JPH0656131B2 - 混流式可変サイクルガスタ−ビンエンジンで推力増強装置ライナの冷却流圧力を制御する方法と装置 - Google Patents

混流式可変サイクルガスタ−ビンエンジンで推力増強装置ライナの冷却流圧力を制御する方法と装置

Info

Publication number
JPH0656131B2
JPH0656131B2 JP61045535A JP4553586A JPH0656131B2 JP H0656131 B2 JPH0656131 B2 JP H0656131B2 JP 61045535 A JP61045535 A JP 61045535A JP 4553586 A JP4553586 A JP 4553586A JP H0656131 B2 JPH0656131 B2 JP H0656131B2
Authority
JP
Japan
Prior art keywords
duct
flow
pressure
bypass
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.)
Expired - Lifetime
Application number
JP61045535A
Other languages
English (en)
Japanese (ja)
Other versions
JPS61241447A (ja
Inventor
ジヨン・ロバート・シモンズ
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 JPS61241447A publication Critical patent/JPS61241447A/ja
Publication of JPH0656131B2 publication Critical patent/JPH0656131B2/ja
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/16—Control of working fluid flow
    • F02C9/18—Control of working fluid flow by bleeding, bypassing or acting on variable working fluid interconnections between turbines or compressors or their stages
    • 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
    • F02C7/12—Cooling of plants
    • F02C7/16—Cooling of plants characterised by cooling medium
    • F02C7/18—Cooling of plants characterised by cooling medium the medium being gaseous, e.g. air
    • 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)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
JP61045535A 1985-03-04 1986-03-04 混流式可変サイクルガスタ−ビンエンジンで推力増強装置ライナの冷却流圧力を制御する方法と装置 Expired - Lifetime JPH0656131B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US70818185A 1985-03-04 1985-03-04
US708181 1985-03-04

Publications (2)

Publication Number Publication Date
JPS61241447A JPS61241447A (ja) 1986-10-27
JPH0656131B2 true JPH0656131B2 (ja) 1994-07-27

Family

ID=24844715

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61045535A Expired - Lifetime JPH0656131B2 (ja) 1985-03-04 1986-03-04 混流式可変サイクルガスタ−ビンエンジンで推力増強装置ライナの冷却流圧力を制御する方法と装置

Country Status (5)

Country Link
JP (1) JPH0656131B2 (fr)
DE (1) DE3606286A1 (fr)
FR (1) FR2578290B1 (fr)
GB (1) GB2172056B (fr)
IT (1) IT1188413B (fr)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE8915860U1 (de) * 1989-02-08 1991-12-05 Deutsche Forschungsanstalt für Luft- und Raumfahrt eV, 5300 Bonn Strahltriebwerk
US5178235A (en) * 1989-08-02 1993-01-12 The Montalvo Corporation Modular brakes and clutches
US5184461A (en) * 1990-05-11 1993-02-09 General Electric Company Method and apparatus for automatic bypass operation
US5113649A (en) * 1990-05-11 1992-05-19 General Electric Company Passive bypass valve assembly
US5048286A (en) * 1990-06-29 1991-09-17 General Electric Company Bypass valve door
US5161364A (en) * 1991-04-01 1992-11-10 United Technologies Corporation Control of aircraft bleed air stage mixing
FR2713749B1 (fr) * 1993-12-15 1996-01-12 Snecma Chambre de post combustion de turbine à gaz.
GB2289504B (en) * 1994-05-11 1998-01-14 British Aerospace Gas turbine propulsion unit
US7658063B1 (en) * 2005-07-15 2010-02-09 Florida Turbine Technologies, Inc. Gas turbine having a single shaft bypass configuration
US10030558B2 (en) * 2015-06-29 2018-07-24 General Electric Company Power generation system exhaust cooling
CN111237085B (zh) * 2020-03-16 2021-05-14 北京航空航天大学 一种涡轮发动机一二次流组合变循环方法

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB782654A (en) * 1953-09-14 1957-09-11 Rolls Royce Improvements in or relating to gas turbine engines
GB1135614A (en) * 1966-02-23 1968-12-04 Rolls Royce Fuel control system for a gas turbine engine
US3866417A (en) * 1973-02-09 1975-02-18 Gen Electric Gas turbine engine augmenter liner coolant flow control system
US4069661A (en) * 1975-06-02 1978-01-24 The United States Of America As Represented By The United States National Aeronautics And Space Administration Variable mixer propulsion cycle
US4010608A (en) * 1975-06-16 1977-03-08 General Electric Company Split fan work gas turbine engine
US4072008A (en) * 1976-05-04 1978-02-07 General Electric Company Variable area bypass injector system
US4159625A (en) * 1977-02-01 1979-07-03 United Technologies Corporation Control for gas turbine engine
US4175384A (en) * 1977-08-02 1979-11-27 General Electric Company Individual bypass injector valves for a double bypass variable cycle turbofan engine
US4285194A (en) * 1979-04-23 1981-08-25 General Electric Company Apparatus and method for controlling fan duct flow in a gas turbine engine
GB2065779B (en) * 1979-12-21 1983-09-21 Rolls Royce Gas turbine fuel system

Also Published As

Publication number Publication date
FR2578290B1 (fr) 1989-10-06
IT1188413B (it) 1988-01-14
GB2172056A (en) 1986-09-10
FR2578290A1 (fr) 1986-09-05
IT8619626A1 (it) 1987-09-04
GB8605215D0 (en) 1986-04-09
JPS61241447A (ja) 1986-10-27
DE3606286A1 (de) 1986-09-04
IT8619626A0 (it) 1986-03-04
GB2172056B (en) 1988-11-09

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