EP1710502A3 - Gas burner assembly for a gas turbine - Google Patents
Gas burner assembly for a gas turbine Download PDFInfo
- 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
Links
- 239000007789 gas Substances 0.000 abstract 4
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 239000002737 fuel gas Substances 0.000 abstract 1
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
- 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
- F23R3/02—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
- F23R3/34—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
- 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
- F23R2900/00016—Retrofitting in general, e.g. to respect new regulations on pollution
-
- 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
Abstract
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)
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)
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)
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)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP1614967B1 (en) * | 2004-07-09 | 2016-03-16 | Siemens Aktiengesellschaft | Method and premixed combustion system |
-
2005
- 2005-03-30 IT ITTO20050208 patent/ITTO20050208A1/en unknown
-
2006
- 2006-03-29 EP EP06111895.6A patent/EP1710502B1/en active Active
Patent Citations (8)
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)
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)
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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