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DE69012071D1 - Ausfallsichere Haltevorrichtung für Treibwerke. - Google Patents

Ausfallsichere Haltevorrichtung für Treibwerke.

Info

Publication number
DE69012071D1
DE69012071D1 DE69012071T DE69012071T DE69012071D1 DE 69012071 D1 DE69012071 D1 DE 69012071D1 DE 69012071 T DE69012071 T DE 69012071T DE 69012071 T DE69012071 T DE 69012071T DE 69012071 D1 DE69012071 D1 DE 69012071D1
Authority
DE
Germany
Prior art keywords
engines
fail
holding device
safe holding
safe
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
DE69012071T
Other languages
English (en)
Other versions
DE69012071T2 (de
Inventor
Kenneth Richard Langley
Derek Herbert Charles Fox
John Michael Treby
Malcolm Short
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
Priority claimed from GB898927464A external-priority patent/GB8927464D0/en
Application filed by Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of DE69012071D1 publication Critical patent/DE69012071D1/de
Publication of DE69012071T2 publication Critical patent/DE69012071T2/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; 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
    • B64D27/404—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
    • B64D27/402—Arrangements for mounting power plants in aircraft comprising box like supporting frames, e.g. pylons or arrangements for embracing the power plant
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Transmission Devices (AREA)
  • Vibration Prevention Devices (AREA)
DE69012071T 1989-12-05 1990-11-21 Ausfallsichere Haltevorrichtung für Treibwerke. Expired - Lifetime DE69012071T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB898927464A GB8927464D0 (en) 1989-12-05 1989-12-05 Failure tolerant engine mounting
GB909000742A GB9000742D0 (en) 1989-12-05 1990-01-12 Failure tolerant engine mounting

Publications (2)

Publication Number Publication Date
DE69012071D1 true DE69012071D1 (de) 1994-10-06
DE69012071T2 DE69012071T2 (de) 1995-04-13

Family

ID=26296313

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69012071T Expired - Lifetime DE69012071T2 (de) 1989-12-05 1990-11-21 Ausfallsichere Haltevorrichtung für Treibwerke.

Country Status (4)

Country Link
US (1) US5078342A (de)
EP (1) EP0431800B1 (de)
JP (1) JPH0687495A (de)
DE (1) DE69012071T2 (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111731489A (zh) * 2019-03-25 2020-10-02 空中客车运营简化股份公司 具有两部分连杆的飞行器后发动机附接结构及包括该结构的飞行器

Families Citing this family (43)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2677953B1 (fr) * 1991-06-19 1993-09-10 Snecma Structure de suspension arriere d'un turboreacteur.
FR2677954B1 (fr) * 1991-06-19 1993-09-10 Snecma Structure de suspension arriere du carter d'echappement d'un turboreacteur.
FR2680353B1 (fr) * 1991-08-14 1993-10-15 Snecma Structure d'accrochage arriere d'un turboreacteur.
US5275357A (en) * 1992-01-16 1994-01-04 General Electric Company Aircraft engine mount
GB2275308B (en) * 1993-02-20 1997-02-26 Rolls Royce Plc A mounting for coupling a turbofan gas turbine engine to an aircraft structure
WO1996020111A1 (en) * 1994-12-23 1996-07-04 United Technologies Corporation A mounting arrangement for a gas turbine engine
US5649417A (en) * 1995-03-24 1997-07-22 The Boeing Company Fail-safe engine mount system
US5620154A (en) 1995-05-03 1997-04-15 The Boeing Company Three link failsafe engine mount
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
US5921500A (en) * 1997-10-08 1999-07-13 General Electric Company Integrated failsafe engine mount
US5927644A (en) * 1997-10-08 1999-07-27 General Electric Company Double failsafe engine mount
FR2770486B1 (fr) * 1997-11-06 2000-01-28 Aerospatiale Dispositif d'accrochage d'un moteur sur un aeronef
US6170252B1 (en) 1998-12-14 2001-01-09 United Technologies Corporation Locator for a gearbox mount
US6212974B1 (en) 1998-12-17 2001-04-10 United Technologies Corporation Variable stiffness positioning link for a gearbox
FR2793767B1 (fr) * 1999-05-17 2001-09-21 Aerospatiale Airbus Dispositif d'accrochage d'un moteur d'aeronef
FR2799432A1 (fr) * 1999-10-07 2001-04-13 Snecma Suspension a securite integree pour groupes motopropulseurs d'aeronefs
GB9927425D0 (en) 1999-11-20 2000-01-19 Rolls Royce Plc A gas turbine engine mounting arrangement
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
FR2818614B1 (fr) * 2000-12-21 2003-01-31 Snecma Moteurs Piece de suspension d'un turboreacteur
US6843449B1 (en) 2004-02-09 2005-01-18 General Electric Company Fail-safe aircraft engine mounting system
FR2868041B1 (fr) * 2004-03-25 2006-05-26 Snecma Moteurs Sa Suspension d'un moteur d'avion
FR2873985B1 (fr) * 2004-08-04 2006-11-24 Airbus France Sas Ensemble moteur pour aeronef
WO2006060005A1 (en) * 2004-12-01 2006-06-08 United Technologies Corporation Fan-turbine rotor assembly with integral inducer section for a tip turbine engine
US9109537B2 (en) * 2004-12-04 2015-08-18 United Technologies Corporation Tip turbine single plane mount
FR2883839B1 (fr) * 2005-03-29 2007-06-29 Snecma Moteurs Sa Suspension arriere de turboreacteur
GB0603539D0 (en) * 2006-02-22 2006-04-05 Airbus Uk Ltd Control surface failsafe drop link
DE102008021431A1 (de) 2008-04-29 2009-11-12 Airbus Deutschland Gmbh Flugzeug mit einer Energie-Versorgungsvorrichtung
GB2466297B (en) * 2008-12-22 2010-11-10 Rolls Royce Plc Catcher pin assembly
US20130074517A1 (en) * 2011-09-23 2013-03-28 United Technologies Corporation Gas turbine engine mount assembly
US9637241B2 (en) 2012-03-16 2017-05-02 The Boeing Company Engine mounting system for an aircraft
US9227734B2 (en) * 2012-08-31 2016-01-05 United Technologies Corporation Secondary load path for gas turbine engine
FR3001714B1 (fr) * 2013-02-05 2016-08-26 Astrium Sas Dispositif de support et de maintien de reservoirs cryogeniques
GB201315968D0 (en) 2013-09-09 2013-10-23 Rolls Royce Plc Aircraft engine mount
FR3010700B1 (fr) * 2013-09-18 2017-11-03 Snecma Dispositif de suspension d'un carter, turbomachine et ensemble propulsif
FR3041935B1 (fr) * 2015-10-05 2017-12-15 Airbus Operations Sas Ensemble moteur pour aeronef comprenant au moins deux attaches moteur arriere decalees axialement l'une de l'autre
US10385868B2 (en) * 2016-07-05 2019-08-20 General Electric Company Strut assembly for an aircraft engine
FR3058388B1 (fr) * 2016-11-04 2019-05-10 Airbus Operations Attache arriere d'un moteur d'aeronef
FR3097203A1 (fr) * 2019-06-14 2020-12-18 Airbus Operations (S.A.S.) Ensemble de motorisation d’aéronef comprenant une attache moteur arrière
US12209539B2 (en) * 2023-04-07 2025-01-28 Rtx Corporation Fusible gearbox support with catcher pin systems and methods
US12044181B1 (en) 2023-04-07 2024-07-23 Rtx Corporation Fusible gearbox center guide support with catcher pin and anti-rotation pin systems and methods
US12196138B2 (en) * 2023-04-07 2025-01-14 Rtx Corporation Frangible gearbox center guide support systems and methods

Family Cites Families (9)

* 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
US3907220A (en) * 1974-03-14 1975-09-23 United Aircraft Corp Rear engine redundant mount
US4044973A (en) * 1975-12-29 1977-08-30 The Boeing Company Nacelle assembly and mounting structures for a turbofan jet propulsion engine
GB1521847A (en) * 1976-04-30 1978-08-16 Rolls Royce Attachment for attaching jet propulsion engines to vehicle structure
GB2045357B (en) * 1979-03-06 1982-11-10 Westland Aircraft Ltd Aircraft turbine engine mounting assembly
GB8300748D0 (en) * 1983-01-12 1983-02-16 British Aerospace Power plant attachment for aircraft wings
US4603822A (en) * 1983-12-08 1986-08-05 The Boeing Company Aft engine mount
FR2599708A1 (fr) * 1986-06-10 1987-12-11 Snecma Dispositif d'accrochage arriere de securite d'un turboreacteur sur un mat d'avion
GB2224707B (en) * 1988-11-12 1992-06-10 Rolls Royce Plc Improvements in or relating to engine mounting integrity

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN111731489A (zh) * 2019-03-25 2020-10-02 空中客车运营简化股份公司 具有两部分连杆的飞行器后发动机附接结构及包括该结构的飞行器

Also Published As

Publication number Publication date
DE69012071T2 (de) 1995-04-13
JPH0687495A (ja) 1994-03-29
EP0431800A1 (de) 1991-06-12
EP0431800B1 (de) 1994-08-31
US5078342A (en) 1992-01-07

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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: WIESE KONNERTH FISCHER PATENTANWAELTE PARTNERSCHAF

8328 Change in the person/name/address of the agent

Representative=s name: SCHROETER LEHMANN FISCHER & NEUGEBAUER, 81479 MUEN