-22

Family

ID=10864828

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60021046T Expired - Lifetime DE60021046T2 (de) 1999-11-20 2000-11-08 Aufhängevorrichtung eines Turbotriebwerks

Country Status (4)

Country Link
US (1) US6474597B1 (de)
EP (1) EP1103463B1 (de)
DE (1) DE60021046T2 (de)
GB (1) GB9927425D0 (de)

Families Citing this family (49)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
GB2375513B (en) * 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
FR2825976B1 (fr) * 2001-06-13 2003-09-05 Eads Airbus Sa Dispositif de reprise d'efforts generes par un moteur d'aeronef
FR2830515B1 (fr) * 2001-10-04 2004-01-30 Snecma Moteurs Suspension de turboreacteur
GB0413276D0 (en) * 2004-06-14 2004-07-14 Rolls Royce Plc Load reduced engine mount
GB0507721D0 (en) * 2005-04-16 2005-05-25 Rolls Royce Plc Gas turbine engine mounting arrangement
FR2891256B1 (fr) * 2005-09-27 2007-10-26 Airbus France Sas Dispositif d'accrochage d'un moteur interpose entre une voilure d'aeronef et ledit moteur
GB0607991D0 (en) * 2006-04-22 2006-05-31 Rolls Royce Plc Aeroengine mounting
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.
US11149650B2 (en) 2007-08-01 2021-10-19 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
US11346289B2 (en) 2007-08-01 2022-05-31 Raytheon Technologies Corporation Turbine section of high bypass turbofan
US11486311B2 (en) 2007-08-01 2022-11-01 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
US8844265B2 (en) 2007-08-01 2014-09-30 United 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
US8950702B2 (en) * 2008-01-18 2015-02-10 United Technologies Corporation Pylon and engine mount configuration
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
US8167237B2 (en) 2008-03-21 2012-05-01 United Technologies Corporation Mounting system for a gas turbine engine
US8695920B2 (en) 2008-06-02 2014-04-15 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
US20140174056A1 (en) 2008-06-02 2014-06-26 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
US8128021B2 (en) * 2008-06-02 2012-03-06 United Technologies Corporation Engine mount system for a turbofan gas turbine engine
US8807477B2 (en) 2008-06-02 2014-08-19 United Technologies Corporation Gas turbine engine compressor arrangement
US8511605B2 (en) 2008-06-02 2013-08-20 United Technologies Corporation Gas turbine engine with low stage count low pressure turbine
GB0810589D0 (en) * 2008-06-11 2008-07-16 Rolls Royce Plc Engine mounting arrangement
GB0902909D0 (en) * 2009-02-23 2009-04-08 Rolls Royce Plc A thrust mount arrangement for an aircraft engine
FR2975077B1 (fr) * 2011-05-12 2013-07-05 Airbus Operations Sas Dispositif d'accrochage d'un moteur d'aeronef, comprenant des cales de serrage d'attache moteur a effet de coin
US8882029B2 (en) 2011-07-14 2014-11-11 United Technologies Corporation Fire resistant structural mount yoke and system
US9828105B2 (en) 2011-08-24 2017-11-28 United Technologies Corporation Nacelle assembly having integrated afterbody mount case
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
US8561942B2 (en) 2012-02-06 2013-10-22 United Technologies Corporation Gas turbine engine mounting structure with secondary load paths
US9637241B2 (en) * 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
US9217337B2 (en) * 2012-05-10 2015-12-22 United Technologies Corporation Adjustable engine mount
GB201306674D0 (en) * 2013-04-12 2013-05-29 Rolls Royce Plc Rigid Raft for a Gas Turbine Engine
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
WO2015088619A2 (en) 2013-10-16 2015-06-18 United Technologies Corporation Geared turbofan engine with targeted modular efficiency
FR3013077B1 (fr) * 2013-11-08 2015-11-20 Snecma Turbomachine comportant des moyens de support d'au moins un equipement
FR3014996B1 (fr) * 2013-12-16 2016-11-04 Microturbo Suspension d'un element tubulaire dans un compartiment d'aeronef
FR3020343B1 (fr) * 2014-04-23 2017-10-27 Airbus Operations Sas Ensemble pour aeronef comprenant une structure primaire de mat d'accrochage constituee par trois elements independants
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
GB201811281D0 (en) * 2018-07-10 2018-08-29 Rolls Royce Plc A geared turbofan bas turbine engine mounting arrangement
FR3096348B1 (fr) * 2019-05-21 2021-10-15 Airbus Operations Sas Systeme d’attache moteur avant pour un moteur d’aeronef comportant des systemes de bielles a deux bielles
FR3096350B1 (fr) * 2019-05-21 2021-07-09 Airbus Operations Sas Systeme d’attache moteur avant pour un moteur d’aeronef comportant une poutre realisee en trois parties
FR3096344A1 (fr) * 2019-05-21 2020-11-27 Airbus Operations Systeme d’attache moteur avant pour un moteur d’aeronef comportant une fixation directe entre le mat reacteur et le moteur
FR3096347B1 (fr) * 2019-05-21 2022-06-24 Airbus Operations Sas Systeme d’attache moteur avant pour un moteur d’aeronef comportant une poutre realisee en deux parties
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
GB202117778D0 (en) * 2021-12-09 2022-01-26 Rolls Royce Plc Support structure for attaching a gas turbine engine to an aircraft pylon

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1236917A (en) * 1967-06-14 1971-06-23 Rolls Royce Improvements in or relating to means for supporting a gas turbine engine in an aircraft
GB1521847A (en) 1976-04-30 1978-08-16 Rolls Royce Attachment for attaching jet propulsion engines to vehicle structure
US4603821A (en) 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
GB2224707B (en) 1988-11-12 1992-06-10 Rolls Royce Plc Improvements in or relating to engine mounting integrity
DE69012071T2 (de) 1989-12-05 1995-04-13 Rolls Royce Plc Ausfallsichere Haltevorrichtung für Treibwerke.
US5320307A (en) 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
US5649417A (en) 1995-03-24 1997-07-22 The Boeing Company Fail-safe engine mount system
FR2755942B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
FR2755944B1 (fr) 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
FR2755943B1 (fr) * 1996-11-21 1998-12-24 Snecma Suspension avant redondante pour turbomachine
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

Also Published As

Publication number Publication date
DE60021046T2 (de) 2005-12-22
EP1103463A1 (de) 2001-05-30
GB9927425D0 (en) 2000-01-19
US6474597B1 (en) 2002-11-05
EP1103463B1 (de) 2005-06-29

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Legal Events

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