CN101395428B - 燃气轮机燃烧器及其运行方法 - Google Patents

燃气轮机燃烧器及其运行方法 Download PDF

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Publication number
CN101395428B
CN101395428B CN2007800071274A CN200780007127A CN101395428B CN 101395428 B CN101395428 B CN 101395428B CN 2007800071274 A CN2007800071274 A CN 2007800071274A CN 200780007127 A CN200780007127 A CN 200780007127A CN 101395428 B CN101395428 B CN 101395428B
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CN
China
Prior art keywords
fuel
gas
combustion
gas turbine
turbine burner
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
CN2007800071274A
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English (en)
Chinese (zh)
Other versions
CN101395428A (zh
Inventor
安德烈亚斯·海洛斯
沃纳·克雷布斯
杰亚普·范坎彭
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Siemens Corp
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Siemens Corp
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Publication date
Application filed by Siemens Corp filed Critical Siemens Corp
Publication of CN101395428A publication Critical patent/CN101395428A/zh
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Publication of CN101395428B publication Critical patent/CN101395428B/zh
Expired - Fee Related legal-status Critical Current
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    • 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
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K3/00—Plants including a gas turbine driving a compressor or a ducted fan
    • F02K3/08—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof
    • F02K3/10—Plants including a gas turbine driving a compressor or a ducted fan with supplementary heating of the working fluid; Control thereof by after-burners
    • 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
    • F23R3/16—Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration with devices inside the flame tube or the combustion chamber to influence the air or gas flow
    • F23R3/18—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants
    • F23R3/24—Flame stabilising means, e.g. flame holders for after-burners of jet-propulsion plants of the fluid-screen type

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gas Burners (AREA)
CN2007800071274A 2006-02-28 2007-02-20 燃气轮机燃烧器及其运行方法 Expired - Fee Related CN101395428B (zh)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
DE102006009562.6 2006-02-28
DE102006009562 2006-02-28
PCT/EP2007/051597 WO2007099046A1 (de) 2006-02-28 2007-02-20 Gasturbinenbrenner und verfahren zum betreiben eines gasturbinenbrenners

Publications (2)

Publication Number Publication Date
CN101395428A CN101395428A (zh) 2009-03-25
CN101395428B true CN101395428B (zh) 2010-12-08

Family

ID=38009771

Family Applications (1)

Application Number Title Priority Date Filing Date
CN2007800071274A Expired - Fee Related CN101395428B (zh) 2006-02-28 2007-02-20 燃气轮机燃烧器及其运行方法

Country Status (6)

Country Link
US (1) US20100043440A1 (enExample)
EP (1) EP1989486A1 (enExample)
JP (1) JP4776697B2 (enExample)
CN (1) CN101395428B (enExample)
RU (1) RU2406034C2 (enExample)
WO (1) WO2007099046A1 (enExample)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9528439B2 (en) * 2013-03-15 2016-12-27 General Electric Company Systems and apparatus relating to downstream fuel and air injection in gas turbines
US10222066B2 (en) * 2016-05-26 2019-03-05 Siemens Energy, Inc. Ducting arrangement with injector assemblies arranged in an expanding cross-sectional area of a downstream combustion stage in a gas turbine engine
US11156156B2 (en) 2018-10-04 2021-10-26 Raytheon Technologies Corporation Gas turbine engine with a unitary structure and method for manufacturing the same
DE102019204746A1 (de) 2019-04-03 2020-10-08 Siemens Aktiengesellschaft Hitzeschildkachel mit Dämpfungsfunktion
US11174792B2 (en) 2019-05-21 2021-11-16 General Electric Company System and method for high frequency acoustic dampers with baffles
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
US12454912B2 (en) 2020-12-03 2025-10-28 Rtx Corporation Supplemental thrust system for a gas turbine engine

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1926728B1 (de) * 1969-05-24 1971-03-25 Messerschmitt Boelkow Blohm Brennkammer fuer Strahltriebwerke,insbesondere fuer Raketen-Staustrahltriebwerke
GB1586752A (en) * 1977-05-23 1981-03-25 Inst Francais Du Petrole Gas turbine engines and methods of operating gas turbine engines
US4896501A (en) * 1987-10-22 1990-01-30 Faulkner Robie L Turbojet engine with sonic injection afterburner
CN1046958A (zh) * 1989-04-26 1990-11-14 通用电气公司 减小加力燃气涡轮发动机压差载荷的装置和方法
US6112512A (en) * 1997-08-05 2000-09-05 Lockheed Martin Corporation Method and apparatus of pulsed injection for improved nozzle flow control

Family Cites Families (20)

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Publication number Priority date Publication date Assignee Title
FR1217843A (fr) * 1958-12-10 1960-05-05 Snecma Brûleur de combustion ou de post-combustion pour combustible chaud
DE1235670B (de) * 1962-11-06 1967-03-02 Deutsche Forsch Luft Raumfahrt Vorrichtung zur Flammenstabilisierung in Gleichdruck-Brennkammern
DE1800611A1 (de) * 1968-10-02 1970-05-27 Hertel Dr Ing Heinrich Anordnung zum Einspritzen von Kraftstoff in einen an einer Einspritzduese mit UEberschallgeschwindigkeit vorbeistroemenden Luftstrom
GB1283827A (en) * 1970-09-26 1972-08-02 Rolls Royce Improvements in or relating to combustion apparatus
US4255777A (en) * 1977-11-21 1981-03-10 Exxon Research & Engineering Co. Electrostatic atomizing device
US4581675A (en) * 1980-09-02 1986-04-08 Exxon Research And Engineering Co. Electrostatic atomizing device
US4683541A (en) * 1985-03-13 1987-07-28 David Constant V Rotary fluidized bed combustion system
US4821512A (en) * 1987-05-05 1989-04-18 United Technologies Corporation Piloting igniter for supersonic combustor
US4793305A (en) * 1987-07-16 1988-12-27 Dresser Industries, Inc. High turbulence combustion chamber for turbocharged lean burn gaseous fueled engine
US4991774A (en) * 1989-08-24 1991-02-12 Charged Injection Corporation Electrostatic injector using vapor and mist insulation
US5093602A (en) * 1989-11-17 1992-03-03 Charged Injection Corporation Methods and apparatus for dispersing a fluent material utilizing an electron beam
RU2035008C1 (ru) * 1992-05-28 1995-05-10 Михаил Яковлевич Бобрик Способ сжигания углеводородного топлива
US5341640A (en) * 1993-03-30 1994-08-30 Faulkner Robie L Turbojet engine with afterburner and thrust augmentation ejectors
US5515681A (en) * 1993-05-26 1996-05-14 Simmonds Precision Engine Systems Commonly housed electrostatic fuel atomizer and igniter apparatus for combustors
CH688899A5 (de) * 1994-05-26 1998-05-15 Asea Brown Boveri Verfahren zur Regelung einer Gasturbogruppe.
JPH08193716A (ja) * 1995-01-17 1996-07-30 Hitachi Ltd ガスタービン燃焼器
RU2116567C1 (ru) * 1996-03-11 1998-07-27 Акционерное общество открытого типа "Северсталь" Многоствольное эжекторное горелочное устройство
GB2390150A (en) * 2002-06-26 2003-12-31 Alstom Reheat combustion system for a gas turbine including an accoustic screen
US6883302B2 (en) * 2002-12-20 2005-04-26 General Electric Company Methods and apparatus for generating gas turbine engine thrust with a pulse detonation thrust augmenter
FR2858661B1 (fr) * 2003-08-05 2005-10-07 Snecma Moteurs Dispositif de post-combustion

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1926728B1 (de) * 1969-05-24 1971-03-25 Messerschmitt Boelkow Blohm Brennkammer fuer Strahltriebwerke,insbesondere fuer Raketen-Staustrahltriebwerke
GB1586752A (en) * 1977-05-23 1981-03-25 Inst Francais Du Petrole Gas turbine engines and methods of operating gas turbine engines
US4896501A (en) * 1987-10-22 1990-01-30 Faulkner Robie L Turbojet engine with sonic injection afterburner
CN1046958A (zh) * 1989-04-26 1990-11-14 通用电气公司 减小加力燃气涡轮发动机压差载荷的装置和方法
US6112512A (en) * 1997-08-05 2000-09-05 Lockheed Martin Corporation Method and apparatus of pulsed injection for improved nozzle flow control

Also Published As

Publication number Publication date
RU2406034C2 (ru) 2010-12-10
RU2008138545A (ru) 2010-04-10
EP1989486A1 (de) 2008-11-12
CN101395428A (zh) 2009-03-25
US20100043440A1 (en) 2010-02-25
JP2009528503A (ja) 2009-08-06
WO2007099046A1 (de) 2007-09-07
JP4776697B2 (ja) 2011-09-21

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SE01 Entry into force of request for substantive examination
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Granted publication date: 20101208

Termination date: 20200220