DE3866856D1 - Brennkammer fuer eine gasturbine. - Google Patents

Brennkammer fuer eine gasturbine.

Info

Publication number
DE3866856D1
DE3866856D1 DE8888117859T DE3866856T DE3866856D1 DE 3866856 D1 DE3866856 D1 DE 3866856D1 DE 8888117859 T DE8888117859 T DE 8888117859T DE 3866856 T DE3866856 T DE 3866856T DE 3866856 D1 DE3866856 D1 DE 3866856D1
Authority
DE
Germany
Prior art keywords
combustion chamber
gas turbine
turbine
gas
combustion
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
DE8888117859T
Other languages
English (en)
Inventor
Hiroaki Okamoto
Takeshi Takahara
Fukuo Maeda
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.)
Toshiba Corp
Original Assignee
Toshiba 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 Toshiba Corp filed Critical Toshiba Corp
Application granted granted Critical
Publication of DE3866856D1 publication Critical patent/DE3866856D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • 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
    • 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
    • F02C3/20—Gas-turbine plants characterised by the use of combustion products as the working fluid using a special fuel, oxidant, or dilution fluid to generate the combustion products
    • F02C3/30—Adding water, steam or other fluids for influencing combustion, e.g. to obtain cleaner exhaust gases
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C6/00—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion
    • F23C6/04—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection
    • F23C6/045—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure
    • F23C6/047—Combustion apparatus characterised by the combination of two or more combustion chambers or combustion zones, e.g. for staged combustion in series connection with staged combustion in a single enclosure with fuel supply in stages
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23L—SUPPLYING AIR OR NON-COMBUSTIBLE LIQUIDS OR GASES TO COMBUSTION APPARATUS IN GENERAL ; VALVES OR DAMPERS SPECIALLY ADAPTED FOR CONTROLLING AIR SUPPLY OR DRAUGHT IN COMBUSTION APPARATUS; INDUCING DRAUGHT IN COMBUSTION APPARATUS; TOPS FOR CHIMNEYS OR VENTILATING SHAFTS; TERMINALS FOR FLUES
    • F23L7/00—Supplying non-combustible liquids or gases, other than air, to the fire, e.g. oxygen, steam
    • 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
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2260/00—Function
    • F05D2260/20—Heat transfer, e.g. cooling
    • F05D2260/232—Heat transfer, e.g. cooling characterized by the cooling medium
    • F05D2260/2322—Heat transfer, e.g. cooling characterized by the cooling medium steam
    • 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
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E20/00—Combustion technologies with mitigation potential
    • Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE8888117859T 1987-10-27 1988-10-26 Brennkammer fuer eine gasturbine. Expired - Lifetime DE3866856D1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP62270576A JPH01114623A (ja) 1987-10-27 1987-10-27 ガスタービン燃焼器

Publications (1)

Publication Number Publication Date
DE3866856D1 true DE3866856D1 (de) 1992-01-23

Family

ID=17488062

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8888117859T Expired - Lifetime DE3866856D1 (de) 1987-10-27 1988-10-26 Brennkammer fuer eine gasturbine.

Country Status (6)

Country Link
US (1) US4955191A (de)
EP (1) EP0314112B1 (de)
JP (1) JPH01114623A (de)
AU (1) AU608083B2 (de)
CA (1) CA1304234C (de)
DE (1) DE3866856D1 (de)

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DE3737247C1 (de) * 1987-11-03 1989-03-02 Zettner Michael L Brenneinrichtung
US5142858A (en) * 1990-11-21 1992-09-01 General Electric Company Compact flameholder type combustor which is staged to reduce emissions
US6289666B1 (en) * 1992-10-27 2001-09-18 Ginter Vast Corporation High efficiency low pollution hybrid Brayton cycle combustor
USRE43252E1 (en) 1992-10-27 2012-03-20 Vast Power Portfolio, Llc High efficiency low pollution hybrid Brayton cycle combustor
US6047550A (en) * 1996-05-02 2000-04-11 General Electric Co. Premixing dry low NOx emissions combustor with lean direct injection of gas fuel
DE19654472A1 (de) * 1996-12-27 1998-07-02 Asea Brown Boveri Verfahren zur Kühlung von thermisch hochbelasteten Aggregaten einer Gasturbogruppe
US5987875A (en) * 1997-07-14 1999-11-23 Siemens Westinghouse Power Corporation Pilot nozzle steam injection for reduced NOx emissions, and method
EP0924459A1 (de) 1997-12-17 1999-06-23 Asea Brown Boveri AG Verfahren und Vorrichtung zum Eindüsen eines Brennstoff-Flüssigkeitsgemisches in die Brennkammer eines Brenners
DE59808754D1 (de) * 1997-12-19 2003-07-24 Mtu Aero Engines Gmbh Vormischbrennkammer für eine Gasturbine
WO2000012933A1 (de) * 1998-08-26 2000-03-09 Siemens Aktiengesellschaft Hybridbrenner und verfahren zum betrieb eines hybridbrenners
GB9915770D0 (en) 1999-07-07 1999-09-08 Rolls Royce Plc A combustion chamber
US6393823B1 (en) * 1999-11-05 2002-05-28 General Electric Company Methods for fuel nozzle staging for gas turbine engines
US6598383B1 (en) * 1999-12-08 2003-07-29 General Electric Co. Fuel system configuration and method for staging fuel for gas turbines utilizing both gaseous and liquid fuels
US6279313B1 (en) 1999-12-14 2001-08-28 General Electric Company Combustion liner for gas turbine having liner stops
CA2397656A1 (en) * 2000-01-17 2001-07-26 Unitec Co. Ltd. Integrated support, integrated minute vessels and permeable membrane, and method of making and using the same
JP2002156115A (ja) 2000-11-17 2002-05-31 Mitsubishi Heavy Ind Ltd 燃焼器
DE50112904D1 (de) * 2000-12-16 2007-10-04 Alstom Technology Ltd Verfahren zum Betrieb eines Vormischbrenners
US6715295B2 (en) * 2002-05-22 2004-04-06 Siemens Westinghouse Power Corporation Gas turbine pilot burner water injection and method of operation
AU2003238326A1 (en) * 2002-07-19 2004-02-09 Alstom Technology Ltd Method for controlling the introduction of inert media into a combustion chamber
US7143583B2 (en) * 2002-08-22 2006-12-05 Hitachi, Ltd. Gas turbine combustor, combustion method of the gas turbine combustor, and method of remodeling a gas turbine combustor
US6755359B2 (en) 2002-09-12 2004-06-29 The Boeing Company Fluid mixing injector and method
US6802178B2 (en) * 2002-09-12 2004-10-12 The Boeing Company Fluid injection and injection method
US6775987B2 (en) 2002-09-12 2004-08-17 The Boeing Company Low-emission, staged-combustion power generation
US6868676B1 (en) 2002-12-20 2005-03-22 General Electric Company Turbine containing system and an injector therefor
EP1510656A1 (de) * 2003-09-01 2005-03-02 Siemens Aktiengesellschaft Verfahren und Vorrichtung zum Erkennen eines Betriebszustandes einer Turbine
EP1819964A2 (de) 2004-06-11 2007-08-22 Vast Power Systems, Inc. Vorrichtung und verfahren zur emissionsarmen verbrennung
US20070089427A1 (en) * 2005-10-24 2007-04-26 Thomas Scarinci Two-branch mixing passage and method to control combustor pulsations
US8671658B2 (en) * 2007-10-23 2014-03-18 Ener-Core Power, Inc. Oxidizing fuel
JP4959524B2 (ja) 2007-11-29 2012-06-27 三菱重工業株式会社 燃焼バーナー
EP2107311A1 (de) * 2008-04-01 2009-10-07 Siemens Aktiengesellschaft Größenskalierung eines Brenners
US8511059B2 (en) * 2008-09-30 2013-08-20 Alstom Technology Ltd. Methods of reducing emissions for a sequential combustion gas turbine and combustor for a gas turbine
US20100089022A1 (en) * 2008-10-14 2010-04-15 General Electric Company Method and apparatus of fuel nozzle diluent introduction
US9121609B2 (en) * 2008-10-14 2015-09-01 General Electric Company Method and apparatus for introducing diluent flow into a combustor
US9410409B1 (en) * 2009-08-11 2016-08-09 EOR Technology LLC Thermal vapor stream apparatus and method
JP5558168B2 (ja) * 2010-03-30 2014-07-23 三菱重工業株式会社 燃焼器及びガスタービン
EP2423591B1 (de) * 2010-08-24 2018-10-31 Ansaldo Energia IP UK Limited Verfahren zum Betrieb einer Brennkammer
US8991187B2 (en) 2010-10-11 2015-03-31 General Electric Company Combustor with a lean pre-nozzle fuel injection system
CH704829A2 (de) * 2011-04-08 2012-11-15 Alstom Technology Ltd Gasturbogruppe und zugehöriges Betriebsverfahren.
US8601820B2 (en) 2011-06-06 2013-12-10 General Electric Company Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
US8407892B2 (en) 2011-08-05 2013-04-02 General Electric Company Methods relating to integrating late lean injection into combustion turbine engines
US9010120B2 (en) 2011-08-05 2015-04-21 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US9140455B2 (en) 2012-01-04 2015-09-22 General Electric Company Flowsleeve of a turbomachine component
CH705965A1 (de) * 2012-01-09 2013-07-15 Alstom Technology Ltd Verfahren zum Betrieb einer Gasturbine.
US9097424B2 (en) * 2012-03-12 2015-08-04 General Electric Company System for supplying a fuel and working fluid mixture to a combustor
US9310078B2 (en) 2012-10-31 2016-04-12 General Electric Company Fuel injection assemblies in combustion turbine engines
JP6010489B2 (ja) * 2013-03-12 2016-10-19 三菱日立パワーシステムズ株式会社 熱電可変型コジェネレーションシステム
US11143407B2 (en) 2013-06-11 2021-10-12 Raytheon Technologies Corporation Combustor with axial staging for a gas turbine engine
US9903588B2 (en) * 2013-07-30 2018-02-27 General Electric Company System and method for barrier in passage of combustor of gas turbine engine with exhaust gas recirculation
US20150159877A1 (en) * 2013-12-06 2015-06-11 General Electric Company Late lean injection manifold mixing system
US9803555B2 (en) * 2014-04-23 2017-10-31 General Electric Company Fuel delivery system with moveably attached fuel tube
US20160053681A1 (en) * 2014-08-20 2016-02-25 General Electric Company Liquid fuel combustor having an oxygen-depleted gas (odg) injection system for a gas turbomachine
KR102046457B1 (ko) * 2017-11-09 2019-11-19 두산중공업 주식회사 연소기 및 이를 포함하는 가스 터빈
US10739007B2 (en) * 2018-05-09 2020-08-11 Power Systems Mfg., Llc Flamesheet diffusion cartridge
CN109489071B (zh) * 2018-11-28 2023-09-12 中国华能集团有限公司 一种低NOx排放的燃烧室、燃气轮机系统、燃气轮机系统的启动方法及负荷调节方法
JP7303011B2 (ja) * 2019-04-05 2023-07-04 三菱重工業株式会社 燃焼器及びガスタービン
EP4206539A1 (de) * 2021-12-30 2023-07-05 Ansaldo Energia Switzerland AG Brennkammeranordnung für eine gasturbinenanordnung, gasturbinenanordnung und verfahren zum betreiben einer brennkammeranordnung für eine gasturbinenanordnung
US11920792B1 (en) 2023-03-13 2024-03-05 Rtx Corporation Cooling turbine engine fuel-air mixer with steam

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US3693347A (en) * 1971-05-12 1972-09-26 Gen Electric Steam injection in gas turbines having fixed geometry components
US3785146A (en) * 1972-05-01 1974-01-15 Gen Electric Self compensating flow divider for a gas turbine steam injection system
US3826080A (en) * 1973-03-15 1974-07-30 Westinghouse Electric Corp System for reducing nitrogen-oxygen compound in the exhaust of a gas turbine
GB1489339A (en) * 1973-11-30 1977-10-19 Rolls Royce Gas turbine engine combustion chambers
JPS5239007A (en) * 1975-09-22 1977-03-26 Hitachi Ltd Combustor used for a gas turbine
US4112676A (en) * 1977-04-05 1978-09-12 Westinghouse Electric Corp. Hybrid combustor with staged injection of pre-mixed fuel
US4259837A (en) * 1979-06-13 1981-04-07 General Electric Company Water and steam injection system for emission control of gas turbines
JPS6057131A (ja) * 1983-09-08 1985-04-02 Hitachi Ltd ガスタ−ビン燃焼器の燃料供給方法
JPH0621572B2 (ja) * 1984-12-14 1994-03-23 株式会社日立製作所 ガスタービンプラントの起動方法及びガスタービンプラント
DE3606625A1 (de) * 1985-03-04 1986-09-04 Kraftwerk Union AG, 4330 Mülheim Pilotbrenner mit geringer no(pfeil abwaerts)x(pfeil abwaerts)-emission fuer feuerungsanlagen, insbesondere von gasturbinenanlagen, und verfahren zu seinem betrieb
DE3663189D1 (en) * 1985-03-04 1989-06-08 Siemens Ag Burner disposition for combustion installations, especially for combustion chambers of gas turbine installations, and method for its operation
US4735052A (en) * 1985-09-30 1988-04-05 Kabushiki Kaisha Toshiba Gas turbine apparatus
JPH0663646B2 (ja) * 1985-10-11 1994-08-22 株式会社日立製作所 ガスタ−ビン用燃焼器
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JPH049527A (ja) * 1990-04-25 1992-01-14 Toshiba Corp 電子レンジ用扉

Also Published As

Publication number Publication date
CA1304234C (en) 1992-06-30
EP0314112A1 (de) 1989-05-03
US4955191A (en) 1990-09-11
JPH01114623A (ja) 1989-05-08
AU2435588A (en) 1989-05-25
AU608083B2 (en) 1991-03-21
EP0314112B1 (de) 1991-12-11

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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

Free format text: BLUMBACH, KRAMER & PARTNER, 81245 MUENCHEN

8328 Change in the person/name/address of the agent

Representative=s name: KRAMER - BARSKE - SCHMIDTCHEN, 81245 MUENCHEN

8339 Ceased/non-payment of the annual fee