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DE69724502D1 - Gasturbinenbrennkammer - Google Patents

Gasturbinenbrennkammer

Info

Publication number
DE69724502D1
DE69724502D1 DE69724502T DE69724502T DE69724502D1 DE 69724502 D1 DE69724502 D1 DE 69724502D1 DE 69724502 T DE69724502 T DE 69724502T DE 69724502 T DE69724502 T DE 69724502T DE 69724502 D1 DE69724502 D1 DE 69724502D1
Authority
DE
Germany
Prior art keywords
gas turbine
turbine combustor
combustor
gas
turbine
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
DE69724502T
Other languages
English (en)
Other versions
DE69724502T2 (de
Inventor
Hisham Salman Alkabie
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
Alstom Power UK Holdings Ltd
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 Alstom Power UK Holdings Ltd filed Critical Alstom Power UK Holdings Ltd
Application granted granted Critical
Publication of DE69724502D1 publication Critical patent/DE69724502D1/de
Publication of DE69724502T2 publication Critical patent/DE69724502T2/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
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/02—Disposition of air supply not passing through burner
    • F23C7/06—Disposition of air supply not passing through burner for heating the incoming air
    • 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
    • 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
    • F23R3/36—Supply of different fuels

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Thermal Sciences (AREA)
  • Gas Burners (AREA)
DE69724502T 1996-03-29 1997-02-20 Gasturbinenbrennkammer Expired - Lifetime DE69724502T2 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB9606628A GB2311596B (en) 1996-03-29 1996-03-29 Combustor for gas - or liquid - fuelled turbine
GB9606628 1996-03-29

Publications (2)

Publication Number Publication Date
DE69724502D1 true DE69724502D1 (de) 2003-10-09
DE69724502T2 DE69724502T2 (de) 2004-06-24

Family

ID=10791258

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69724502T Expired - Lifetime DE69724502T2 (de) 1996-03-29 1997-02-20 Gasturbinenbrennkammer

Country Status (4)

Country Link
US (1) US6209325B1 (de)
EP (1) EP0803682B1 (de)
DE (1) DE69724502T2 (de)
GB (1) GB2311596B (de)

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US9581081B2 (en) 2013-01-13 2017-02-28 General Electric Company System and method for protecting components in a gas turbine engine with exhaust gas recirculation
JP6038674B2 (ja) * 2013-02-04 2016-12-07 株式会社東芝 ガスタービン燃焼器およびガスタービン
US9512759B2 (en) 2013-02-06 2016-12-06 General Electric Company System and method for catalyst heat utilization for gas turbine with exhaust gas recirculation
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TW201502356A (zh) 2013-02-21 2015-01-16 Exxonmobil Upstream Res Co 氣渦輪機排氣中氧之減少
US10221762B2 (en) * 2013-02-28 2019-03-05 General Electric Company System and method for a turbine combustor
CN105008499A (zh) 2013-03-08 2015-10-28 埃克森美孚上游研究公司 发电和从甲烷水合物中回收甲烷
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US9958161B2 (en) * 2013-03-12 2018-05-01 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9228747B2 (en) 2013-03-12 2016-01-05 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9541292B2 (en) 2013-03-12 2017-01-10 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
US9127843B2 (en) 2013-03-12 2015-09-08 Pratt & Whitney Canada Corp. Combustor for gas turbine engine
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US20140366541A1 (en) * 2013-06-14 2014-12-18 General Electric Company Systems and apparatus relating to fuel injection in gas turbines
US9835089B2 (en) 2013-06-28 2017-12-05 General Electric Company System and method for a fuel nozzle
US9617914B2 (en) 2013-06-28 2017-04-11 General Electric Company Systems and methods for monitoring gas turbine systems having exhaust gas recirculation
US9631542B2 (en) 2013-06-28 2017-04-25 General Electric Company System and method for exhausting combustion gases from gas turbine engines
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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
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Also Published As

Publication number Publication date
DE69724502T2 (de) 2004-06-24
EP0803682A2 (de) 1997-10-29
US6209325B1 (en) 2001-04-03
EP0803682A3 (de) 1999-11-03
GB9606628D0 (en) 1996-06-05
GB2311596A (en) 1997-10-01
GB2311596B (en) 2000-07-12
EP0803682B1 (de) 2003-09-03

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8364 No opposition during term of opposition
8327 Change in the person/name/address of the patent owner

Owner name: SIEMENS AG, 80333 MUENCHEN, DE