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DE69523992D1 - Regelung einer Gasturbinenbrennkammer - Google Patents

Regelung einer Gasturbinenbrennkammer

Info

Publication number
DE69523992D1
DE69523992D1 DE69523992T DE69523992T DE69523992D1 DE 69523992 D1 DE69523992 D1 DE 69523992D1 DE 69523992 T DE69523992 T DE 69523992T DE 69523992 T DE69523992 T DE 69523992T DE 69523992 D1 DE69523992 D1 DE 69523992D1
Authority
DE
Germany
Prior art keywords
regulation
combustion chamber
gas turbine
turbine combustion
gas
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 - Fee Related
Application number
DE69523992T
Other languages
English (en)
Other versions
DE69523992T2 (de
Inventor
Davis, Jr
Warren J Mick
David Orus Fitts
Michael Bruce Sciochetti
Mitchell R Cohen
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
Application granted granted Critical
Publication of DE69523992D1 publication Critical patent/DE69523992D1/de
Publication of DE69523992T2 publication Critical patent/DE69523992T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • 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
    • F02C7/22—Fuel supply systems
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34—Feeding into different combustion zones
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • 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
    • F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE69523992T 1994-06-10 1995-05-12 Regelung einer Gasturbinenbrennkammer Expired - Fee Related DE69523992T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/258,112 US5491970A (en) 1994-06-10 1994-06-10 Method for staging fuel in a turbine between diffusion and premixed operations

Publications (2)

Publication Number Publication Date
DE69523992D1 true DE69523992D1 (de) 2002-01-03
DE69523992T2 DE69523992T2 (de) 2002-08-29

Family

ID=22979142

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69523992T Expired - Fee Related DE69523992T2 (de) 1994-06-10 1995-05-12 Regelung einer Gasturbinenbrennkammer

Country Status (5)

Country Link
US (1) US5491970A (de)
EP (1) EP0691511B1 (de)
JP (1) JP3477274B2 (de)
KR (1) KR100372907B1 (de)
DE (1) DE69523992T2 (de)

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US9822649B2 (en) * 2008-11-12 2017-11-21 General Electric Company Integrated combustor and stage 1 nozzle in a gas turbine and method
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US9267443B2 (en) 2009-05-08 2016-02-23 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
US9671797B2 (en) 2009-05-08 2017-06-06 Gas Turbine Efficiency Sweden Ab Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications
US8437941B2 (en) 2009-05-08 2013-05-07 Gas Turbine Efficiency Sweden Ab Automated tuning of gas turbine combustion systems
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US8720206B2 (en) * 2009-05-14 2014-05-13 General Electric Company Methods and systems for inducing combustion dynamics
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US9003761B2 (en) 2010-05-28 2015-04-14 General Electric Company System and method for exhaust gas use in gas turbine engines
US8984895B2 (en) 2010-07-09 2015-03-24 Icr Turbine Engine Corporation Metallic ceramic spool for a gas turbine engine
US9557050B2 (en) 2010-07-30 2017-01-31 General Electric Company Fuel nozzle and assembly and gas turbine comprising the same
CA2813680A1 (en) 2010-09-03 2012-03-08 Icr Turbine Engine Corporation Gas turbine engine configurations
US9488105B2 (en) * 2010-12-01 2016-11-08 Siemens Aktiengesellschaft Gas turbine assembly and method therefor
US20120183911A1 (en) * 2011-01-18 2012-07-19 General Electric Company Combustor and a method for repairing a combustor
US9068750B2 (en) * 2011-03-04 2015-06-30 General Electric Company Combustor with a pre-nozzle mixing cap assembly
US9051873B2 (en) 2011-05-20 2015-06-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine shaft attachment
EP2551470A1 (de) * 2011-07-26 2013-01-30 Siemens Aktiengesellschaft Verfahren zum Hochfahren einer stationären Gasturbine
US20130040254A1 (en) * 2011-08-08 2013-02-14 General Electric Company System and method for monitoring a combustor
US20130192237A1 (en) * 2012-01-31 2013-08-01 Solar Turbines Inc. Fuel injector system with fluidic oscillator
US9341376B2 (en) * 2012-02-20 2016-05-17 General Electric Company Combustor and method for supplying fuel to a combustor
US9395084B2 (en) * 2012-06-06 2016-07-19 General Electric Company Fuel pre-mixer with planar and swirler vanes
US9310072B2 (en) 2012-07-06 2016-04-12 Hamilton Sundstrand Corporation Non-symmetric arrangement of fuel nozzles in a combustor
US10094288B2 (en) 2012-07-24 2018-10-09 Icr Turbine Engine Corporation Ceramic-to-metal turbine volute attachment for a gas turbine engine
US10215412B2 (en) * 2012-11-02 2019-02-26 General Electric Company System and method for load control with diffusion combustion in a stoichiometric exhaust gas recirculation gas turbine system
US9291098B2 (en) * 2012-11-14 2016-03-22 General Electric Company Turbomachine and staged combustion system of a turbomachine
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Also Published As

Publication number Publication date
JP3477274B2 (ja) 2003-12-10
DE69523992T2 (de) 2002-08-29
US5491970A (en) 1996-02-20
EP0691511B1 (de) 2001-11-21
KR960001441A (ko) 1996-01-25
JPH0854120A (ja) 1996-02-27
EP0691511A1 (de) 1996-01-10
KR100372907B1 (ko) 2003-04-26

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: ROEGER UND KOLLEGEN, 73728 ESSLINGEN

8339 Ceased/non-payment of the annual fee