JPS50127008A - - Google Patents

Info

Publication number
JPS50127008A
JPS50127008A JP50030655A JP3065575A JPS50127008A JP S50127008 A JPS50127008 A JP S50127008A JP 50030655 A JP50030655 A JP 50030655A JP 3065575 A JP3065575 A JP 3065575A JP S50127008 A JPS50127008 A JP S50127008A
Authority
JP
Japan
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.)
Pending
Application number
JP50030655A
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 JPS50127008A publication Critical patent/JPS50127008A/ja
Pending legal-status Critical Current

Links

Classifications

    • 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
    • F16M—FRAMES, CASINGS OR BEDS OF ENGINES, MACHINES OR APPARATUS, NOT SPECIFIC TO ENGINES, MACHINES OR APPARATUS PROVIDED FOR ELSEWHERE; STANDS; SUPPORTS
    • F16M7/00—Details of attaching or adjusting engine beds, frames, or supporting-legs on foundation or base; Attaching non-moving engine parts, e.g. cylinder blocks
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plant in aircraft; Aircraft characterised thereby
    • B64D27/02—Aircraft characterised by the type or position of power plant
    • B64D27/16—Aircraft characterised by the type or position of power plant of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plant of jet type within or attached to wing
    • B64D27/40—
    • B64D27/404—
JP50030655A 1974-03-14 1975-03-13 Pending JPS50127008A (ja)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US451661A US3907220A (en) 1974-03-14 1974-03-14 Rear engine redundant mount

Publications (1)

Publication Number Publication Date
JPS50127008A true JPS50127008A (ja) 1975-10-06

Family

ID=23793169

Family Applications (1)

Application Number Title Priority Date Filing Date
JP50030655A Pending JPS50127008A (ja) 1974-03-14 1975-03-13

Country Status (9)

Country Link
US (1) US3907220A (ja)
JP (1) JPS50127008A (ja)
BR (1) BR7501450A (ja)
CA (1) CA1020142A (ja)
DE (1) DE2510213C2 (ja)
FR (1) FR2264241B1 (ja)
GB (1) GB1488928A (ja)
IL (1) IL46569A (ja)
IT (1) IT1034150B (ja)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4022018A (en) * 1975-04-29 1977-05-10 General Electric Company Mounting system for a thrust generating engine
US4266741A (en) * 1978-05-22 1981-05-12 The Boeing Company Mounting apparatus for fan jet engine having mixed flow nozzle installation
US4531694A (en) * 1982-10-18 1985-07-30 Soloy Conversions, Ltd. Turbine engine drive and mounting assembly for fixed wing aircraft
GB2129498B (en) * 1982-10-29 1986-04-03 Rolls Royce Mounting system for two coupled turboshaft gas turbine engines
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
FR2599708A1 (fr) * 1986-06-10 1987-12-11 Snecma Dispositif d'accrochage arriere de securite d'un turboreacteur sur un mat d'avion
US4759262A (en) * 1987-05-11 1988-07-26 The Dow Chemical Company Apparatus for restraining rotary motion of a motor component
US4854525A (en) * 1987-05-19 1989-08-08 The Boeing Company Engine mounting assembly
EP0431800B1 (en) * 1989-12-05 1994-08-31 ROLLS-ROYCE plc Failure tolerant engine mounting
US5176339A (en) * 1991-09-30 1993-01-05 Lord Corporation Resilient pivot type aircraft mounting
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
US6196795B1 (en) * 1996-02-13 2001-03-06 Kvaerner Energy A.S. Turbine pack and method for adapting a turbine pack
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
US6170252B1 (en) * 1998-12-14 2001-01-09 United Technologies Corporation Locator for a gearbox mount
US6357220B1 (en) * 1998-12-22 2002-03-19 United Technologies Corporation Gearbox accessory mount
US7594623B2 (en) * 2002-09-17 2009-09-29 Bell Helicopter Textron Inc. Torsionally de-coupled engine mount system
GB0328671D0 (en) * 2003-12-11 2004-01-14 Rolls Royce Plc Aircraft engine mounting
US9719428B2 (en) * 2007-11-30 2017-08-01 United Technologies Corporation Gas turbine engine with pylon mounted accessory drive
US20090205341A1 (en) * 2008-02-20 2009-08-20 Muldoon Marc J Gas turbine engine with twin towershaft accessory gearbox
US9816441B2 (en) * 2009-03-30 2017-11-14 United Technologies Corporation Gas turbine engine with stacked accessory components
US20110016881A1 (en) * 2009-07-21 2011-01-27 Jose Luis Ruiz Gas turbine with exhaust gas casing and method for producing a gas turbine
WO2014070640A1 (en) * 2012-11-02 2014-05-08 United Technologies Corporation Redundant mount system
WO2016003534A2 (en) * 2014-05-02 2016-01-07 Sikorsky Aircraft Corporation Articulated mounts
US11167842B2 (en) * 2017-10-10 2021-11-09 Bell Helicopter Textron Inc. Mount for supporting a component and attenuating noise
FR3073823B1 (fr) * 2017-11-21 2019-11-08 Airbus Operations Attache moteur arriere pour un moteur d'aeronef

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1871957A (en) * 1929-05-28 1932-08-16 Delco Prod Corp Oscillating pivot joint
US2650753A (en) * 1947-06-11 1953-09-01 Gen Electric Turbomachine stator casing
DE1292501B (de) * 1961-09-29 1969-04-10 Gen Electric Halterungssystem fuer ein Turbinen-Propeller-Triebwerk an einer Flugzeugzelle
US3164342A (en) * 1962-06-19 1965-01-05 Solar Aircraft Co Engine mount
US3135487A (en) * 1962-09-07 1964-06-02 United Aircraft Corp Mount support with torque indicator
US3188808A (en) * 1962-12-03 1965-06-15 Cooper Bessemer Corp Gas turbine thrust compensating device
DE1506083A1 (de) * 1965-03-16 1969-10-23 Rolls Royce Triebwerkseinbau in Flugzeugen
GB1328410A (en) * 1969-11-29 1973-08-30 Ver Flugtechnische Werke Aircraft engine mounting means
DE2300125A1 (de) * 1973-01-03 1974-07-04 Dolgij Triebwerksaufhaengung fuer flugzeuge

Also Published As

Publication number Publication date
CA1020142A (en) 1977-11-01
AU7789975A (en) 1976-08-05
DE2510213A1 (de) 1976-02-26
IT1034150B (it) 1979-09-10
DE2510213C2 (de) 1986-12-04
GB1488928A (en) 1977-10-19
US3907220A (en) 1975-09-23
IL46569A (en) 1979-12-30
IL46569A0 (en) 1975-06-25
FR2264241B1 (ja) 1979-03-09
FR2264241A1 (ja) 1975-10-10
BR7501450A (pt) 1975-12-23

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