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DE69305285D1 - Motorlager - Google Patents

Motorlager

Info

Publication number
DE69305285D1
DE69305285D1 DE69305285T DE69305285T DE69305285D1 DE 69305285 D1 DE69305285 D1 DE 69305285D1 DE 69305285 T DE69305285 T DE 69305285T DE 69305285 T DE69305285 T DE 69305285T DE 69305285 D1 DE69305285 D1 DE 69305285D1
Authority
DE
Germany
Prior art keywords
engine mounts
mounts
engine
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
DE69305285T
Other languages
English (en)
Other versions
DE69305285T2 (de
Inventor
John J Gwinn
Marshall W Downing
Warren E Schmidt
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.)
Lord Corp
Original Assignee
Lord Corp
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 Lord Corp filed Critical Lord Corp
Publication of DE69305285D1 publication Critical patent/DE69305285D1/de
Application granted granted Critical
Publication of DE69305285T2 publication Critical patent/DE69305285T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • B64D27/40—Arrangements for mounting power plants in aircraft
    • B64D27/404—Suspension arrangements specially adapted for supporting vertical loads
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C27/00—Elastic or yielding bearings or bearing supports, for exclusively rotary movement
    • F16C27/06—Elastic or yielding bearings or bearing supports, for exclusively rotary movement by means of parts of rubber or like materials
    • F16C27/063—Sliding contact bearings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/38—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers with a sleeve of elastic material between a rigid outer sleeve and a rigid inner sleeve or pin, i.e. bushing-type
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16F—SPRINGS; SHOCK-ABSORBERS; MEANS FOR DAMPING VIBRATION
    • F16F1/00—Springs
    • F16F1/36—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers
    • F16F1/40—Springs made of rubber or other material having high internal friction, e.g. thermoplastic elastomers consisting of a stack of similar elements separated by non-elastic intermediate layers
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
    • F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
    • F16C2326/00—Articles relating to transporting
    • F16C2326/43—Aeroplanes; Helicopters
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • General Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Architecture (AREA)
  • Vibration Prevention Devices (AREA)
  • Springs (AREA)
DE69305285T 1992-08-11 1993-08-10 Motorlager Expired - Fee Related DE69305285T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/928,925 US5351930A (en) 1992-08-11 1992-08-11 Mounting for engines and the like

Publications (2)

Publication Number Publication Date
DE69305285D1 true DE69305285D1 (de) 1996-11-14
DE69305285T2 DE69305285T2 (de) 1997-03-20

Family

ID=25457016

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69305285T Expired - Fee Related DE69305285T2 (de) 1992-08-11 1993-08-10 Motorlager

Country Status (3)

Country Link
US (1) US5351930A (de)
EP (1) EP0583158B1 (de)
DE (1) DE69305285T2 (de)

Families Citing this family (65)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5649417A (en) * 1995-03-24 1997-07-22 The Boeing Company Fail-safe engine mount system
US5860623A (en) * 1995-05-03 1999-01-19 The Boeing Company Three link failsafe engine mount
US5620154A (en) * 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
US5687948A (en) * 1995-09-26 1997-11-18 Lord Corporation Vibration isolation system including a passive tuned vibration absorber
US5762295A (en) * 1996-02-23 1998-06-09 Lord Corporation Dynamically optimized engine suspension system
US5725181A (en) * 1996-05-01 1998-03-10 The Boeing Company Aircraft engine thrust mount
US6065742A (en) * 1996-09-13 2000-05-23 Lord Corporation Multi-directional tuned vibration absorber
US5957440A (en) * 1997-04-08 1999-09-28 Lord Corporation Active fluid mounting
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
FR2774358B1 (fr) * 1998-02-04 2000-04-21 Aerospatiale Dispositif d'accrochage d'un moteur d'aeronef
FR2775465B1 (fr) 1998-03-02 2000-05-26 Aerospatiale Dispositif d'accrochage d'un moteur sur un pylone d'aeronef
US6328293B1 (en) 1998-09-18 2001-12-11 Lord Corporation Multi-linkage suspension system including outboard isolators
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
US6330995B1 (en) * 2000-02-29 2001-12-18 General Electric Company Aircraft engine mount
US6296203B1 (en) * 2000-05-24 2001-10-02 General Electric Company Snubber thrust mount
US6715746B2 (en) 2000-07-21 2004-04-06 Lord Corporation Vibration isolation device with load dependent stiffness
EP1320488A2 (de) 2000-09-27 2003-06-25 Lord Corporation Befestigungsvorrichtung eines hilfsaggregats (apu) in einem flugzeug
FR2818614B1 (fr) * 2000-12-21 2003-01-31 Snecma Moteurs Piece de suspension d'un turboreacteur
FR2820402B1 (fr) * 2001-02-08 2003-05-02 Eads Airbus Sa Dispositif d'accrochage d'un moteur sur un aeronef
FR2855494B1 (fr) * 2003-05-27 2006-09-22 Snecma Moteurs Dispositif d'accrocharge arriere de moteur d'avion
FR2855495B1 (fr) * 2003-05-27 2006-11-24 Snecma Moteurs Dispositif d'accrochage avant de moteur d'avion
US6843449B1 (en) 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system
FR2867155B1 (fr) * 2004-03-08 2007-06-29 Snecma Moteurs Suspension d'un moteur a la structure d'un avion
FR2869874B1 (fr) * 2004-05-04 2006-06-23 Snecma Moteurs Sa Moteur d'avion avec des moyens de suspension a la structure d'un avion
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
FR2891244B1 (fr) 2005-09-26 2009-04-03 Airbus France Sas Mat d'accrochage de moteur pour aeronef
FR2891245B1 (fr) * 2005-09-26 2007-10-26 Airbus France Sas Procede de montage d'un moteur d'aeronef sur une structure rigide d'un mat d'accrochage du moteur
FR2891253B1 (fr) * 2005-09-28 2007-10-26 Airbus France Sas Attache arriere d'un moteur d'aeronef a deux manilles
US8104736B2 (en) * 2005-12-01 2012-01-31 Hamilton Sundstrand Corporation Gas turbine engine auxiliary component mount
FR2914907B1 (fr) * 2007-04-16 2009-10-30 Snecma Sa Suspension souple avec peigne pour turbomoteur
FR2916424B1 (fr) * 2007-05-23 2009-08-21 Airbus France Sa Mat d'accrochage de moteur pour aeronef comprenant une cale biaise pour la fixation de l'attache moteur avant
WO2008150202A1 (en) * 2007-06-08 2008-12-11 Volvo Aero Corporation A structure for transferring loads at a gas turbine engine, and an engine and an aircraft with such a structure
FR2917711B1 (fr) * 2007-06-25 2010-01-15 Snecma Suspension d'un turbomoteur a la structure d'un aeronef
DE102008021431A1 (de) * 2008-04-29 2009-11-12 Airbus Deutschland Gmbh Flugzeug mit einer Energie-Versorgungsvorrichtung
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
FR2933070B1 (fr) * 2008-06-25 2010-08-20 Snecma Systeme propulsif d'aeronef
US7950633B2 (en) * 2008-08-07 2011-05-31 Drs Rsta, Inc. Vibration isolator system
RU2388659C1 (ru) * 2008-11-24 2010-05-10 Государственное предприятие "Запорожское машиностроительное конструкторское бюро "Прогресс" имени академика А.Г. Ивченко Устройство крепления газотурбинного двигателя к летательному аппарату
US9527598B2 (en) 2009-01-26 2016-12-27 Lord Corporation Aircraft engine mounting system and method of mounting aircraft engines
US8313293B2 (en) * 2009-05-15 2012-11-20 Pratt & Whitney Canada Corp. Turbofan mounting system
US8567202B2 (en) 2009-05-15 2013-10-29 Pratt & Whitney Canada Corp. Support links with lockable adjustment feature
US8979491B2 (en) 2009-05-15 2015-03-17 Pratt & Whitney Canada Corp. Turbofan mounting arrangement
US7784773B1 (en) 2009-08-04 2010-08-31 Itt Manufacturing Enterprises, Inc. Isolator useful for in-line mounting with a strut
KR101767071B1 (ko) 2010-06-14 2017-08-10 로오드 코포레이션 헬리콥터 엔진 장착 시스템 및 방법
US9988155B2 (en) * 2013-02-07 2018-06-05 United Technologies Corporation System and method for aft mount of gas turbine engine
US8979020B2 (en) 2013-06-07 2015-03-17 Pratt & Whitney Canada Corp. Mounting system for mounting engine nacelle components and associated method
US10144524B2 (en) * 2013-06-14 2018-12-04 Rohr, Inc. Assembly for mounting a turbine engine to a pylon
GB201315968D0 (en) * 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
FR3015434B1 (fr) * 2013-12-23 2017-12-08 Snecma Suspension de turbomachine
GB2530733A (en) * 2014-09-30 2016-04-06 Rolls Royce Plc Gas Turbine Engine Mounting Arrangement
CN107108039B (zh) * 2015-01-07 2019-08-30 洛德公司 飞行器发动机安装架
FR3040076B1 (fr) * 2015-08-13 2017-08-11 Airbus Operations Sas Ensemble moteur pour aeronef comprenant une structure primaire de mat d'accrochage equipee d'une extension de caisson comprenant deux parties en forme globale d'arceau
US10029801B2 (en) * 2015-08-17 2018-07-24 The Boeing Company AFT engine mounting link rotational stop collar
US11066178B2 (en) * 2015-09-02 2021-07-20 Raytheon Technologies Corporation Link for aircraft component mounting
FR3049264B1 (fr) * 2016-03-25 2019-07-05 Airbus Operations Systeme de montage pour un aeronef, destine a la fixation d’un moteur sur un mat d’attache.
FR3058986B1 (fr) * 2016-11-21 2021-04-16 Airbus Operations Sas Attache arriere d'un moteur d'aeronef comportant des temoins de rupture
FR3093995A1 (fr) * 2019-03-18 2020-09-25 Airbus Operations (S.A.S.) Attache moteur arrière d’un aéronef présentant un encombrement réduit en largeur et aéronef comprenant au moins une telle attache moteur arrière
FR3098194B1 (fr) * 2019-07-01 2021-07-16 Airbus Operations Sas Attache moteur pour un moteur d’un aeronef comportant une bielle et un systeme de maintien de la bielle
US11273923B2 (en) * 2019-07-12 2022-03-15 Spirit Aerosystems, Inc. Fail-safe engine support system
FR3106126B1 (fr) * 2020-01-10 2022-01-07 Safran Aircraft Engines Assemblage entre un pylône d’aéronef et une turbomachine
CN112486203B (zh) * 2020-11-18 2022-04-08 南京航空航天大学 一种飞翼无人机赫伯斯特机动飞行控制方法
US12172524B1 (en) * 2021-11-17 2024-12-24 Nissan Motor Co., Ltd. Motor mount system

Family Cites Families (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3085773A (en) * 1960-02-01 1963-04-16 North American Aviation Inc Adjustable engine mount
US3487888A (en) * 1966-08-22 1970-01-06 Mc Donnell Douglas Corp Cabin engine sound suppressor
GB1328410A (en) * 1969-11-29 1973-08-30 Ver Flugtechnische Werke Aircraft engine mounting means
US3809340A (en) * 1972-12-26 1974-05-07 A Dolgy Devices for mounting an engine on an aircraft pylon
US3907220A (en) * 1974-03-14 1975-09-23 United Aircraft Corp Rear engine redundant mount
FR2469566A1 (fr) * 1979-11-12 1981-05-22 Snecma Perfectionnements aux dispositifs de fixation de turboreacteurs multiflux
US4494738A (en) * 1982-03-08 1985-01-22 Oil States Industries, Inc. Shock-absorbing joint and assembly with rotating arms and elastomeric spring action
GB2129498B (en) * 1982-10-29 1986-04-03 Rolls Royce Mounting system for two coupled turboshaft gas turbine engines
WO1985002596A1 (en) * 1983-12-08 1985-06-20 The Boeing Company Aft engine mount
US4634081A (en) * 1983-12-30 1987-01-06 The Boeing Company Aft engine mount with vibration isolators
US4571936A (en) * 1985-07-10 1986-02-25 The United States Of America As Represented By The Secretary Of The Air Force Length adjustable strut link with low aerodynamic drag
US4717094A (en) * 1986-05-19 1988-01-05 The Boeing Company Aircraft engine mount system with vibration isolators
FR2599708A1 (fr) * 1986-06-10 1987-12-11 Snecma Dispositif d'accrochage arriere de securite d'un turboreacteur sur un mat d'avion
US4725019A (en) * 1986-08-11 1988-02-16 The Boeing Company Aircraft engine mount with vertical vibration isolation
US4875655A (en) * 1987-03-13 1989-10-24 General Electric Company Vibration isolating engine mount
US4854525A (en) * 1987-05-19 1989-08-08 The Boeing Company Engine mounting assembly
US4805851A (en) * 1987-08-10 1989-02-21 Herbst Paul T Turbine engine mounting bracket assembly
US4821980A (en) * 1987-09-29 1989-04-18 The Boeing Company Vibration isolating engine mount
FR2635751B1 (fr) * 1988-09-01 1991-01-04 Snecma Dispositif de fixation d'une biellette de suspension d'un turboreacteur
JP2790185B2 (ja) * 1989-02-15 1998-08-27 辰治 石丸 差動二重梃子機構を有する構造体の免震・制振機構
US5108045A (en) * 1990-04-25 1992-04-28 Law Thomas R Engine mounting assembly
US5176339A (en) * 1991-09-30 1993-01-05 Lord Corporation Resilient pivot type aircraft mounting

Also Published As

Publication number Publication date
EP0583158B1 (de) 1996-10-09
US5351930A (en) 1994-10-04
EP0583158A1 (de) 1994-02-16
DE69305285T2 (de) 1997-03-20

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ZEITLER, VOLPERT, KANDLBINDER, 80539 MUENCHEN

8339 Ceased/non-payment of the annual fee