WO2005093326A3 - Gas turbine combustion chamber and corresponding operating method - Google Patents

Gas turbine combustion chamber and corresponding operating method Download PDF

Info

Publication number
WO2005093326A3
WO2005093326A3 PCT/EP2005/051192 EP2005051192W WO2005093326A3 WO 2005093326 A3 WO2005093326 A3 WO 2005093326A3 EP 2005051192 W EP2005051192 W EP 2005051192W WO 2005093326 A3 WO2005093326 A3 WO 2005093326A3
Authority
WO
WIPO (PCT)
Prior art keywords
combustion chamber
burner
gas turbine
operating method
corresponding operating
Prior art date
Application number
PCT/EP2005/051192
Other languages
German (de)
French (fr)
Other versions
WO2005093326A2 (en
Inventor
Peter Flohr
Alexander Ni
Rajeshriben Patel
Majed Toqan
Original Assignee
Alstom Technology Ltd
Peter Flohr
Alexander Ni
Rajeshriben Patel
Majed Toqan
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 Technology Ltd, Peter Flohr, Alexander Ni, Rajeshriben Patel, Majed Toqan filed Critical Alstom Technology Ltd
Publication of WO2005093326A2 publication Critical patent/WO2005093326A2/en
Publication of WO2005093326A3 publication Critical patent/WO2005093326A3/en

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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23M—CASINGS, LININGS, WALLS OR DOORS SPECIALLY ADAPTED FOR COMBUSTION CHAMBERS, e.g. FIREBRIDGES; DEVICES FOR DEFLECTING AIR, FLAMES OR COMBUSTION PRODUCTS IN COMBUSTION CHAMBERS; SAFETY ARRANGEMENTS SPECIALLY ADAPTED FOR COMBUSTION APPARATUS; DETAILS OF COMBUSTION CHAMBERS, NOT OTHERWISE PROVIDED FOR
    • F23M20/00—Details of combustion chambers, not otherwise provided for, e.g. means for storing heat from flames
    • F23M20/005—Noise absorbing means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N5/00—Systems for controlling 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
    • F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
    • F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2225/00—Measuring
    • F23N2225/08—Measuring temperature
    • F23N2225/16—Measuring temperature burner temperature
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23N—REGULATING OR CONTROLLING COMBUSTION
    • F23N2237/00—Controlling
    • F23N2237/02—Controlling 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00014—Reducing thermo-acoustic vibrations by passive means, e.g. by Helmholtz resonators

Abstract

The invention relates to a combustion chamber (1) for a gas turbine, comprising an annular combustion chamber (2) and at least one annular burner arrangement (4). The burner arrangement has several burners (5), which are arranged in a distributed manner in peripheral direction at the entrance (3) of the combustion chamber (2). In order to reduce pressure pulsations in the combustion chamber (2), the combustion chamber (1) comprises an actuation system (6) that is configured to individually actuate each burner (5) of the burner arrangement (4), in addition to a control system (8) that individually monitors each burner (5) of the burner arrangement (4) by means of an appropriate sensor system (9) and controls each individual burner by means of the actuation system (6) with the aim of reducing pressure pulsations.
PCT/EP2005/051192 2004-03-29 2005-03-16 Gas turbine combustion chamber and corresponding operating method WO2005093326A2 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102004015186.5 2004-03-29
DE102004015186A DE102004015186A1 (en) 2004-03-29 2004-03-29 Gas turbine combustor and associated operating method

Publications (2)

Publication Number Publication Date
WO2005093326A2 WO2005093326A2 (en) 2005-10-06
WO2005093326A3 true WO2005093326A3 (en) 2006-02-09

Family

ID=34962253

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/EP2005/051192 WO2005093326A2 (en) 2004-03-29 2005-03-16 Gas turbine combustion chamber and corresponding operating method

Country Status (2)

Country Link
DE (1) DE102004015186A1 (en)
WO (1) WO2005093326A2 (en)

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102004036911A1 (en) * 2004-07-29 2006-03-23 Alstom Technology Ltd Operating procedure for a combustion plant
DE102006015230A1 (en) * 2006-03-30 2007-10-18 Alstom Technology Ltd. combustion chamber
US8631656B2 (en) * 2008-03-31 2014-01-21 General Electric Company Gas turbine engine combustor circumferential acoustic reduction using flame temperature nonuniformities
DE102017201771A1 (en) 2017-02-03 2018-08-09 Siemens Aktiengesellschaft Circumferential grading concept for a burner assembly
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
EP4148327A1 (en) * 2021-09-09 2023-03-15 Ansaldo Energia Switzerland AG Gas turbine engine with acoustic mode stabilization, method for controlling and method for retrofitting a gas turbine engine

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4414232A1 (en) * 1994-04-23 1995-10-26 Abb Management Ag Device for damping thermoacoustic vibrations in a combustion chamber
US5533329A (en) * 1993-05-17 1996-07-09 Hitachi, Ltd. Control apparatus for and control method of gas turbine
US5544478A (en) * 1994-11-15 1996-08-13 General Electric Company Optical sensing of combustion dynamics
EP0962704A2 (en) * 1998-05-29 1999-12-08 United Technologies Corporation Method and apparatus for use with a gas fueled combustor
US6205764B1 (en) * 1997-02-06 2001-03-27 Jakob Hermann Method for the active damping of combustion oscillation and combustion apparatus
EP1096201A1 (en) * 1999-10-29 2001-05-02 Siemens Aktiengesellschaft Burner
EP1180646A1 (en) * 2000-08-10 2002-02-20 ROLLS-ROYCE plc A combustion chamber
US6464489B1 (en) * 1997-11-24 2002-10-15 Alstom Method and apparatus for controlling thermoacoustic vibrations in a combustion system
EP1255074A1 (en) * 2001-05-01 2002-11-06 ABB Schweiz AG Oscillation reduction in a combustion chamber

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5487266A (en) * 1992-05-05 1996-01-30 General Electric Company Combustion control for producing low NOx emissions through use of flame spectroscopy
DE19636093B4 (en) * 1996-09-05 2004-07-29 Siemens Ag Method and device for acoustic modulation of a flame generated by a hybrid burner

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5533329A (en) * 1993-05-17 1996-07-09 Hitachi, Ltd. Control apparatus for and control method of gas turbine
DE4414232A1 (en) * 1994-04-23 1995-10-26 Abb Management Ag Device for damping thermoacoustic vibrations in a combustion chamber
US5544478A (en) * 1994-11-15 1996-08-13 General Electric Company Optical sensing of combustion dynamics
US6205764B1 (en) * 1997-02-06 2001-03-27 Jakob Hermann Method for the active damping of combustion oscillation and combustion apparatus
US6464489B1 (en) * 1997-11-24 2002-10-15 Alstom Method and apparatus for controlling thermoacoustic vibrations in a combustion system
EP0962704A2 (en) * 1998-05-29 1999-12-08 United Technologies Corporation Method and apparatus for use with a gas fueled combustor
EP1096201A1 (en) * 1999-10-29 2001-05-02 Siemens Aktiengesellschaft Burner
EP1180646A1 (en) * 2000-08-10 2002-02-20 ROLLS-ROYCE plc A combustion chamber
EP1255074A1 (en) * 2001-05-01 2002-11-06 ABB Schweiz AG Oscillation reduction in a combustion chamber

Also Published As

Publication number Publication date
WO2005093326A2 (en) 2005-10-06
DE102004015186A1 (en) 2005-10-20

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