CA1031972A - Regulateur de combustion pour moteur de turbine a gaz - Google Patents

Regulateur de combustion pour moteur de turbine a gaz

Info

Publication number
CA1031972A
CA1031972A CA233,388A CA233388A CA1031972A CA 1031972 A CA1031972 A CA 1031972A CA 233388 A CA233388 A CA 233388A CA 1031972 A CA1031972 A CA 1031972A
Authority
CA
Canada
Prior art keywords
gas turbine
turbine engine
combustion control
combustion
control
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
Application number
CA233,388A
Other languages
English (en)
Other versions
CA233388S (en
Inventor
Alan L. Hitzelberger
Donald J. Armstrong
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.)
Motors Liquidation Co
Original Assignee
General Motors Corp
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 Motors Corp filed Critical General Motors Corp
Application granted granted Critical
Publication of CA1031972A publication Critical patent/CA1031972A/fr
Expired 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
    • F02C9/26—Control of fuel supply
    • F02C9/38—Control of fuel supply characterised by throttling and returning of fuel to sump
    • 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
    • F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
    • F02C3/04—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor
    • F02C3/10—Gas-turbine plants characterised by the use of combustion products as the working fluid having a turbine driving a compressor with another turbine driving an output shaft but not driving the compressor
    • 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
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/26—Controlling the air flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)
  • Measuring Volume Flow (AREA)
CA233,388A 1974-11-04 1975-08-13 Regulateur de combustion pour moteur de turbine a gaz Expired CA1031972A (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US520452A US3919838A (en) 1974-11-04 1974-11-04 Combustion control

Publications (1)

Publication Number Publication Date
CA1031972A true CA1031972A (fr) 1978-05-30

Family

ID=24072649

Family Applications (1)

Application Number Title Priority Date Filing Date
CA233,388A Expired CA1031972A (fr) 1974-11-04 1975-08-13 Regulateur de combustion pour moteur de turbine a gaz

Country Status (5)

Country Link
US (1) US3919838A (fr)
JP (1) JPS5169710A (fr)
CA (1) CA1031972A (fr)
DE (1) DE2545468A1 (fr)
GB (1) GB1485228A (fr)

Families Citing this family (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3977182A (en) * 1975-06-20 1976-08-31 General Motors Corporation Gas turbine control
EP0100135B1 (fr) * 1982-07-22 1986-06-11 The Garrett Corporation Chambre de combustion
US4497170A (en) * 1982-07-22 1985-02-05 The Garrett Corporation Actuation system for a variable geometry combustor
US4594848A (en) * 1982-07-22 1986-06-17 The Garrett Corporation Gas turbine combustor operating method
US4532762A (en) * 1982-07-22 1985-08-06 The Garrett Corporation Gas turbine engine variable geometry combustor apparatus
GB2197910A (en) * 1986-11-27 1988-06-02 Orian Emilia Modular gas turbine plant
US4813226A (en) * 1987-01-12 1989-03-21 Grosselfinger Robert A Demand control of variable geometry gas turbine power plant
US5002459A (en) * 1988-07-28 1991-03-26 Rotoflow Corporation Surge control system
US5617719A (en) * 1992-10-27 1997-04-08 Ginter; J. Lyell Vapor-air steam engine
USRE43252E1 (en) 1992-10-27 2012-03-20 Vast Power Portfolio, Llc High efficiency low pollution hybrid Brayton cycle combustor
US5309710A (en) * 1992-11-20 1994-05-10 General Electric Company Gas turbine combustor having poppet valves for air distribution control
US5319931A (en) * 1992-12-30 1994-06-14 General Electric Company Fuel trim method for a multiple chamber gas turbine combustion system
EP0646705B1 (fr) * 1993-09-06 1999-06-09 Asea Brown Boveri Ag Procédé pour produire des régimes de fonctionnement partiel dans une installation pour turbine à gaz
DE69421896T2 (de) * 1993-12-22 2000-05-31 Siemens Westinghouse Power Corp., Orlando Umleitungsventil für die Brennkammer einer Gasturbine
DE19545311B4 (de) * 1995-12-05 2006-09-14 Alstom Verfahren zur Betrieb einer mit Vormischbrennern bestückten Brennkammer
GB2351343A (en) * 1999-06-22 2000-12-27 Alstom Gas Turbines Ltd Telescopically-moveable combustion chamber
US6609362B2 (en) 2001-07-13 2003-08-26 Pratt & Whitney Canada Corp. Apparatus for adjusting combustor cycle
US8099941B2 (en) * 2008-12-31 2012-01-24 General Electric Company Methods and systems for controlling a combustor in turbine engines
US10738697B2 (en) * 2017-06-23 2020-08-11 Hamilton Sundstrand Corporation Parallel combustor configuration for unmanned underwater vehicle propulsion turbine

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2227666A (en) * 1936-12-10 1941-01-07 Bbc Brown Boveri & Cie Starting up system for heat producing and consuming plants
US3618319A (en) * 1966-08-02 1971-11-09 Gen Electric Main combustion system and combustion process
US3584459A (en) * 1968-09-12 1971-06-15 Gen Motors Corp Gas turbine engine with combustion chamber bypass for fuel-air ratio control and turbine cooling

Also Published As

Publication number Publication date
DE2545468A1 (de) 1976-05-13
US3919838A (en) 1975-11-18
JPS5169710A (fr) 1976-06-16
GB1485228A (en) 1977-09-08

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