FR2313565A1 - Moteur a turbine a gaz a by-pass reglable et procede pour commander ce moteur - Google Patents

Moteur a turbine a gaz a by-pass reglable et procede pour commander ce moteur

Info

Publication number
FR2313565A1
FR2313565A1 FR7616703A FR7616703A FR2313565A1 FR 2313565 A1 FR2313565 A1 FR 2313565A1 FR 7616703 A FR7616703 A FR 7616703A FR 7616703 A FR7616703 A FR 7616703A FR 2313565 A1 FR2313565 A1 FR 2313565A1
Authority
FR
France
Prior art keywords
engine
adjustable
pass
control
gas turbine
Prior art date
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.)
Granted
Application number
FR7616703A
Other languages
English (en)
Other versions
FR2313565B1 (fr
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
General Electric Co
Original Assignee
General Electric Co
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 General Electric Co filed Critical General Electric Co
Publication of FR2313565A1 publication Critical patent/FR2313565A1/fr
Application granted granted Critical
Publication of FR2313565B1 publication Critical patent/FR2313565B1/fr
Granted legal-status Critical Current

Links

Classifications

    • 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
FR7616703A 1975-06-02 1976-06-02 Moteur a turbine a gaz a by-pass reglable et procede pour commander ce moteur Granted FR2313565A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/583,055 US4069661A (en) 1975-06-02 1975-06-02 Variable mixer propulsion cycle

Publications (2)

Publication Number Publication Date
FR2313565A1 true FR2313565A1 (fr) 1976-12-31
FR2313565B1 FR2313565B1 (fr) 1983-01-07

Family

ID=24331511

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7616703A Granted FR2313565A1 (fr) 1975-06-02 1976-06-02 Moteur a turbine a gaz a by-pass reglable et procede pour commander ce moteur

Country Status (8)

Country Link
US (1) US4069661A (fr)
JP (1) JPS6018826B2 (fr)
BE (1) BE842433A (fr)
CA (1) CA1053011A (fr)
DE (1) DE2624282C2 (fr)
FR (1) FR2313565A1 (fr)
GB (1) GB1544454A (fr)
IT (1) IT1060787B (fr)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2578290A1 (fr) * 1985-03-04 1986-09-05 Gen Electric Procede et moyen de reglage de la pression d'un fluide de refroidissement de la chemise d'un systeme de post-combustion pour moteur a cycle variable
FR2646474A1 (fr) * 1989-04-26 1990-11-02 Gen Electric Moyens et procede pour reduire la charge due a la pression differentielle dans un moteur a turbine a gaz comportant une chambre de post-combustion
EP1995442A2 (fr) * 2007-05-25 2008-11-26 General Electric Company Ensemble de moteur à turbine et procédé de montage correspondant
WO2013184042A2 (fr) * 2012-06-09 2013-12-12 Kostyukov Vladimir Nikolaevich Turbomachine à étages multiples (variantes)
RU175183U1 (ru) * 2016-12-29 2017-11-24 Федеральное государственное автономное образовательное учреждение высшего образования "Санкт-Петербургский политехнический университет Петра Великого" Осевая турбина
FR3081149A1 (fr) * 2018-05-17 2019-11-22 Safran Nacelles Nacelle pour turboreacteur d’aeronef et ensemble propulsif comportant une telle nacelle

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US5694767A (en) * 1981-11-02 1997-12-09 General Electric Company Variable slot bypass injector system
GB2305976B (en) * 1981-12-21 1998-01-07 British Aerospace Jet propulsion powerplants
US4461145A (en) * 1982-10-08 1984-07-24 The United States Of America As Represented By The Secretary Of The Air Force Stall elimination and restart enhancement device
DE3441288A1 (de) * 1984-04-24 1985-10-31 Paul Schneider Rohrleitungsbau GmbH, 8633 Rödental Verfahren zur waerme- und/oder mittels eines gasfoermigen reagens durchgefuehrten chemischen behandlung von gut in einem langgestreckten behandlungsraum und behandlungsraum zur durchfuehrung des verfahrens
GB2165892B (en) * 1984-10-22 1988-10-26 Gen Electric Variable cycle engine
US5680754A (en) * 1990-02-12 1997-10-28 General Electric Company Compressor splitter for use with a forward variable area bypass injector
US5307624A (en) * 1990-04-04 1994-05-03 General Electric Company Variable area bypass valve assembly
US5231825A (en) * 1990-04-09 1993-08-03 General Electric Company Method for compressor air extraction
US5155993A (en) * 1990-04-09 1992-10-20 General Electric Company Apparatus for compressor air extraction
US5113649A (en) * 1990-05-11 1992-05-19 General Electric Company Passive bypass valve assembly
US5184461A (en) * 1990-05-11 1993-02-09 General Electric Company Method and apparatus for automatic bypass operation
US5054286A (en) * 1990-06-29 1991-10-08 General Electric Company Bypass valve system
US5048286A (en) * 1990-06-29 1991-09-17 General Electric Company Bypass valve door
FR2685385B1 (fr) * 1991-12-24 1995-03-31 Snecma Moteur de propulsion a cycle variable pour avion supersonique.
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
US5381655A (en) * 1993-05-10 1995-01-17 General Electric Company Admission mixing duct assembly
US5404713A (en) * 1993-10-04 1995-04-11 General Electric Company Spillage drag and infrared reducing flade engine
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
US7093442B2 (en) * 2003-04-30 2006-08-22 United Technologies Corporation Augmentor
US7334409B2 (en) * 2004-05-19 2008-02-26 Alltech, Inc. Retractable afterburner for jet engine
US7762084B2 (en) * 2004-11-12 2010-07-27 Rolls-Royce Canada, Ltd. System and method for controlling the working line position in a gas turbine engine compressor
US7424805B2 (en) * 2005-04-29 2008-09-16 General Electric Company Supersonic missile turbojet engine
US7509797B2 (en) * 2005-04-29 2009-03-31 General Electric Company Thrust vectoring missile turbojet
US7475545B2 (en) * 2005-04-29 2009-01-13 General Electric Company Fladed supersonic missile turbojet
US7448199B2 (en) * 2005-04-29 2008-11-11 General Electric Company Self powdered missile turbojet
US7475532B2 (en) * 2005-08-29 2009-01-13 General Electric Company Valve assembly for a gas turbine engine
US7730714B2 (en) * 2005-11-29 2010-06-08 General Electric Company Turbofan gas turbine engine with variable fan outlet guide vanes
US7614210B2 (en) * 2006-02-13 2009-11-10 General Electric Company Double bypass turbofan
US7717667B2 (en) * 2006-09-29 2010-05-18 General Electric Company Method and apparatus for operating gas turbine engines
US7770381B2 (en) * 2006-12-18 2010-08-10 General Electric Company Duct burning mixed flow turbofan and method of operation
US7877980B2 (en) * 2006-12-28 2011-02-01 General Electric Company Convertible gas turbine engine
RU2447308C2 (ru) * 2010-07-09 2012-04-10 Федеральное государственное унитарное предприятие "Летно-исследовательский институт имени М.М. Громова" Турбореактивный двухконтурный двигатель с перераспределением энергии потока воздуха на входе
US8961114B2 (en) 2010-11-22 2015-02-24 General Electric Company Integrated variable geometry flow restrictor and heat exchanger
US8938943B2 (en) * 2010-12-28 2015-01-27 Rolls-Royce North American Technoloies, Inc. Gas turbine engine with bypass mixer
US9057328B2 (en) * 2011-11-01 2015-06-16 United Technologies Corporation Gas turbine engine with intercooling turbine section
US20130104522A1 (en) * 2011-11-01 2013-05-02 Daniel B. Kupratis Gas turbine engine with variable pitch first stage fan section
US9279388B2 (en) * 2011-11-01 2016-03-08 United Technologies Corporation Gas turbine engine with two-spool fan and variable vane turbine
FR2983917B1 (fr) * 2011-12-07 2013-12-27 Snecma Tuyere convergente-divergente de turbomachine
US20130192195A1 (en) 2012-01-31 2013-08-01 Eric J. Wehmeier Gas turbine engine with compressor inlet guide vane positioned for starting
US8291690B1 (en) * 2012-01-31 2012-10-23 United Technologies Corporation Gas turbine engine with variable area fan nozzle positioned for starting
US9157366B2 (en) * 2012-05-30 2015-10-13 United Technologies Corporation Adaptive fan with cold turbine
US9341075B2 (en) * 2012-06-25 2016-05-17 United Technologies Corporation Pre-turbine engine case variable area mixing plane
US10400710B2 (en) 2013-05-07 2019-09-03 General Electric Company Secondary nozzle for jet engine
US9920710B2 (en) 2013-05-07 2018-03-20 General Electric Company Multi-nozzle flow diverter for jet engine
US9909529B2 (en) * 2013-09-20 2018-03-06 United Technologies Corporation Flow path routing within a gas turbine engine
US10371090B2 (en) 2014-01-13 2019-08-06 United Technologies Corporation Variable area exhaust mixer for a gas turbine engine
US10030606B2 (en) 2014-01-27 2018-07-24 United Technologies Corporation Variable exhaust mixer and cooler for a three-stream gas turbine engine
JP6264161B2 (ja) * 2014-04-04 2018-01-24 株式会社Ihi ジェットエンジン
DE102014221049A1 (de) * 2014-10-16 2016-04-21 Rolls-Royce Deutschland Ltd & Co Kg Anordnung und Verfahren zum Abblasen von Verdichterluft in einem Triebwerk
WO2016189712A1 (fr) 2015-05-27 2016-12-01 株式会社Ihi Moteur à réaction
US10215070B2 (en) * 2015-06-29 2019-02-26 General Electric Company Power generation system exhaust cooling
US10060316B2 (en) * 2015-06-29 2018-08-28 General Electric Company Power generation system exhaust cooling
US20160376908A1 (en) * 2015-06-29 2016-12-29 General Electric Company Power generation system exhaust cooling
US9840953B2 (en) 2015-06-29 2017-12-12 General Electric Company Power generation system exhaust cooling
US10030558B2 (en) * 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
US9850794B2 (en) * 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US9856768B2 (en) 2015-06-29 2018-01-02 General Electric Company Power generation system exhaust cooling
US10077694B2 (en) * 2015-06-29 2018-09-18 General Electric Company Power generation system exhaust cooling
US10087801B2 (en) * 2015-06-29 2018-10-02 General Electric Company Power generation system exhaust cooling
US9938874B2 (en) * 2015-06-29 2018-04-10 General Electric Company Power generation system exhaust cooling
US9850818B2 (en) 2015-06-29 2017-12-26 General Electric Company Power generation system exhaust cooling
US20160376909A1 (en) * 2015-06-29 2016-12-29 General Electric Company Power generation system exhaust cooling
US10578028B2 (en) 2015-08-18 2020-03-03 General Electric Company Compressor bleed auxiliary turbine
US10711702B2 (en) * 2015-08-18 2020-07-14 General Electric Company Mixed flow turbocore
US10151217B2 (en) * 2016-02-11 2018-12-11 General Electric Company Turbine frame cooling systems and methods of assembly for use in a gas turbine engine
US20170307311A1 (en) * 2016-04-26 2017-10-26 United Technologies Corporation Simple Heat Exchanger Using Super Alloy Materials for Challenging Applications
US10316759B2 (en) 2016-05-31 2019-06-11 General Electric Company Power generation system exhaust cooling
US9926883B1 (en) * 2017-02-11 2018-03-27 Florida Turbine Technologies, Inc. Gas turbine engine with axial flow fan with twin stream impeller and variable area bypass nozzle
US11125187B2 (en) 2018-08-01 2021-09-21 Raytheon Technologies Corporation Turbomachinery transition duct for wide bypass ratio ranges
CN113048511A (zh) * 2021-02-03 2021-06-29 南京航空航天大学 一种ai调控的加力燃烧室内外涵掺混装置
CN114076324B (zh) * 2022-01-19 2022-07-08 中国航发四川燃气涡轮研究院 能够自动调节掺混进气的燃烧室

Citations (9)

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US2458600A (en) * 1942-01-26 1949-01-11 Rateau Soc Aerodynamic propelling means operating through direct reaction jet and scavenging
FR1052152A (fr) * 1952-03-06 1954-01-21 Havilland Engine Co Ltd Perfectionnements aux installations de combustion interne du type turbo-machines
FR1217723A (fr) * 1957-12-02 1960-05-05 Le Ministre De La Defense Nati Installation propulsive à tuyère finale à section variable pour aéronefs
FR1306025A (fr) * 1961-08-08 1962-10-13 Snecma Mélangeur à coefficient de blocage variable dans les réacteurs à double flux à flux mélangés
FR79090E (fr) * 1960-07-11 1962-10-19 Nord Aviation Combiné turboréacteur-statoréacteur
FR1377199A (fr) * 1963-12-17 1964-10-31 Rolls Royce Moteur à turbine à gaz
GB1009314A (en) * 1963-09-10 1965-11-10 Gen Motors Corp By-pass gas turbine engines
US3432100A (en) * 1966-04-20 1969-03-11 Snecma Ejecting nozzle for propellers provided with a plurality of driving streams and,more particularly,two driving streams
US3514952A (en) * 1964-07-01 1970-06-02 Us Air Force Variable bypass turbofan engine

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US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
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FR1271544A (fr) * 1960-07-11 1961-09-15 Nord Aviation Combiné turboréacteur-statoréacteur
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Publication number Priority date Publication date Assignee Title
US2458600A (en) * 1942-01-26 1949-01-11 Rateau Soc Aerodynamic propelling means operating through direct reaction jet and scavenging
FR1052152A (fr) * 1952-03-06 1954-01-21 Havilland Engine Co Ltd Perfectionnements aux installations de combustion interne du type turbo-machines
FR1217723A (fr) * 1957-12-02 1960-05-05 Le Ministre De La Defense Nati Installation propulsive à tuyère finale à section variable pour aéronefs
FR79090E (fr) * 1960-07-11 1962-10-19 Nord Aviation Combiné turboréacteur-statoréacteur
FR1306025A (fr) * 1961-08-08 1962-10-13 Snecma Mélangeur à coefficient de blocage variable dans les réacteurs à double flux à flux mélangés
GB1009314A (en) * 1963-09-10 1965-11-10 Gen Motors Corp By-pass gas turbine engines
FR1377199A (fr) * 1963-12-17 1964-10-31 Rolls Royce Moteur à turbine à gaz
US3514952A (en) * 1964-07-01 1970-06-02 Us Air Force Variable bypass turbofan engine
US3432100A (en) * 1966-04-20 1969-03-11 Snecma Ejecting nozzle for propellers provided with a plurality of driving streams and,more particularly,two driving streams

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2578290A1 (fr) * 1985-03-04 1986-09-05 Gen Electric Procede et moyen de reglage de la pression d'un fluide de refroidissement de la chemise d'un systeme de post-combustion pour moteur a cycle variable
FR2646474A1 (fr) * 1989-04-26 1990-11-02 Gen Electric Moyens et procede pour reduire la charge due a la pression differentielle dans un moteur a turbine a gaz comportant une chambre de post-combustion
EP1995442A2 (fr) * 2007-05-25 2008-11-26 General Electric Company Ensemble de moteur à turbine et procédé de montage correspondant
EP1995442A3 (fr) * 2007-05-25 2012-05-30 General Electric Company Ensemble de moteur à turbine et procédé de montage correspondant
WO2013184042A2 (fr) * 2012-06-09 2013-12-12 Kostyukov Vladimir Nikolaevich Turbomachine à étages multiples (variantes)
WO2013184042A3 (fr) * 2012-06-09 2014-01-30 Kostyukov Vladimir Nikolaevich Turbomachine à étages multiples (variantes)
RU175183U1 (ru) * 2016-12-29 2017-11-24 Федеральное государственное автономное образовательное учреждение высшего образования "Санкт-Петербургский политехнический университет Петра Великого" Осевая турбина
FR3081149A1 (fr) * 2018-05-17 2019-11-22 Safran Nacelles Nacelle pour turboreacteur d’aeronef et ensemble propulsif comportant une telle nacelle

Also Published As

Publication number Publication date
BE842433A (fr) 1976-10-01
JPS6018826B2 (ja) 1985-05-13
DE2624282C2 (de) 1986-04-24
DE2624282A1 (de) 1976-12-16
GB1544454A (en) 1979-04-19
FR2313565B1 (fr) 1983-01-07
IT1060787B (it) 1982-09-30
JPS521221A (en) 1977-01-07
US4069661A (en) 1978-01-24
CA1053011A (fr) 1979-04-24

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