BE811011A - Dispositif pour appliquer la poussee propulsive d'un moteur a turbine a gaz a un vehicule - Google Patents

Dispositif pour appliquer la poussee propulsive d'un moteur a turbine a gaz a un vehicule

Info

Publication number
BE811011A
BE811011A BE140888A BE140888A BE811011A BE 811011 A BE811011 A BE 811011A BE 140888 A BE140888 A BE 140888A BE 140888 A BE140888 A BE 140888A BE 811011 A BE811011 A BE 811011A
Authority
BE
Belgium
Prior art keywords
applying
vehicle
gas turbine
turbine engine
propulsive thrust
Prior art date
Application number
BE140888A
Other languages
English (en)
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 filed Critical
Publication of BE811011A publication Critical patent/BE811011A/fr

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
    • 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
    • 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)
BE140888A 1973-02-14 1974-02-14 Dispositif pour appliquer la poussee propulsive d'un moteur a turbine a gaz a un vehicule BE811011A (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
BE811011A true BE811011A (fr) 1974-05-29

Family

ID=23298229

Family Applications (1)

Application Number Title Priority Date Filing Date
BE140888A BE811011A (fr) 1973-02-14 1974-02-14 Dispositif pour appliquer la poussee propulsive d'un moteur a turbine a gaz a un vehicule

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)

Families Citing this family (59)

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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
US4428189A (en) 1980-04-02 1984-01-31 United Technologies Corporation Case deflection control in aircraft gas turbine engines
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
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
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
FR2915177B1 (fr) * 2007-04-20 2009-07-10 Airbus France Sa Dispositif d'accrochage de moteur d'aeronef et aeronef comportant au moins un tel dispositif
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
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
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
US8347500B2 (en) * 2008-11-28 2013-01-08 Pratt & Whitney Canada Corp. Method of assembly and disassembly of a gas turbine 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
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
GB0904970D0 (en) * 2009-03-24 2009-05-06 Rolls Royce Plc A casing arrangement
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
US10336459B2 (en) 2016-02-01 2019-07-02 Bell Helicopter Textron Inc. Clamped splines 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
US20260035082A1 (en) * 2024-08-01 2026-02-05 Rtx Corporation Low spool electrical machine arrangements for hybrid-electric engines

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

Also Published As

Publication number Publication date
DE2406302A1 (de) 1974-08-22
CA1016523A (en) 1977-08-30
JPS49112399A (fr) 1974-10-25
FR2217549A1 (fr) 1974-09-06
GB1455603A (en) 1976-11-17
IT1007374B (it) 1976-10-30
US3844115A (en) 1974-10-29

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