FR2217549A1 - - Google Patents

Info

Publication number
FR2217549A1
FR2217549A1 FR7404967A FR7404967A FR2217549A1 FR 2217549 A1 FR2217549 A1 FR 2217549A1 FR 7404967 A FR7404967 A FR 7404967A FR 7404967 A FR7404967 A FR 7404967A FR 2217549 A1 FR2217549 A1 FR 2217549A1
Authority
FR
France
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.)
Withdrawn
Application number
FR7404967A
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.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2217549A1 publication Critical patent/FR2217549A1/fr
Withdrawn legal-status Critical Current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; 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
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/20—Mounting or supporting of plant; Accommodating heat expansion or creep
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
FR7404967A 1973-02-14 1974-02-14 Withdrawn FR2217549A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00332435A US3844115A (en) 1973-02-14 1973-02-14 Load distributing thrust mount

Publications (1)

Publication Number Publication Date
FR2217549A1 true FR2217549A1 (fr) 1974-09-06

Family

ID=23298229

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7404967A Withdrawn FR2217549A1 (fr) 1973-02-14 1974-02-14

Country Status (8)

Country Link
US (1) US3844115A (fr)
JP (1) JPS49112399A (fr)
BE (1) BE811011A (fr)
CA (1) CA1016523A (fr)
DE (1) DE2406302A1 (fr)
FR (1) FR2217549A1 (fr)
GB (1) GB1455603A (fr)
IT (1) IT1007374B (fr)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2755942A1 (fr) * 1996-11-21 1998-05-22 Snecma Suspension avant redondante pour turbomachine
FR2755943A1 (fr) * 1996-11-21 1998-05-22 Snecma Suspension avant redondante pour turbomachine
FR2755944A1 (fr) * 1996-11-21 1998-05-22 Snecma Suspension avant redondante pour turbomachine
FR2915177A1 (fr) * 2007-04-20 2008-10-24 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif
EP2256303A2 (fr) * 2009-03-24 2010-12-01 Rolls-Royce plc Agencement de boîtier

Families Citing this family (52)

* Cited by examiner, † Cited by third party
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GB1521847A (en) * 1976-04-30 1978-08-16 Rolls Royce Attachment for attaching jet propulsion engines to vehicle structure
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
GB1599730A (en) * 1978-05-30 1981-10-07 Greenmeadow Engs Ltd Attachment of masses to aircraft and spacecraft
US4221227A (en) * 1978-08-09 1980-09-09 Mars, Incorporated Separable coin storage tube assembly
US4438625A (en) * 1978-10-26 1984-03-27 Rice Ivan G Reheat gas turbine combined with steam turbine
FR2516609A1 (fr) * 1981-11-19 1983-05-20 Snecma Dispositif de fixation de deux pieces de revolution en materiaux ayant des coefficients de dilatation differents
GB8300748D0 (en) * 1983-01-12 1983-02-16 British Aerospace Power plant attachment for aircraft wings
US4528811A (en) * 1983-06-03 1985-07-16 General Electric Co. Closed-cycle gas turbine chemical processor
US4658579A (en) * 1983-07-14 1987-04-21 United Technologies Corporation Load sharing for engine nacelle
US4603821A (en) * 1983-12-30 1986-08-05 The Boeing Company System for mounting a jet engine
FR2560854B1 (fr) * 1984-03-07 1986-09-12 Snecma Capotages structuraux participant a la rigidite d'ensemble d'un turboreacteur
US4725019A (en) * 1986-08-11 1988-02-16 The Boeing Company Aircraft engine mount with vertical vibration isolation
GB2220034B (en) * 1988-06-22 1992-12-02 Rolls Royce Plc Aerodynamic loading in gas turbine engines
US5174525A (en) * 1991-09-26 1992-12-29 General Electric Company Structure for eliminating lift load bending in engine core of turbofan
US5320307A (en) * 1992-03-25 1994-06-14 General Electric Company Aircraft engine thrust mount
GB2271390B (en) * 1992-10-12 1995-07-05 Rolls Royce Plc Mounting for a gas turbine engine
US5452575A (en) * 1993-09-07 1995-09-26 General Electric Company Aircraft gas turbine engine thrust mount
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
US5467941A (en) * 1993-12-30 1995-11-21 The Boeing Company Pylon and engine installation for ultra-high by-pass turbo-fan engines
US5860623A (en) * 1995-05-03 1999-01-19 The Boeing Company Three link failsafe engine 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
US6659878B2 (en) * 2001-03-30 2003-12-09 General Electric Company Method and apparatus for coupling male threads to female threads
US6708482B2 (en) * 2001-11-29 2004-03-23 General Electric Company Aircraft engine with inter-turbine engine frame
FR2836672B1 (fr) * 2002-03-04 2004-06-04 Airbus France Mat d'accrochage d'un moteur sous une voilure d'aeronef
GB0607991D0 (en) * 2006-04-22 2006-05-31 Rolls Royce Plc Aeroengine mounting
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
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.
US8256707B2 (en) * 2007-08-01 2012-09-04 United Technologies Corporation Engine mounting configuration for a turbofan gas turbine engine
US8118251B2 (en) * 2008-01-18 2012-02-21 United Technologies Corporation Mounting system for a gas turbine engine
US8347500B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitney Canada Corp. Method of assembly and disassembly of a gas turbine mid turbine frame
US8099962B2 (en) * 2008-11-28 2012-01-24 Pratt & Whitney Canada Corp. Mid turbine frame system and radial locator for radially centering a bearing for gas turbine engine
US8091371B2 (en) * 2008-11-28 2012-01-10 Pratt & Whitney Canada Corp. Mid turbine frame for gas turbine engine
US20100132371A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8061969B2 (en) * 2008-11-28 2011-11-22 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8245518B2 (en) * 2008-11-28 2012-08-21 Pratt & Whitney Canada Corp. Mid turbine frame system for gas turbine engine
US8347635B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitey Canada Corp. Locking apparatus for a radial locator for gas turbine engine mid turbine frame
US20100132377A1 (en) * 2008-11-28 2010-06-03 Pratt & Whitney Canada Corp. Fabricated itd-strut and vane ring for gas turbine engine
US8182204B2 (en) * 2009-04-24 2012-05-22 Pratt & Whitney Canada Corp. Deflector for a gas turbine strut and vane assembly
US8348191B2 (en) * 2010-07-14 2013-01-08 Spirit Aerosystems, Inc. Fail-safe aircraft engine mounting apparatus
FR2966125B1 (fr) * 2010-10-15 2013-04-26 Aircelle Sa Ensemble d'accrochage d'une suspension d'un ensemble propulsif d'aeronef
FR2969578B1 (fr) * 2010-12-27 2013-02-08 Snecma Dispositif de suspension d'un turboreacteur
US10132197B2 (en) 2015-04-20 2018-11-20 General Electric Company Shroud assembly and shroud for gas turbine engine
US10464684B2 (en) 2016-02-01 2019-11-05 Bell Textron Inc. Tapered sockets for aircraft engine mount assemblies
US10384790B2 (en) 2016-02-01 2019-08-20 Bell Textron Inc. Engine mount assemblies for aircraft
US10723471B2 (en) 2017-06-14 2020-07-28 General Electric Company Method and system for mounting an aircraft engine
US10882629B2 (en) * 2018-08-07 2021-01-05 The Boeing Company Roll load bearing aircraft propulsor moveable panel systems and methods
CN109592051A (zh) * 2018-12-03 2019-04-09 江西洪都航空工业集团有限责任公司 一种发动机安装结构
US11273923B2 (en) 2019-07-12 2022-03-15 Spirit Aerosystems, Inc. Fail-safe engine support system
US11970278B2 (en) 2020-07-14 2024-04-30 General Electric Company Thrust mounts with load-balancing thrust link-lever
US11428160B2 (en) 2020-12-31 2022-08-30 General Electric Company Gas turbine engine with interdigitated turbine and gear assembly
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

Family Cites Families (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2457340A (en) * 1943-12-30 1948-12-28 Bristol Aeroplane Co Ltd Mounting for vibratory bodies
US2477501A (en) * 1945-02-24 1949-07-26 United Aircraft Corp Engine suspension means
US2720370A (en) * 1950-12-04 1955-10-11 Hasbrouck Augustus Resilient engine mounting system, including flexible self-compensating joints
GB798832A (en) * 1955-02-04 1958-07-30 Rolls Royce Improvements in or relating to flexible mounting systems for vibrating bodies
US3188808A (en) * 1962-12-03 1965-06-15 Cooper Bessemer Corp Gas turbine thrust compensating device
US3675418A (en) * 1970-11-19 1972-07-11 United Aircraft Corp Jet engine force frame

Cited By (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5871176A (en) * 1996-11-21 1999-02-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Redundant front suspension system for a turboshaft engine
FR2755942A1 (fr) * 1996-11-21 1998-05-22 Snecma Suspension avant redondante pour turbomachine
FR2755944A1 (fr) * 1996-11-21 1998-05-22 Snecma Suspension avant redondante pour turbomachine
EP0844172A1 (fr) * 1996-11-21 1998-05-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Suspension avant redondante pour turbomachine
EP0844174A1 (fr) * 1996-11-21 1998-05-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Suspension avant redondante pour turbomachine
EP0844173A1 (fr) * 1996-11-21 1998-05-27 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Suspension avant redondante pour turbomachine
FR2755943A1 (fr) * 1996-11-21 1998-05-22 Snecma Suspension avant redondante pour turbomachine
US5871175A (en) * 1996-11-21 1999-02-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation Redundant front suspension system for a turboshaft engine
US5871177A (en) * 1996-11-21 1999-02-16 Societe Nationale D'etude Et De Construction De Moteurs D'aviation "Snecma" Redundant front suspension system for a turboshaft engine
FR2915177A1 (fr) * 2007-04-20 2008-10-24 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif
WO2008135366A1 (fr) * 2007-04-20 2008-11-13 Airbus France Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif
US8146856B2 (en) 2007-04-20 2012-04-03 Airbus Operations Sas Device for attaching an aircraft engine and aircraft comprising at least one such device
EP2256303A2 (fr) * 2009-03-24 2010-12-01 Rolls-Royce plc Agencement de boîtier
EP2256303A3 (fr) * 2009-03-24 2014-12-31 Rolls-Royce plc Agencement de boîtier

Also Published As

Publication number Publication date
JPS49112399A (fr) 1974-10-25
DE2406302A1 (de) 1974-08-22
US3844115A (en) 1974-10-29
BE811011A (fr) 1974-05-29
GB1455603A (en) 1976-11-17
IT1007374B (it) 1976-10-30
CA1016523A (en) 1977-08-30

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Legal Events

Date Code Title Description
ST Notification of lapse