IT1008306B - Motore a turbina e relativa carcassa - Google Patents

Motore a turbina e relativa carcassa

Info

Publication number
IT1008306B
IT1008306B IT48654/74A IT4865474A IT1008306B IT 1008306 B IT1008306 B IT 1008306B IT 48654/74 A IT48654/74 A IT 48654/74A IT 4865474 A IT4865474 A IT 4865474A IT 1008306 B IT1008306 B IT 1008306B
Authority
IT
Italy
Prior art keywords
turbine engine
relative housing
housing
relative
turbine
Prior art date
Application number
IT48654/74A
Other languages
English (en)
Original Assignee
Avco 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 Avco Corp filed Critical Avco Corp
Application granted granted Critical
Publication of IT1008306B publication Critical patent/IT1008306B/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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT48654/74A 1973-02-26 1974-02-25 Motore a turbina e relativa carcassa IT1008306B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US00335750A US3830058A (en) 1973-02-26 1973-02-26 Fan engine mounting

Publications (1)

Publication Number Publication Date
IT1008306B true IT1008306B (it) 1976-11-10

Family

ID=23313101

Family Applications (1)

Application Number Title Priority Date Filing Date
IT48654/74A IT1008306B (it) 1973-02-26 1974-02-25 Motore a turbina e relativa carcassa

Country Status (6)

Country Link
US (1) US3830058A (it)
JP (1) JPS539324B2 (it)
FR (1) FR2219313A1 (it)
GB (1) GB1428091A (it)
IT (1) IT1008306B (it)
SE (1) SE390052B (it)

Families Citing this family (50)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4068470A (en) * 1974-11-08 1978-01-17 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with convertible accessories
GB1533551A (en) * 1974-11-08 1978-11-29 Gen Electric Gas turbofan engines
US4055041A (en) * 1974-11-08 1977-10-25 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Integrated gas turbine engine-nacelle
US4083181A (en) * 1976-06-14 1978-04-11 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Gas turbine engine with recirculating bleed
GB1557096A (en) * 1977-05-26 1979-12-05 Rolls Royce Rotor support structure for a gas turbine engine
GB2046843B (en) * 1979-04-17 1983-01-26 Rolls Royce Gas turbine engines-de-icing-icing
GB2192233B (en) * 1986-07-02 1990-11-28 Rolls Royce Plc A gas turbine engine load transfer structure
GB2195712B (en) * 1986-10-08 1990-08-29 Rolls Royce Plc A turbofan gas turbine engine
GB8630754D0 (en) * 1986-12-23 1987-02-04 Rolls Royce Plc Turbofan gas turbine engine
US4785625A (en) * 1987-04-03 1988-11-22 United Technologies Corporation Ducted fan gas turbine power plant mounting
US4820117A (en) * 1987-07-09 1989-04-11 United Technologies Corporation Crossed I-beam structural strut
US4914904A (en) * 1988-11-09 1990-04-10 Avco Corporation Oil cooler for fan jet engines
JPH06105048B2 (ja) * 1991-05-28 1994-12-21 ゼネラル・エレクトリック・カンパニイ コアフレームを静翼フレームに安定中央リングで着脱自在に取付ける装置
FR2738283B1 (fr) * 1995-08-30 1997-09-26 Snecma Agencement de turbomachine comprenant une grille d'aubes et un carter intermediaire
US6357220B1 (en) * 1998-12-22 2002-03-19 United Technologies Corporation Gearbox accessory mount
US7055306B2 (en) * 2003-04-30 2006-06-06 Hamilton Sundstrand Corporation Combined stage single shaft turbofan engine
GB0315894D0 (en) * 2003-07-08 2003-08-13 Rolls Royce Plc Aircraft engine arrangement
EP1649145B1 (en) * 2003-07-29 2008-05-28 Pratt & Whitney Canada Corp. Turbofan casing, turbofan engine and corresponding method
US7055303B2 (en) * 2003-12-22 2006-06-06 Pratt & Whitney Canada Corp. Gas turbine engine architecture
US7124572B2 (en) * 2004-09-14 2006-10-24 Honeywell International, Inc. Recuperator and turbine support adapter for recuperated gas turbine engines
US20080016876A1 (en) * 2005-06-02 2008-01-24 General Electric Company Method and apparatus for reducing gas turbine engine emissions
US8235325B2 (en) * 2005-10-04 2012-08-07 United Technologies Corporation Fan variable area nozzle positional measurement system
GB0622405D0 (en) 2006-11-10 2006-12-20 Rolls Royce Plc A turbine engine mounting arrangement
US7716914B2 (en) * 2006-12-21 2010-05-18 General Electric Company Turbofan engine assembly and method of assembling same
FR2919344B1 (fr) * 2007-07-26 2013-08-16 Snecma Turboreacteur a double flux comprenant une conduite de soufflante a un seul bras de passage de servitudes.
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
US8172512B2 (en) * 2008-04-23 2012-05-08 Hamilton Sundstrand Corporation Accessory gearbox system with compressor driven seal air supply
US8192143B2 (en) * 2008-05-21 2012-06-05 United Technologies Corporation Gearbox assembly
US9816441B2 (en) * 2009-03-30 2017-11-14 United Technologies Corporation Gas turbine engine with stacked accessory components
DE102010001059A1 (de) * 2010-01-20 2011-07-21 Rolls-Royce Deutschland Ltd & Co KG, 15827 Zwischengehäuse für ein Gasturbinentriebwerk
US8845277B2 (en) 2010-05-24 2014-09-30 United Technologies Corporation Geared turbofan engine with integral gear and bearing supports
US8753075B2 (en) * 2010-07-20 2014-06-17 Rolls-Royce Corporation Fan case assembly and method
GB2497934B (en) * 2011-12-22 2014-06-04 Rolls Royce Plc Aeroengine arrangement
US8979484B2 (en) 2012-01-05 2015-03-17 Pratt & Whitney Canada Corp. Casing for an aircraft turbofan bypass engine
FR2986040B1 (fr) 2012-01-20 2016-03-25 Turbomeca Support de palier de turbomachine
FR2988777B1 (fr) * 2012-03-29 2014-04-25 Snecma Propulsion Solide Integration de pieces d'arriere-corps de moteur aeronautique
US9410441B2 (en) 2012-09-13 2016-08-09 Pratt & Whitney Canada Corp. Turboprop engine with compressor turbine shroud
US9376935B2 (en) * 2012-12-18 2016-06-28 Pratt & Whitney Canada Corp. Gas turbine engine mounting ring
US9297314B2 (en) * 2012-12-19 2016-03-29 United Technologies Corporation Gas turbine engine with accessory gear box
WO2014130103A2 (en) 2013-02-20 2014-08-28 United Technologies Corporation Integrated heat exchangers for low fan pressure ratio geared turbofan
US20150098816A1 (en) * 2013-10-03 2015-04-09 General Electric Company System and method for controlling backbone bending in a gas turbine engine
DE102014112955A1 (de) * 2014-09-09 2016-03-10 Rolls-Royce Deutschland Ltd & Co Kg Gehäusevorrichtung eines Strahltriebwerks
DE102014112960A1 (de) * 2014-09-09 2016-03-10 Rolls-Royce Deutschland Ltd & Co Kg Gehäusevorrichtung eines Strahltriebwerks
US10316856B2 (en) 2015-12-01 2019-06-11 General Electric Company Casing for use in a turbofan engine and method of scavenging fluid therefrom
US10836499B2 (en) * 2017-08-22 2020-11-17 General Electric Company Turbine engine with single wall cantilevered architecture
BE1025975B1 (fr) * 2018-02-02 2019-09-03 Safran Aero Boosters S.A. Carter structural pour turbomachine axiale
US20220307417A1 (en) * 2019-06-14 2022-09-29 Rolls-Royce Deutschland Ltd & Co Kg Gas turbine engine and heat management system for cooling oil in an oil system of a gas turbine engine
GB2589125B (en) * 2019-11-21 2022-10-19 Gkn Aerospace Sweden Ab Heat exchanger integration
US11939886B2 (en) * 2022-05-30 2024-03-26 Pratt & Whitney Canada Corp. Aircraft engine having stator vanes made of different materials

Family Cites Families (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2539960A (en) * 1946-05-22 1951-01-30 Bristol Aeroplane Co Ltd Mounting structure for gas-turbine power plants for aircraft
GB937826A (en) * 1961-05-02 1963-09-25 Rolls Royce Engine driven fan
GB1041587A (en) * 1962-08-27 1966-09-07 Bristol Siddeley Engines Ltd Improvements in gas turbine engines
US3190591A (en) * 1963-02-11 1965-06-22 Cal Val Res & Dev Corp Core assembly for an engine mount
US3540682A (en) * 1964-12-02 1970-11-17 Gen Electric Turbofan type engine frame and support system
DE1503604A1 (de) * 1965-04-10 1969-09-11 Seifert Dr Ing Gerd W Axial- oder Radialgeblaese
US3327473A (en) * 1966-01-11 1967-06-27 Gen Motors Corp Engine support structure
US3398535A (en) * 1966-05-25 1968-08-27 Gen Electric Engine supporting structure
US3390527A (en) * 1967-07-19 1968-07-02 Avco Corp High bypass ratio turbofan
US3494129A (en) * 1968-03-06 1970-02-10 Gen Electric Fluid compressors and turbofan engines employing same
US3673802A (en) * 1970-06-18 1972-07-04 Gen Electric Fan engine with counter rotating geared core booster
GB1318748A (en) * 1970-08-11 1973-05-31 Secr Defence Gas turgine ducted fan engines for aircraft
US3688560A (en) * 1971-01-29 1972-09-05 Gen Electric Gas turbine engine with improved auxiliary power take-off
US3792586A (en) * 1973-01-22 1974-02-19 Avco Corp Bearing assembly systems

Also Published As

Publication number Publication date
JPS5024623A (it) 1975-03-15
US3830058A (en) 1974-08-20
SE390052B (sv) 1976-11-29
JPS539324B2 (it) 1978-04-05
FR2219313A1 (it) 1974-09-20
DE2402007A1 (de) 1974-09-12
DE2402007B2 (de) 1976-12-30
GB1428091A (en) 1976-03-17

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