IL54895A - Variable cycle turboengine and method of operating an aircraft engine of this type - Google Patents

Variable cycle turboengine and method of operating an aircraft engine of this type

Info

Publication number
IL54895A
IL54895A IL54895A IL5489578A IL54895A IL 54895 A IL54895 A IL 54895A IL 54895 A IL54895 A IL 54895A IL 5489578 A IL5489578 A IL 5489578A IL 54895 A IL54895 A IL 54895A
Authority
IL
Israel
Prior art keywords
turboengine
operating
type
aircraft engine
variable cycle
Prior art date
Application number
IL54895A
Other languages
English (en)
Original Assignee
Gen Electric
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 Gen Electric filed Critical Gen Electric
Publication of IL54895A publication Critical patent/IL54895A/xx

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
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/003—Gas-turbine plants with heaters between turbine stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/02—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber
    • F02K3/04—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type
    • F02K3/075—Plants including a gas turbine driving a compressor or a ducted fan in which part of the working fluid by-passes the turbine and combustion chamber the plant including ducted fans, i.e. fans with high volume, low pressure outputs, for augmenting the jet thrust, e.g. of double-flow type controlling flow ratio between flows
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof

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)
IL54895A 1977-07-25 1978-06-13 Variable cycle turboengine and method of operating an aircraft engine of this type IL54895A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/818,473 US4222235A (en) 1977-07-25 1977-07-25 Variable cycle engine

Publications (1)

Publication Number Publication Date
IL54895A true IL54895A (en) 1982-12-31

Family

ID=25225620

Family Applications (1)

Application Number Title Priority Date Filing Date
IL54895A IL54895A (en) 1977-07-25 1978-06-13 Variable cycle turboengine and method of operating an aircraft engine of this type

Country Status (8)

Country Link
US (1) US4222235A (ru)
JP (1) JPS5440912A (ru)
AU (1) AU519600B2 (ru)
DE (1) DE2831802A1 (ru)
FR (1) FR2398891A1 (ru)
GB (1) GB1602699A (ru)
IL (1) IL54895A (ru)
IT (1) IT1097388B (ru)

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US5694768A (en) * 1990-02-23 1997-12-09 General Electric Company Variable cycle turbofan-ramjet engine
US5381655A (en) * 1993-05-10 1995-01-17 General Electric Company Admission mixing duct assembly
GB2307008A (en) * 1995-11-13 1997-05-14 Fred Moseley Gas turbine engine with two stage combustion
CN1105827C (zh) * 1995-12-20 2003-04-16 谢逢申 移出式超扇发动机
US5806303A (en) * 1996-03-29 1998-09-15 General Electric Company Turbofan engine with a core driven supercharged bypass duct and fixed geometry nozzle
US5809772A (en) * 1996-03-29 1998-09-22 General Electric Company Turbofan engine with a core driven supercharged bypass duct
GB2313580B (en) * 1996-05-31 2000-02-23 Astovl Limited An aircraft power plant
US6385959B1 (en) 1999-08-24 2002-05-14 MONTOYA CéSAR AGUILERA Gas turbine engine with increased fuel efficiency and method for accomplishing the same
FR2826056B1 (fr) * 2001-06-14 2003-12-19 Snecma Moteurs Dispositif de propulsion a cycle variable par transmission mecanique pour avion supersonique
US6837038B2 (en) * 2001-10-16 2005-01-04 United Technologies Corporation Variable cycle boost propulsor
US6792745B2 (en) * 2002-08-09 2004-09-21 The Boeing Company High bypass multi-fan engine
US7216475B2 (en) * 2003-11-21 2007-05-15 General Electric Company Aft FLADE engine
US7540450B2 (en) * 2004-07-16 2009-06-02 Pratt & Whitney Canada Corp. Aircraft propulsion system
US7134271B2 (en) * 2004-11-05 2006-11-14 General Electric Company Thrust vectoring aft FLADE engine
US8336289B2 (en) * 2007-08-30 2012-12-25 United Technologies Corporation Gas turbine engine systems and related methods involving multiple gas turbine cores
DE102008011643A1 (de) * 2008-02-28 2009-09-03 Rolls-Royce Deutschland Ltd & Co Kg Flugzeugantriebseinheit mit Multi-Fan-Ausgestaltung
US8387357B2 (en) * 2008-08-12 2013-03-05 Pratt & Whitney Recuperated bypass turbine engine
DE102008062813A1 (de) * 2008-12-23 2010-07-15 Rolls-Royce Deutschland Ltd & Co Kg Flugzeug mit einer Heck-Propeller-Triebwerksanordnung
US8382436B2 (en) 2009-01-06 2013-02-26 General Electric Company Non-integral turbine blade platforms and systems
US8262345B2 (en) 2009-02-06 2012-09-11 General Electric Company Ceramic matrix composite turbine engine
DE102010009477A1 (de) * 2010-02-26 2011-09-01 Rolls-Royce Deutschland Ltd & Co Kg Fluggasturbinenantrieb
US8701381B2 (en) * 2010-11-24 2014-04-22 Rolls-Royce Corporation Remote shaft driven open rotor propulsion system with electrical power generation
US9188083B2 (en) * 2011-10-28 2015-11-17 United Technologies Corporation Gas turbine engine with auxiliary fan
US8935912B2 (en) 2011-12-09 2015-01-20 United Technologies Corporation Gas turbine engine with variable overall pressure ratio
WO2013102113A2 (en) 2011-12-30 2013-07-04 Rolls-Royce North American Technologies Inc. Gas turbine engine with variable speed turbines
FR2998012B1 (fr) * 2012-11-09 2018-07-13 Safran Helicopter Engines Assemblage de compression pour turbomachine
US10036317B2 (en) * 2013-03-05 2018-07-31 Industrial Turbine Company (Uk) Limited Capacity control of turbine by the use of a reheat combustor in multi shaft engine
US9624829B2 (en) 2013-03-05 2017-04-18 Industrial Turbine Company (Uk) Limited Cogen heat load matching through reheat and capacity match
US9752500B2 (en) * 2013-03-14 2017-09-05 Pratt & Whitney Canada Corp. Gas turbine engine with transmission and method of adjusting rotational speed
GB201406386D0 (en) * 2014-04-09 2014-05-21 Rolls Royce Plc Gas turbine engine
US20160363003A1 (en) * 2014-08-15 2016-12-15 Gen Electric Mechanical drive architectures with hybrid-type low-loss bearings and low-density materials
US20160047335A1 (en) * 2014-08-15 2016-02-18 General Electric Company Mechanical drive architectures with mono-type low-loss bearings and low-density materials
US10711702B2 (en) * 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
FR3041934B1 (fr) * 2015-10-05 2018-07-13 Safran Aircraft Engines Ensemble de propulsion d'un aeronef
GB201518929D0 (en) * 2015-10-27 2015-12-09 Rolls Royce Plc Gas turbine engine
FR3056556B1 (fr) * 2016-09-29 2018-10-19 Safran Aircraft Engines Aeronef a turbomachine integree au fuselage arriere comportant une helice entourant un carter d'echappement
US10737801B2 (en) * 2016-10-31 2020-08-11 Rolls-Royce Corporation Fan module with rotatable vane ring power system
US10618667B2 (en) 2016-10-31 2020-04-14 Rolls-Royce Corporation Fan module with adjustable pitch blades and power system
GB201619960D0 (en) * 2016-11-25 2017-01-11 Rolls Royce Plc Gas turbine engine
GB201811401D0 (en) * 2018-07-12 2018-08-29 Rolls Royce Plc Supersonic aircraft propulsion installation
CN115956159A (zh) * 2020-07-13 2023-04-11 拉斐尔·马丁内斯-比拉诺瓦·皮农 用于航空器的喷气引擎
US11781479B2 (en) * 2021-05-06 2023-10-10 Rtx Corporation Turbofan gas turbine engine with combusted compressor bleed flow
CN113323769A (zh) * 2021-06-07 2021-08-31 北京航空航天大学 一种基于多涵道进气级间燃烧室的变循环发动机构型
CN114962063B (zh) * 2022-05-16 2024-08-13 中国航空发动机研究院 一种双低压系统的变循环航空发动机

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US2409177A (en) * 1942-04-01 1946-10-15 Allis Chalmers Mfg Co Jet propulsion apparatus
US2465099A (en) * 1943-11-20 1949-03-22 Allis Chalmers Mfg Co Propulsion means comprising an internal-combustion engine and a propulsive jet
GB588097A (en) * 1944-04-22 1947-05-14 Power Jets Res & Dev Ltd Improvements in or relating to internal combustion turbine power plants
US2619795A (en) * 1947-01-20 1952-12-02 Gen Electric Aircraft booster jet power unit
DE1077919B (de) * 1958-02-14 1960-03-17 Johann Endres Dr Ing Mehrkreis-Turbolader-Strahltriebwerk fuer Flugzeugantrieb mit getrennter Anordnung der Kreise
DE1081277B (de) * 1958-08-16 1960-05-05 Johann Endres Dr Ing Zweistrombrennkammer fuer Gasturbinen, insbesondere Gasturbinen-Strahltriebwerke
CH246174A (de) * 1959-06-24 1946-12-15 Eidg Flugzeugwerk Rückstosstriebwerk für Verkehrsmittel, insbesondere Flugzeuge.
US3016698A (en) * 1959-07-02 1962-01-16 Gen Motors Corp Bypass engine
US3677012A (en) * 1962-05-31 1972-07-18 Gen Electric Composite cycle turbomachinery
GB1069033A (en) * 1965-01-30 1967-05-17 Rolls Royce Improvements in or relating to gas turbine jet propulsion engines
US3632224A (en) * 1970-03-02 1972-01-04 Gen Electric Adjustable-blade turbine
US3938328A (en) * 1971-11-08 1976-02-17 The Boeing Company Multicycle engine
GB1338499A (en) * 1971-12-03 1973-11-21 Rolls Royce Gas turbine engine
US4025221A (en) * 1973-05-22 1977-05-24 United Turbine AB and Co., Kommanditbolag Automotive gas turbine power plant

Also Published As

Publication number Publication date
IT1097388B (it) 1985-08-31
AU519600B2 (en) 1981-12-10
GB1602699A (en) 1981-11-11
IT7826025A0 (it) 1978-07-24
AU3710278A (en) 1979-12-20
US4222235A (en) 1980-09-16
DE2831802A1 (de) 1979-02-15
JPS6153545B2 (ru) 1986-11-18
FR2398891B1 (ru) 1985-04-19
JPS5440912A (en) 1979-03-31
FR2398891A1 (fr) 1979-02-23
DE2831802C2 (ru) 1990-07-05

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