DE59801583D1 - BURNER ARRANGEMENT FOR A COMBUSTION PLANT, IN PARTICULAR A GAS TURBINE COMBUSTION CHAMBER - Google Patents

BURNER ARRANGEMENT FOR A COMBUSTION PLANT, IN PARTICULAR A GAS TURBINE COMBUSTION CHAMBER

Info

Publication number
DE59801583D1
DE59801583D1 DE59801583T DE59801583T DE59801583D1 DE 59801583 D1 DE59801583 D1 DE 59801583D1 DE 59801583 T DE59801583 T DE 59801583T DE 59801583 T DE59801583 T DE 59801583T DE 59801583 D1 DE59801583 D1 DE 59801583D1
Authority
DE
Germany
Prior art keywords
gas turbine
burner arrangement
combustion chamber
plant
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
DE59801583T
Other languages
German (de)
Inventor
Bernd Prade
Holger Streb
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.)
Siemens AG
Original Assignee
Siemens AG
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 Siemens AG filed Critical Siemens AG
Application granted granted Critical
Publication of DE59801583D1 publication Critical patent/DE59801583D1/en
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
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/26—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid with provision for a retention flame
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/82—Preventing flashback or blowback
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
    • F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D23/00—Assemblies of two or more 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
    • F23R3/04—Air inlet arrangements
    • F23R3/10—Air inlet arrangements for primary air
    • F23R3/12—Air inlet arrangements for primary air inducing a vortex
    • F23R3/14—Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • 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
    • 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
    • F23R3/343—Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2206/00—Burners for specific applications
    • F23D2206/10—Turbines
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03343—Pilot burners operating in premixed mode

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE59801583T 1997-07-17 1998-07-07 BURNER ARRANGEMENT FOR A COMBUSTION PLANT, IN PARTICULAR A GAS TURBINE COMBUSTION CHAMBER Expired - Lifetime DE59801583D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19730734 1997-07-17
PCT/DE1998/001871 WO1999004196A1 (en) 1997-07-17 1998-07-07 Arrangement of burners for heating installation, in particular a gas turbine combustion chamber

Publications (1)

Publication Number Publication Date
DE59801583D1 true DE59801583D1 (en) 2001-10-31

Family

ID=7836051

Family Applications (1)

Application Number Title Priority Date Filing Date
DE59801583T Expired - Lifetime DE59801583D1 (en) 1997-07-17 1998-07-07 BURNER ARRANGEMENT FOR A COMBUSTION PLANT, IN PARTICULAR A GAS TURBINE COMBUSTION CHAMBER

Country Status (4)

Country Link
EP (1) EP0995066B1 (en)
JP (1) JP2001510885A (en)
DE (1) DE59801583D1 (en)
WO (1) WO1999004196A1 (en)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2000049337A1 (en) * 1999-02-16 2000-08-24 Siemens Aktiengesellschaft Burner arrangement and method for operating a burner arrangement
US6354072B1 (en) * 1999-12-10 2002-03-12 General Electric Company Methods and apparatus for decreasing combustor emissions
EP1239219A4 (en) 1999-12-15 2003-03-12 Osaka Gas Co Ltd Fluid distributor, burner device, gas turbine engine, and cogeneration system
US6327860B1 (en) * 2000-06-21 2001-12-11 Honeywell International, Inc. Fuel injector for low emissions premixing gas turbine combustor
US6363726B1 (en) * 2000-09-29 2002-04-02 General Electric Company Mixer having multiple swirlers
US6367262B1 (en) * 2000-09-29 2002-04-09 General Electric Company Multiple annular swirler
DE10104695B4 (en) 2001-02-02 2014-11-20 Alstom Technology Ltd. Premix burner for a gas turbine
US6484489B1 (en) * 2001-05-31 2002-11-26 General Electric Company Method and apparatus for mixing fuel to decrease combustor emissions
US6848260B2 (en) 2002-09-23 2005-02-01 Siemens Westinghouse Power Corporation Premixed pilot burner for a combustion turbine engine
EP1460339A1 (en) * 2003-03-21 2004-09-22 Siemens Aktiengesellschaft Gas turbine
US7303388B2 (en) 2004-07-01 2007-12-04 Air Products And Chemicals, Inc. Staged combustion system with ignition-assisted fuel lances
EP1624252A1 (en) * 2004-08-06 2006-02-08 Siemens Aktiengesellschaft Burner, Gas Turbine and Method for Operating a Burner
ITTO20050208A1 (en) * 2005-03-30 2006-09-30 Ansaldo Energia Spa GAS BURNER GROUP FOR A GAS TURBINE
EP1764553A1 (en) * 2005-09-14 2007-03-21 Enel Produzione S.p.A. High-stability premix burner for gas turbines
EP2023041A1 (en) * 2007-07-27 2009-02-11 Siemens Aktiengesellschaft Premix burner and method for operating a premix burner
JP5193088B2 (en) * 2009-02-20 2013-05-08 三菱重工業株式会社 Combustor and gas turbine
US20100307160A1 (en) * 2009-06-03 2010-12-09 Vinayak Barve Convex Pilot Cone
US8474266B2 (en) 2009-07-24 2013-07-02 General Electric Company System and method for a gas turbine combustor having a bleed duct from a diffuser to a fuel nozzle
EP2397764A1 (en) * 2010-06-18 2011-12-21 Siemens Aktiengesellschaft Turbine burner
GB201511841D0 (en) 2015-07-07 2015-08-19 Rolls Royce Plc Fuel spray nozel for a gas turbine engine

Family Cites Families (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE3241162A1 (en) 1982-11-08 1984-05-10 Kraftwerk Union AG, 4330 Mülheim PRE-MIXING BURNER WITH INTEGRATED DIFFUSION BURNER
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
JP3335713B2 (en) * 1993-06-28 2002-10-21 株式会社東芝 Gas turbine combustor
GB9326367D0 (en) * 1993-12-23 1994-02-23 Rolls Royce Plc Fuel injection apparatus
US5467926A (en) * 1994-02-10 1995-11-21 Solar Turbines Incorporated Injector having low tip temperature
US5408830A (en) * 1994-02-10 1995-04-25 General Electric Company Multi-stage fuel nozzle for reducing combustion instabilities in low NOX gas turbines
JP2950720B2 (en) * 1994-02-24 1999-09-20 株式会社東芝 Gas turbine combustion device and combustion control method therefor
JP3449802B2 (en) * 1994-10-31 2003-09-22 東京瓦斯株式会社 Gas combustion equipment
FR2727192B1 (en) * 1994-11-23 1996-12-20 Snecma INJECTION SYSTEM FOR A TWO-HEAD COMBUSTION CHAMBER
ES2169273T3 (en) * 1995-09-22 2002-07-01 Siemens Ag BURNER, ESPECIALLY FOR A GAS TURBINE.
GB9607010D0 (en) * 1996-04-03 1996-06-05 Rolls Royce Plc Gas turbine engine combustion equipment

Also Published As

Publication number Publication date
WO1999004196A1 (en) 1999-01-28
EP0995066B1 (en) 2001-09-26
JP2001510885A (en) 2001-08-07
EP0995066A1 (en) 2000-04-26

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition