IT8619626A0 - Mezzi e metodo per controllare lapressione di un flusso di refrigerante di camicia di potenziatore in un turbomotore agas a flusso e ciclo variabile. - Google Patents

Mezzi e metodo per controllare lapressione di un flusso di refrigerante di camicia di potenziatore in un turbomotore agas a flusso e ciclo variabile.

Info

Publication number
IT8619626A0
IT8619626A0 IT8619626A IT1962686A IT8619626A0 IT 8619626 A0 IT8619626 A0 IT 8619626A0 IT 8619626 A IT8619626 A IT 8619626A IT 1962686 A IT1962686 A IT 1962686A IT 8619626 A0 IT8619626 A0 IT 8619626A0
Authority
IT
Italy
Prior art keywords
turboengine
agas
controling
enhancer
cycle
Prior art date
Application number
IT8619626A
Other languages
English (en)
Other versions
IT8619626A1 (it
IT1188413B (it
Inventor
John Robert Simmons
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 IT8619626A0 publication Critical patent/IT8619626A0/it
Publication of IT8619626A1 publication Critical patent/IT8619626A1/it
Application granted granted Critical
Publication of IT1188413B publication Critical patent/IT1188413B/it

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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
IT19626/86A 1985-03-04 1986-03-04 Mezzi e metodo per controllare la pressione di un flusso di refrigerante di camicia di potenziatore in un turbomotore a gas a flusso e ciclo variabile IT1188413B (it)

Applications Claiming Priority (1)

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

Publications (3)

Publication Number Publication Date
IT8619626A0 true IT8619626A0 (it) 1986-03-04
IT8619626A1 IT8619626A1 (it) 1987-09-04
IT1188413B IT1188413B (it) 1988-01-14

Family

ID=24844715

Family Applications (1)

Application Number Title Priority Date Filing Date
IT19626/86A IT1188413B (it) 1985-03-04 1986-03-04 Mezzi e metodo per controllare la pressione di un flusso di refrigerante di camicia di potenziatore in un turbomotore a gas a flusso e ciclo variabile

Country Status (5)

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

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
IT8619626A1 (it) 1987-09-04
JPH0656131B2 (ja) 1994-07-27
GB2172056B (en) 1988-11-09
GB8605215D0 (en) 1986-04-09
GB2172056A (en) 1986-09-10
DE3606286A1 (de) 1986-09-04
FR2578290B1 (fr) 1989-10-06
FR2578290A1 (fr) 1986-09-05
IT1188413B (it) 1988-01-14
JPS61241447A (ja) 1986-10-27

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Legal Events

Date Code Title Description
TA Fee payment date (situation as of event date), data collected since 19931001

Effective date: 19930323