JPS55142937A - Operating device for gas turbine engine - Google Patents

Operating device for gas turbine engine

Info

Publication number
JPS55142937A
JPS55142937A JP5049980A JP5049980A JPS55142937A JP S55142937 A JPS55142937 A JP S55142937A JP 5049980 A JP5049980 A JP 5049980A JP 5049980 A JP5049980 A JP 5049980A JP S55142937 A JPS55142937 A JP S55142937A
Authority
JP
Japan
Prior art keywords
gas turbine
turbine engine
operating device
engine
operating
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
JP5049980A
Other languages
English (en)
Japanese (ja)
Other versions
JPS642774B2 (xx
Inventor
Ooen Natsushiyu Datsudorei
Shimonzu Kureiton Toomasu
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 JPS55142937A publication Critical patent/JPS55142937A/ja
Publication of JPS642774B2 publication Critical patent/JPS642774B2/ja
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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Toys (AREA)
JP5049980A 1979-04-23 1980-04-18 Operating device for gas turbine engine Granted JPS55142937A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US3233079A 1979-04-23 1979-04-23

Publications (2)

Publication Number Publication Date
JPS55142937A true JPS55142937A (en) 1980-11-07
JPS642774B2 JPS642774B2 (xx) 1989-01-18

Family

ID=21864363

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5049980A Granted JPS55142937A (en) 1979-04-23 1980-04-18 Operating device for gas turbine engine

Country Status (6)

Country Link
JP (1) JPS55142937A (xx)
DE (1) DE3015119A1 (xx)
FR (1) FR2455179A1 (xx)
GB (1) GB2047815B (xx)
IL (1) IL59497A (xx)
IT (1) IT1131033B (xx)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58200038A (ja) * 1982-05-18 1983-11-21 ゼネラル・エレクトリツク・カンパニイ ガスタ−ビン機関の作動装置
JP2004108364A (ja) * 2002-09-13 2004-04-08 General Electric Co <Ge> 可変バイパス弁システムを支持するための方法及び装置
JP2005113919A (ja) * 2003-10-07 2005-04-28 General Electric Co <Ge> 可変圧力比ファンシステムを有するガスタービンエンジン

Families Citing this family (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2527688B1 (fr) * 1982-06-01 1987-03-27 Gen Electric Systeme de manoeuvre d'un element monte a l'interieur d'un carter
US5417055A (en) * 1988-06-28 1995-05-23 Rolls-Royce Plc Valve for diverting fluid flows in turbomachines
GB8815292D0 (en) * 1988-06-28 1994-10-26 Rolls Royce Plc Valve for diverting fluid flows in turbomachines
DE3911715A1 (de) * 1989-04-10 1990-10-11 Mtu Muenchen Gmbh Absperreinrichtung fuer geblaese-, insbesondere geblaese-staustrahltriebwerke
DE4004416C2 (de) * 1990-02-13 1993-10-14 Mtu Muenchen Gmbh Turbo-Staustrahltriebwerk mit Absperreinrichtung für variablen Umschaltbetrieb
US5123240A (en) * 1990-03-19 1992-06-23 General Electric Co. Method and apparatus for ejecting foreign matter from the primary flow path of a gas turbine engine
CA2036821A1 (en) * 1990-06-29 1991-12-30 Larry W. Stransky Bypass valve system
GB2259328B (en) * 1991-09-03 1995-07-19 Gen Electric Gas turbine engine variable bleed pivotal flow splitter
US5287697A (en) * 1992-01-02 1994-02-22 General Electric Company Variable area bypass injector seal
FR2926328B1 (fr) * 2008-01-14 2015-08-07 Snecma Turbomachine a double flux comportant une veine primaire et un bec mobile dans cette veine primaire
US20120070271A1 (en) 2010-09-21 2012-03-22 Urban Justin R Gas turbine engine with bleed duct for minimum reduction of bleed flow and minimum rejection of hail during hail ingestion events
US8935926B2 (en) 2010-10-28 2015-01-20 United Technologies Corporation Centrifugal compressor with bleed flow splitter for a gas turbine engine
DE102011101331A1 (de) * 2011-05-12 2012-11-15 Rolls-Royce Deutschland Ltd & Co Kg Gasturbinentriebwerk mit Zapfluftentnahmevorrichtung
CN109162829B (zh) * 2018-09-04 2019-08-23 中国航发沈阳发动机研究所 变循环发动机的压缩系统
CN111636978B (zh) * 2020-06-16 2021-06-18 南京航空航天大学 一种适用于涡轮基循环组合发动机的流量调节机构

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3060680A (en) * 1957-12-30 1962-10-30 Rolls Royce By-pass gas-turbine engine and control therefor
GB864519A (en) * 1958-08-05 1961-04-06 Rolls Royce Improved annular fluid control valve device
US2934895A (en) * 1958-09-15 1960-05-03 Curtiss Wright Corp Dual cycle engine distributor construction
US3153904A (en) * 1961-12-29 1964-10-27 Stanley H Ellis Turbo-ramjet configuration
GB1124169A (en) * 1967-04-07 1968-08-21 Rolls Royce Mechanism e.g. for use in a jet nozzle
GB1300405A (en) * 1969-06-25 1972-12-20 Secr Defence Improvements in nozzles for gas turbine jet propulsion engines
FR2085470B1 (xx) * 1970-04-23 1974-05-03 Snecma
US3638428A (en) * 1970-05-04 1972-02-01 Gen Electric Bypass valve mechanism
DE2247400C2 (de) * 1972-09-27 1975-01-16 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Vorrichtung zum Abblasen von verdichteter Luft aus einem Verdichter eines Gasturbinenstrahltriebwerks
US4175384A (en) * 1977-08-02 1979-11-27 General Electric Company Individual bypass injector valves for a double bypass variable cycle turbofan engine
DE2740904A1 (de) * 1977-09-10 1979-03-22 Motoren Turbinen Union Vorrichtung zur betaetigung von absperrorganen in gasturbinentriebwerken, insbesondere gasturbinenstrahltriebwerken

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPS58200038A (ja) * 1982-05-18 1983-11-21 ゼネラル・エレクトリツク・カンパニイ ガスタ−ビン機関の作動装置
JP2004108364A (ja) * 2002-09-13 2004-04-08 General Electric Co <Ge> 可変バイパス弁システムを支持するための方法及び装置
JP4641713B2 (ja) * 2002-09-13 2011-03-02 ゼネラル・エレクトリック・カンパニイ 可変バイパス弁システムを支持するための方法及び装置
JP2005113919A (ja) * 2003-10-07 2005-04-28 General Electric Co <Ge> 可変圧力比ファンシステムを有するガスタービンエンジン
JP4559180B2 (ja) * 2003-10-07 2010-10-06 ゼネラル・エレクトリック・カンパニイ 可変圧力比ファンシステムを有するガスタービンエンジン

Also Published As

Publication number Publication date
IT8020837A0 (it) 1980-03-21
FR2455179A1 (fr) 1980-11-21
FR2455179B1 (xx) 1984-07-20
JPS642774B2 (xx) 1989-01-18
IT1131033B (it) 1986-06-18
DE3015119A1 (de) 1980-11-06
IL59497A0 (en) 1980-05-30
GB2047815A (en) 1980-12-03
GB2047815B (en) 1983-03-30
IL59497A (en) 1984-08-31

Similar Documents

Publication Publication Date Title
JPS5681228A (en) Device for sealing gas turbine engine
GB2047354B (en) Gas turbine engines
JPS5560624A (en) Airrcooled turbine for gas turbine engine
JPS53131313A (en) Turbine for gas turbine engine
JPS55128626A (en) Cowling for gas turbine engine
GB2006881B (en) Combustion apparatus for gas turbine engines
JPS55123924A (en) Gas turbine engine
JPS5625607A (en) Duplex fufl injection device for gas turbine engine
GB2062763B (en) Gas turbine engine cooling
GB2027866B (en) Gas turbine engine comounting
JPS5575537A (en) Gas turbine engine
JPS5587826A (en) Gas turbine engine
JPS5647628A (en) Controller for gas turbine engine
JPS55131531A (en) Gas turbine engine
GB1545365A (en) Gas turbine engines
JPS55142937A (en) Operating device for gas turbine engine
GB2004329B (en) Gas turbine engines
JPS566004A (en) Gas turbine engine
GB2007302B (en) Gas turbine engine
DE3061595D1 (en) Combustion apparatus for gas turbine engines
JPS5677629A (en) Gas turbine engine for automobile
JPS55139935A (en) Gas turbine engine
GB2044361B (en) Gas turbine engine
GB2038425B (en) Gas turbine engine
JPS54111007A (en) Gas turbine engine