EP1710502A3 - Gas burner assembly for a gas turbine - Google Patents

Gas burner assembly for a gas turbine Download PDF

Info

Publication number
EP1710502A3
EP1710502A3 EP06111895A EP06111895A EP1710502A3 EP 1710502 A3 EP1710502 A3 EP 1710502A3 EP 06111895 A EP06111895 A EP 06111895A EP 06111895 A EP06111895 A EP 06111895A EP 1710502 A3 EP1710502 A3 EP 1710502A3
Authority
EP
European Patent Office
Prior art keywords
gas
burner
swirler
burner assembly
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.)
Granted
Application number
EP06111895A
Other languages
German (de)
French (fr)
Other versions
EP1710502B1 (en
EP1710502A2 (en
Inventor
Federico Bonzani
Giacomo Pollarolo
Vittorio Corona
Carlo Piana
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.)
Ansaldo Energia SpA
Original Assignee
Ansaldo Energia SpA
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 Ansaldo Energia SpA filed Critical Ansaldo Energia SpA
Publication of EP1710502A2 publication Critical patent/EP1710502A2/en
Publication of EP1710502A3 publication Critical patent/EP1710502A3/en
Application granted granted Critical
Publication of EP1710502B1 publication Critical patent/EP1710502B1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/286Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply having fuel-air premixing devices
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/02Continuous combustion chambers using liquid or gaseous fuel characterised by the air-flow or gas-flow configuration
    • F23R3/04Air inlet arrangements
    • F23R3/10Air inlet arrangements for primary air
    • F23R3/12Air inlet arrangements for primary air inducing a vortex
    • F23R3/14Air inlet arrangements for primary air inducing a vortex by using swirl vanes
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R3/00Continuous combustion chambers using liquid or gaseous fuel
    • F23R3/28Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
    • F23R3/34Feeding into different combustion zones
    • F23R3/343Pilot flames, i.e. fuel nozzles or injectors using only a very small proportion of the total fuel to insure continuous combustion
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00016Retrofitting in general, e.g. to respect new regulations on pollution
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23RGENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
    • F23R2900/00Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/03343Pilot burners operating in premixed mode

Abstract

A gas burner assembly for a gas turbine has a first, premix, burner (5), and a second burner (4) surrounded by the first burner (5); the second burner has a swirler (16) with vanes (21), a channel (40, 55) for feeding combustion air into the gaps (22) in the swirler (16), and at least a first gas feed line (52) for feeding a stream of fuel gas into the gaps (22); the first gas feed line (52) has an outlet (51) designed to generate a premix pilot flame, and the channel (40) has a number of calibrated-section choke holes (56) for setting combustion air flow to the swirler (16).
EP06111895.6A 2005-03-30 2006-03-29 Gas burner assembly for a gas turbine Active EP1710502B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITTO20050208 ITTO20050208A1 (en) 2005-03-30 2005-03-30 GAS BURNER GROUP FOR A GAS TURBINE

Publications (3)

Publication Number Publication Date
EP1710502A2 EP1710502A2 (en) 2006-10-11
EP1710502A3 true EP1710502A3 (en) 2007-03-14
EP1710502B1 EP1710502B1 (en) 2016-05-11

Family

ID=36648560

Family Applications (1)

Application Number Title Priority Date Filing Date
EP06111895.6A Active EP1710502B1 (en) 2005-03-30 2006-03-29 Gas burner assembly for a gas turbine

Country Status (2)

Country Link
EP (1) EP1710502B1 (en)
IT (1) ITTO20050208A1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2444640C2 (en) * 2007-08-01 2012-03-10 Ансальдо Энергия С.П.А. Device and method of gas turbine engine exhaust temperature adjustment

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP2169312A1 (en) * 2008-09-25 2010-03-31 Siemens Aktiengesellschaft Stepped swirler for dynamic control
ITMI20090556A1 (en) * 2009-04-07 2010-10-08 Ansaldo Energia Spa METHOD FOR OPERATING A GAS TURBINE PLANT
EP2244015A1 (en) * 2009-04-23 2010-10-27 Siemens Aktiengesellschaft Pre-mix burner
US8590864B2 (en) * 2010-10-21 2013-11-26 Woodward Fst, Inc. Semi-tubular vane air swirler
ITMI20110808A1 (en) * 2011-05-10 2012-11-11 Ansaldo Energia Spa BURNER GROUP FOR A GAS TURBINE AND METHOD FOR FUEL FEEDING TO A COMBUSTION CHAMBER OF A GAS TURBINE
ITMI20111943A1 (en) * 2011-10-26 2013-04-27 Ansaldo Energia Spa METHOD TO MODIFY A BURNER GROUP OF A GAS TURBINE
EP2886955A1 (en) * 2013-12-17 2015-06-24 Siemens Aktiengesellschaft Calibration means for air flow adjustment of a gas turbine swirler
CN106247408B (en) * 2016-07-27 2019-01-18 中国科学院工程热物理研究所 A kind of nozzle, nozzle array and burner for widening tempering nargin

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2280022A (en) * 1993-06-28 1995-01-18 Toshiba Kk Gas turbine combustor
WO1999004196A1 (en) * 1997-07-17 1999-01-28 Siemens Aktiengesellschaft Arrangement of burners for heating installation, in particular a gas turbine combustion chamber
WO2000012933A1 (en) * 1998-08-26 2000-03-09 Siemens Aktiengesellschaft Hybrid burner and method for operating a hybrid burner
EP1193449A2 (en) * 2000-09-29 2002-04-03 General Electric Company Multiple annular swirler
DE10104695A1 (en) * 2001-02-02 2002-08-08 Alstom Switzerland Ltd Premix burner and method for operating such a premix burner
EP1400754A1 (en) * 2002-09-23 2004-03-24 Siemens Westinghouse Power Corporation Premixed pilot burner for a combustion turbine engine
US20040144094A1 (en) * 1999-12-15 2004-07-29 Koji Moriya Fluid distributor, burner apparatus, gas turbine engine and co-generation system
EP1645805A1 (en) * 2004-10-11 2006-04-12 Siemens Aktiengesellschaft burner for fluidic fuels and method for operating such a burner

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
EP1614967B1 (en) * 2004-07-09 2016-03-16 Siemens Aktiengesellschaft Method and premixed combustion system

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2280022A (en) * 1993-06-28 1995-01-18 Toshiba Kk Gas turbine combustor
WO1999004196A1 (en) * 1997-07-17 1999-01-28 Siemens Aktiengesellschaft Arrangement of burners for heating installation, in particular a gas turbine combustion chamber
WO2000012933A1 (en) * 1998-08-26 2000-03-09 Siemens Aktiengesellschaft Hybrid burner and method for operating a hybrid burner
US20040144094A1 (en) * 1999-12-15 2004-07-29 Koji Moriya Fluid distributor, burner apparatus, gas turbine engine and co-generation system
EP1193449A2 (en) * 2000-09-29 2002-04-03 General Electric Company Multiple annular swirler
DE10104695A1 (en) * 2001-02-02 2002-08-08 Alstom Switzerland Ltd Premix burner and method for operating such a premix burner
EP1400754A1 (en) * 2002-09-23 2004-03-24 Siemens Westinghouse Power Corporation Premixed pilot burner for a combustion turbine engine
EP1645805A1 (en) * 2004-10-11 2006-04-12 Siemens Aktiengesellschaft burner for fluidic fuels and method for operating such a burner

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
MAGHON H ET AL: "PROGRESS IN NOX AND CO EMISSION REDUCTION OF GAS TURBINES", AMERICAN SOCIETY OF MECHANICAL ENGINEERS SYMPOSIA SERIES, NEW YORK,NY, US, 21 October 1990 (1990-10-21), pages 1 - 7, XP000648263 *

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2444640C2 (en) * 2007-08-01 2012-03-10 Ансальдо Энергия С.П.А. Device and method of gas turbine engine exhaust temperature adjustment

Also Published As

Publication number Publication date
EP1710502B1 (en) 2016-05-11
EP1710502A2 (en) 2006-10-11
ITTO20050208A1 (en) 2006-09-30

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