JPS539324B2 - - Google Patents

Info

Publication number
JPS539324B2
JPS539324B2 JP1866074A JP1866074A JPS539324B2 JP S539324 B2 JPS539324 B2 JP S539324B2 JP 1866074 A JP1866074 A JP 1866074A JP 1866074 A JP1866074 A JP 1866074A JP S539324 B2 JPS539324 B2 JP S539324B2
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.)
Expired
Application number
JP1866074A
Other languages
Japanese (ja)
Other versions
JPS5024623A (https=
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 JPS5024623A publication Critical patent/JPS5024623A/ja
Publication of JPS539324B2 publication Critical patent/JPS539324B2/ja
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00Features, 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
    • F02C7/20Mounting 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)
JP1866074A 1973-02-26 1974-02-18 Expired JPS539324B2 (https=)

Applications Claiming Priority (1)

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

Publications (2)

Publication Number Publication Date
JPS5024623A JPS5024623A (https=) 1975-03-15
JPS539324B2 true JPS539324B2 (https=) 1978-04-05

Family

ID=23313101

Family Applications (1)

Application Number Title Priority Date Filing Date
JP1866074A Expired JPS539324B2 (https=) 1973-02-26 1974-02-18

Country Status (6)

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

Families Citing this family (56)

* Cited by examiner, † Cited by third party
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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
RU2243392C2 (ru) * 2003-01-04 2004-12-27 Открытое акционерное общество "Авиадвигатель" Обтекатель компрессора газотурбинного двигателя
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
EP1777378A3 (en) * 2003-07-29 2011-03-09 Pratt & Whitney Canada Corp. Turbofan case and method of making
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
RU2385270C1 (ru) * 2008-10-14 2010-03-27 Федеральное Государственное Унитарное предприятие "Уральский научно-исследовательский институт композиционных материалов" Рама реактивной двигательной установки
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
US9945325B2 (en) * 2013-02-20 2018-04-17 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
DE102014112960A1 (de) * 2014-09-09 2016-03-10 Rolls-Royce Deutschland Ltd & Co Kg Gehäusevorrichtung eines Strahltriebwerks
DE102014112955A1 (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
US12049847B2 (en) * 2019-06-14 2024-07-30 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
US12123373B2 (en) * 2020-07-17 2024-10-22 Rtx Corporation Geared turbofan with over-speed protection
US11939886B2 (en) * 2022-05-30 2024-03-26 Pratt & Whitney Canada Corp. Aircraft engine having stator vanes made of different materials
US12091178B2 (en) 2022-05-30 2024-09-17 Pratt & Whitney Canada Corp. Aircraft engine with stator having varying geometry
US12017782B2 (en) 2022-05-30 2024-06-25 Pratt & Whitney Canada Corp. Aircraft engine with stator having varying pitch
US20240218835A1 (en) * 2023-01-04 2024-07-04 General Electric Company Outlet guide vanes and an accessory drive gearbox for a gas turbine engine

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
SE390052B (sv) 1976-11-29
DE2402007A1 (de) 1974-09-12
US3830058A (en) 1974-08-20
JPS5024623A (https=) 1975-03-15
DE2402007B2 (de) 1976-12-30
IT1008306B (it) 1976-11-10
GB1428091A (en) 1976-03-17
FR2219313A1 (https=) 1974-09-20

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