DE59907940D1 - COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER - Google Patents

COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER

Info

Publication number
DE59907940D1
DE59907940D1 DE59907940T DE59907940T DE59907940D1 DE 59907940 D1 DE59907940 D1 DE 59907940D1 DE 59907940 T DE59907940 T DE 59907940T DE 59907940 T DE59907940 T DE 59907940T DE 59907940 D1 DE59907940 D1 DE 59907940D1
Authority
DE
Germany
Prior art keywords
combustion chamber
operating
combustion
chamber
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
DE59907940T
Other languages
German (de)
Inventor
Gerwig Poeschl
Heinrich Puetz
Stefan Hoffmann
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 DE59907940D1 publication Critical patent/DE59907940D1/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
    • F23D14/12—Radiant burners
    • F23D14/16—Radiant burners using permeable blocks
    • 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
    • F23R3/002—Wall structures
    • 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
    • F23R3/007—Continuous combustion chambers using liquid or gaseous fuel constructed mainly of ceramic components
    • 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
    • F23R3/346—Feeding into different combustion zones for staged combustion

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Ceramic Engineering (AREA)
DE59907940T 1998-03-10 1999-02-25 COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER Expired - Lifetime DE59907940D1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19810276 1998-03-10
PCT/DE1999/000513 WO1999046540A1 (en) 1998-03-10 1999-02-25 Combustion chamber and method for operating a combustion chamber

Publications (1)

Publication Number Publication Date
DE59907940D1 true DE59907940D1 (en) 2004-01-15

Family

ID=7860355

Family Applications (1)

Application Number Title Priority Date Filing Date
DE59907940T Expired - Lifetime DE59907940D1 (en) 1998-03-10 1999-02-25 COMBUSTION CHAMBER AND METHOD FOR OPERATING A COMBUSTION CHAMBER

Country Status (4)

Country Link
EP (1) EP1062461B1 (en)
JP (1) JP4365027B2 (en)
DE (1) DE59907940D1 (en)
WO (1) WO1999046540A1 (en)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP4524902B2 (en) * 2000-10-25 2010-08-18 株式会社Ｉｈｉ Low NOx combustor with premixed fuel injection valve
EP1286112A1 (en) 2001-08-09 2003-02-26 Siemens Aktiengesellschaft Premix burner and method of operating the same
EP1460339A1 (en) * 2003-03-21 2004-09-22 Siemens Aktiengesellschaft Gas turbine
EP1557607B1 (en) * 2004-01-21 2010-09-29 Siemens Aktiengesellschaft Burner with cooled component, gas turbine and method for cooling the component
EP1847684A1 (en) 2006-04-21 2007-10-24 Siemens Aktiengesellschaft Turbine blade
EP1847696A1 (en) 2006-04-21 2007-10-24 Siemens Aktiengesellschaft Component for a secondary combustion system in a gas turbine and corresponding gas turbine.
US8800293B2 (en) 2007-07-10 2014-08-12 United Technologies Corporation Floatwell panel assemblies and related systems
EP2161500A1 (en) 2008-09-04 2010-03-10 Siemens Aktiengesellschaft Combustor system and method of reducing combustion instability and/or emissions of a combustor system
DE102017207487A1 (en) 2017-05-04 2018-11-08 Siemens Aktiengesellschaft combustion chamber
WO2019172925A2 (en) * 2018-03-09 2019-09-12 Siemens Aktiengesellschaft Finely distributed combustion system for a gas turbine engine
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

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE253189C (en) *
BE790956A (en) * 1971-11-05 1973-03-01 Penny Robert N FLAME TUBE FOR AGAZ TURBINE ENGINE COMBUSTION CHAMBER
US3981675A (en) * 1974-12-19 1976-09-21 United Technologies Corporation Ceramic burner construction
US4112676A (en) * 1977-04-05 1978-09-12 Westinghouse Electric Corp. Hybrid combustor with staged injection of pre-mixed fuel
US4910957A (en) * 1988-07-13 1990-03-27 Prutech Ii Staged lean premix low nox hot wall gas turbine combustor with improved turndown capability
FR2647534B1 (en) * 1989-05-29 1991-09-13 Europ Propulsion REACTOR CHAMBER AND METHOD FOR THE PRODUCTION THEREOF
EP0576697B1 (en) 1992-06-29 1997-08-27 Abb Research Ltd. Combustor chamber for a gas turbine
DE59208713D1 (en) 1992-11-09 1997-08-21 Asea Brown Boveri Gas turbine combustor
JP3404981B2 (en) * 1995-04-21 2003-05-12 日本鋼管株式会社 Gas heating device

Also Published As

Publication number Publication date
EP1062461A1 (en) 2000-12-27
JP4365027B2 (en) 2009-11-18
EP1062461B1 (en) 2003-12-03
WO1999046540A1 (en) 1999-09-16
JP2002506193A (en) 2002-02-26

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition