FR2612271B1 - Systeme et procede de suspension pour un moteur d'aeronef - Google Patents

Systeme et procede de suspension pour un moteur d'aeronef

Info

Publication number
FR2612271B1
FR2612271B1 FR8717829A FR8717829A FR2612271B1 FR 2612271 B1 FR2612271 B1 FR 2612271B1 FR 8717829 A FR8717829 A FR 8717829A FR 8717829 A FR8717829 A FR 8717829A FR 2612271 B1 FR2612271 B1 FR 2612271B1
Authority
FR
France
Prior art keywords
suspension system
aircraft engine
aircraft
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 - Fee Related
Application number
FR8717829A
Other languages
English (en)
Other versions
FR2612271A1 (fr
Inventor
Stanley Irwin Bender
Lawrence Butler
Peter Winston Dawes
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 FR2612271A1 publication Critical patent/FR2612271A1/fr
Application granted granted Critical
Publication of FR2612271B1 publication Critical patent/FR2612271B1/fr
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Vibration Prevention Devices (AREA)
FR8717829A 1987-03-13 1987-12-21 Systeme et procede de suspension pour un moteur d'aeronef Expired - Fee Related FR2612271B1 (fr)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US07/025,541 US4875655A (en) 1987-03-13 1987-03-13 Vibration isolating engine mount
CA000567248A CA1320710C (fr) 1987-03-13 1988-05-19 Bati de moteur anti-vibratile

Publications (2)

Publication Number Publication Date
FR2612271A1 FR2612271A1 (fr) 1988-09-16
FR2612271B1 true FR2612271B1 (fr) 1993-06-11

Family

ID=25671904

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8717829A Expired - Fee Related FR2612271B1 (fr) 1987-03-13 1987-12-21 Systeme et procede de suspension pour un moteur d'aeronef

Country Status (7)

Country Link
US (1) US4875655A (fr)
JP (1) JPS63231094A (fr)
CA (1) CA1320710C (fr)
DE (1) DE3739941A1 (fr)
FR (1) FR2612271B1 (fr)
GB (1) GB2202279B (fr)
SE (1) SE8704582L (fr)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5064144A (en) * 1987-05-19 1991-11-12 The Boeing Company Engine mounting assembly
US5400196A (en) * 1992-04-30 1995-03-21 International Business Machines Corporation DASD with spindle imbalance isolation and method for producing same
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
GB2271390B (en) * 1992-10-12 1995-07-05 Rolls Royce Plc Mounting for a gas turbine engine
US5277382A (en) * 1992-10-13 1994-01-11 General Electric Company Aircraft engine forward mount
US5390878A (en) * 1993-02-09 1995-02-21 Grumman Aerospace Corporation Strain isolator assembly
US5443229A (en) * 1993-12-13 1995-08-22 General Electric Company Aircraft gas turbine engine sideways mount
FR2738034B1 (fr) 1995-08-23 1997-09-19 Snecma Dispositif de suspension d'un turbopropulseur
GB2375513B (en) * 2001-05-19 2005-03-23 Rolls Royce Plc A mounting arrangement for a gas turbine engine
US6669393B2 (en) 2001-10-10 2003-12-30 General Electric Co. Connector assembly for gas turbine engines
EP1796962A2 (fr) * 2004-09-17 2007-06-20 Aurora Flight Sciences Commande d'approche destinee a un avion a decollage et a atterrissage vertical de type tail sitter (assis sur la queue)
WO2007001371A2 (fr) * 2004-09-17 2007-01-04 Aurora Flight Sciences Systeme d'attache reacteur antivibratile, et procede se rapportant a un aeronef a soufflante canalisee
US20070221783A1 (en) * 2004-09-17 2007-09-27 Robert Parks Adaptive landing gear
US7559191B2 (en) 2004-09-17 2009-07-14 Aurora Flight Sciences Corporation Ducted spinner for engine cooling
US7441724B2 (en) * 2004-09-17 2008-10-28 Aurora Flight Sciences Corporation System and method for controlling a roll rate of a torsionally-disconnected freewing aircraft
WO2007001369A2 (fr) * 2004-09-17 2007-01-04 Aurora Flight Sciences Systeme et methode pour commander le regime d'un moteur a soufflante canalisee
US7552903B2 (en) * 2005-12-13 2009-06-30 Solar Turbines Incorporated Machine mounting system
FR2917711B1 (fr) * 2007-06-25 2010-01-15 Snecma Suspension d'un turbomoteur a la structure d'un aeronef
FR2939409B1 (fr) * 2008-12-08 2011-02-11 Airbus France Systeme de fixation entre deux composants tels qu'un moteur d'aeronef et son mat d'accrochage
FR2955311B1 (fr) * 2010-01-15 2012-03-23 Airbus Operations Sas Dispositif d'accrochage d'un turbopropulseur, de preference sous une voilure d'aeronef
FR2976914B1 (fr) * 2011-06-23 2014-12-26 Snecma Structure d'accrochage d'une turbomachine
GB201121971D0 (en) * 2011-12-21 2012-02-01 Rolls Royce Deutschland & Co Kg Accessory mounting for a gas turbine
US9212607B2 (en) 2012-07-18 2015-12-15 Spirit Aerosystems, Inc. Intermediate structure for independently de-mountable propulsion components
JP6266775B2 (ja) 2013-07-26 2018-01-24 エムアールエイ・システムズ・エルエルシー 航空機エンジンパイロン
US10518891B2 (en) * 2014-11-21 2019-12-31 General Electric Company Turbine engine assembly and method of manufacturing thereof
ES2703452T3 (es) 2015-09-23 2019-03-08 Mag Soar Sl Amortiguador de vibraciones magnético mejorado con emparejamiento de impedancia mecánica
US10385868B2 (en) * 2016-07-05 2019-08-20 General Electric Company Strut assembly for an aircraft engine
US11420755B2 (en) * 2019-08-08 2022-08-23 General Electric Company Shape memory alloy isolator for a gas turbine engine
CN112498708B (zh) * 2020-06-01 2022-02-08 重庆宗申航空发动机制造有限公司 一种航空无人机以及航空发动机安装支架

Family Cites Families (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1053209A (fr) *
US2310882A (en) * 1939-11-13 1943-02-09 Wright Aeronautical Corp Resilient engine mount
US2241408A (en) * 1940-03-06 1941-05-13 Lord Mfg Co Mounting
US2270673A (en) * 1940-08-28 1942-01-20 Lord Mfg Co Resilient mounting
US2332264A (en) * 1940-11-26 1943-10-19 Saurer Curt Motor support
US2365421A (en) * 1941-02-17 1944-12-19 Lord Mfg Co Resilient mounting
US2420452A (en) * 1944-10-02 1947-05-13 Lord Mfg Co Resilient mounting
US2753140A (en) * 1951-07-28 1956-07-03 United Aircraft Corp Engine mount
US3056569A (en) * 1954-09-29 1962-10-02 Textron Inc Airplane engine suspension system
GB798832A (en) * 1955-02-04 1958-07-30 Rolls Royce Improvements in or relating to flexible mounting systems for vibrating bodies
FR1160826A (fr) * 1956-11-12 1958-08-11 Snecma Dispositif de suspension de réacteurs
GB843655A (en) * 1957-08-19 1960-08-10 Rolls Royce Improvements in or relating to aircraft engine installations
US3085773A (en) * 1960-02-01 1963-04-16 North American Aviation Inc Adjustable engine mount
US3201069A (en) * 1962-05-31 1965-08-17 Haskin Simon Jet-propelled aircraft engine mounting
US3222017A (en) * 1964-03-30 1965-12-07 Gen Electric Engine mounting
US3288404A (en) * 1964-08-24 1966-11-29 Lord Corp Engine mounting system
US3464657A (en) * 1967-08-30 1969-09-02 Us Army Vibration damped platform
GB1328410A (en) * 1969-11-29 1973-08-30 Ver Flugtechnische Werke Aircraft engine mounting means
US3675418A (en) * 1970-11-19 1972-07-11 United Aircraft Corp Jet engine force frame
US3831888A (en) * 1972-07-27 1974-08-27 Mc Donnell Douglas Corp Aircraft engine suspension system
US3848832A (en) * 1973-03-09 1974-11-19 Boeing Co Aircraft engine installation
US3836100A (en) * 1973-06-13 1974-09-17 United Aircraft Corp Engine mounting arrangement
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
GB2010969A (en) * 1977-12-22 1979-07-04 Rolls Royce Mounting for Gas Turbine Jet Propulsion Engine
US4213585A (en) * 1978-05-22 1980-07-22 The Boeing Company Mounting system for a wing mounted aircraft engine
GB2049817A (en) * 1979-05-31 1980-12-31 Rolls Royce Mounting for Gas Turbine Engine
FR2469566A1 (fr) * 1979-11-12 1981-05-22 Snecma Perfectionnements aux dispositifs de fixation de turboreacteurs multiflux
US4403762A (en) * 1981-02-20 1983-09-13 General Motors Corporation Low force transmissibility mount

Also Published As

Publication number Publication date
GB8726681D0 (en) 1987-12-16
SE8704582D0 (sv) 1987-11-20
CA1320710C (fr) 1993-07-27
FR2612271A1 (fr) 1988-09-16
SE8704582L (sv) 1988-09-14
US4875655A (en) 1989-10-24
GB2202279A (en) 1988-09-21
GB2202279B (en) 1991-11-06
JPS63231094A (ja) 1988-09-27
DE3739941A1 (de) 1988-09-22

Similar Documents

Publication Publication Date Title
FR2612271B1 (fr) Systeme et procede de suspension pour un moteur d'aeronef
FR2648556B1 (fr) Systeme et procede d'excitation de tremblement pour un gyrolaser
EP0249776A3 (en) Cooling and lubrication system for an internal-combustion engine
FR2608807B1 (fr) Systeme multiprocesseur et procede d'equilibrage de charge pour ledit systeme
EP0356227A3 (en) Cooling system for multi-cylinder engine
GB8812727D0 (en) Turbo-charger engine system
EP0222089A3 (en) Lubricating oil filtration system for an engine
GB8805454D0 (en) Cooling system for i c engine & method of controlling such cooling system
FR2553596B1 (fr) Systeme d'actionnement d'helice de moteur
FR2610752B1 (fr) Procede de representation de l'image en perspective d'un terrain et systeme pour sa mise en oeuvre
AU5170590A (en) Method and system for controlled combustion engines
GB8825649D0 (en) Lubricating system for turbo-engine
EP0276003A3 (en) Fail-safe method and system for automotive engines
FR2520892B1 (fr) Systeme regulateur de la vitesse d'un moteur
FR2534098B1 (fr) Procede d'enregistrement simultane de dessins et de traces graphiques
FR2615288B1 (fr) Procede automatique d'identification de defauts par ultrasons et systeme correspondant
GB8411951D0 (en) Intake system for ic engine
GB8829132D0 (en) Lubrication system for engines
GB8728114D0 (en) Engine control & combustion quality detection system & method
GB2094903B (en) Lubrication system of ic engine
FR2613158B1 (fr) Procede et systeme de transmission d'informations
FR2542539B1 (fr) Procede et systeme d'enregistrement d'images transformees
FR2549255B1 (fr) Procede d'interpretation de sujet pour un systeme d'enseignement assiste par ordinateur
FR2624964B1 (fr) Systeme de reference de vitesse pour le pilotage d'un aeronef
FR2558527B1 (fr) Systeme de decompression automatique pour le demarrage d'un moteur

Legal Events

Date Code Title Description
ST Notification of lapse