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IT8323356A0 - Accoppiati. sistema di supporto per motori a turbina a gas turboalbero - Google Patents

Accoppiati. sistema di supporto per motori a turbina a gas turboalbero

Info

Publication number
IT8323356A0
IT8323356A0 IT8323356A IT2335683A IT8323356A0 IT 8323356 A0 IT8323356 A0 IT 8323356A0 IT 8323356 A IT8323356 A IT 8323356A IT 2335683 A IT2335683 A IT 2335683A IT 8323356 A0 IT8323356 A0 IT 8323356A0
Authority
IT
Italy
Prior art keywords
coupled
gas turbine
support system
turbine engines
shaft gas
Prior art date
Application number
IT8323356A
Other languages
English (en)
Other versions
IT1169856B (it
Inventor
Alfred Walter Osborn
Original Assignee
Rolls Royce
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 Rolls Royce filed Critical Rolls Royce
Publication of IT8323356A0 publication Critical patent/IT8323356A0/it
Application granted granted Critical
Publication of IT1169856B publication Critical patent/IT1169856B/it

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)
  • Control Of Turbines (AREA)
IT23356/83A 1982-10-29 1983-10-19 Sistema di supporto per motori a turbina a gas turboalbero accoppiati IT1169856B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB08231063A GB2129498B (en) 1982-10-29 1982-10-29 Mounting system for two coupled turboshaft gas turbine engines

Publications (2)

Publication Number Publication Date
IT8323356A0 true IT8323356A0 (it) 1983-10-19
IT1169856B IT1169856B (it) 1987-06-03

Family

ID=10533946

Family Applications (1)

Application Number Title Priority Date Filing Date
IT23356/83A IT1169856B (it) 1982-10-29 1983-10-19 Sistema di supporto per motori a turbina a gas turboalbero accoppiati

Country Status (3)

Country Link
US (1) US4500054A (it)
GB (1) GB2129498B (it)
IT (1) IT1169856B (it)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4759262A (en) * 1987-05-11 1988-07-26 The Dow Chemical Company Apparatus for restraining rotary motion of a motor component
GB2224707B (en) * 1988-11-12 1992-06-10 Rolls Royce Plc Improvements in or relating to engine mounting integrity
US5351930A (en) * 1992-08-11 1994-10-04 Lord Corporation Mounting for engines and the like
FR2728538A1 (fr) * 1994-12-23 1996-06-28 Eurocopter France Dispositif de suspension anti-vibratoire de rotor d'helicoptere
DE19846328A1 (de) * 1998-10-08 2000-04-13 Flender A F & Co Doppelseitige Drehmomentstütze
US6581874B2 (en) 2000-09-27 2003-06-24 Lord Corporation Mounting assembly for an aircraft auxiliary power unit and method
US6484970B2 (en) * 2001-03-22 2002-11-26 Honeywell International, Inc. Ballistic shield for dual engine single output shaft propulsion system
BE1017836A3 (nl) * 2007-11-05 2009-08-04 Hansen Transmissions Int Reactiearm voor een windturbineaandrijving.
FR2935954B1 (fr) * 2008-09-18 2011-06-03 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs traversant le fuselage et reliee a celui-ci par au moins une bielle.
FR2935953B1 (fr) * 2008-09-18 2010-10-29 Airbus France Partie arriere d'aeronef comprenant deux semi-structures de support de moteurs rapportees l'une sur l'autre au sein d'un espace interieur d'aeronef.
FR2935955B1 (fr) * 2008-09-18 2010-10-15 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs reliee au fuselage par au moins un element de blocage sollicite en compression.
FR2943623B1 (fr) * 2009-03-30 2011-04-29 Airbus France Partie arriere d'aeronef comprenant une structure de support de moteurs montee oscillante sur le fuselage
US20130319003A1 (en) * 2012-05-30 2013-12-05 Jason Peel Auxiliary power unit mount with fire resistant shielding
US10472079B2 (en) * 2014-05-02 2019-11-12 Sikorsky Aircraft Corporation Articulated mounts
US10215100B2 (en) 2016-03-14 2019-02-26 Hamilton Sundstrand Corporation One degree-of-constraint semi-fusible gearbox mounting link
US10012149B2 (en) 2016-03-14 2018-07-03 Hamilton Sundstrand Corporation Two degree-of-constraint semi-fusible gearbox mounting link
US10006373B2 (en) 2016-03-14 2018-06-26 Hamilton Sundstrand Coporation Two degree-of-constraint semi-fusible gearbox mounting link
US10066552B2 (en) 2016-03-14 2018-09-04 Hamilton Sundstrand Corporation One degree-of-constraint semi-fusible gearbox mounting link
EP3736045A1 (de) * 2019-05-10 2020-11-11 Flender GmbH Stützvorrichtung für zwei getriebe sowie vorrichtung mit einer solchen stützvorrichtung

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1664129A (en) * 1927-02-16 1928-03-27 Emil Pallenberg Resilient seat mount
US2324542A (en) * 1942-09-14 1943-07-20 Marmon Herrington Co Inc Dual transmission control
US2539960A (en) * 1946-05-22 1951-01-30 Bristol Aeroplane Co Ltd Mounting structure for gas-turbine power plants for aircraft
US2718756A (en) * 1951-06-14 1955-09-27 Gen Motors Corp Mounting and supporting structure for aircraft gas turbine power plants having reduction gearing
US2828607A (en) * 1955-10-24 1958-04-01 Gen Motors Corp Dual engine support
US3180426A (en) * 1962-03-30 1965-04-27 United Aircraft Corp Free turbine engine control system
GB1074067A (en) * 1964-06-23 1967-06-28 Rolls Royce Mounting arrangement for jet propulsion engines
US3288404A (en) * 1964-08-24 1966-11-29 Lord Corp Engine mounting system
GB1029106A (en) * 1965-02-19 1966-05-11 Rolls Royce Aircraft
DE1531395A1 (de) * 1967-07-18 1970-01-29 Entwicklungsring Sued Gmbh Triebwerksaufhaengung,insbesondere fuer die Strahltriebwerke von Kurz- oder Senkrechtstartflugzeugen
US3907220A (en) * 1974-03-14 1975-09-23 United Aircraft Corp Rear engine redundant mount
DE2720957A1 (de) * 1977-05-10 1978-11-23 Willi Klotz Doppelantrieb fuer motorsegler (motorsegelflugzeug)

Also Published As

Publication number Publication date
GB2129498A (en) 1984-05-16
GB2129498B (en) 1986-04-03
US4500054A (en) 1985-02-19
IT1169856B (it) 1987-06-03

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