DE69617290D1 - Combustion device for gas turbine engine - Google Patents
Combustion device for gas turbine engineInfo
- Publication number
- DE69617290D1 DE69617290D1 DE69617290T DE69617290T DE69617290D1 DE 69617290 D1 DE69617290 D1 DE 69617290D1 DE 69617290 T DE69617290 T DE 69617290T DE 69617290 T DE69617290 T DE 69617290T DE 69617290 D1 DE69617290 D1 DE 69617290D1
- Authority
- DE
- Germany
- Prior art keywords
- gas turbine
- turbine engine
- combustion device
- combustion
- engine
- 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
Links
- 238000002485 combustion reaction Methods 0.000 title 1
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
- F23D14/46—Details, e.g. noise reduction means
- F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
- F23D14/74—Preventing flame lift-off
-
- 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
- F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
-
- 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
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C2202/00—Fluegas recirculation
- F23C2202/40—Inducing local whirls around flame
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2204/00—Burners adapted for simultaneous or alternative combustion having more than one fuel supply
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2206/00—Burners for specific applications
- F23D2206/10—Turbines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2207/00—Ignition devices associated with burner
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
- F23D2900/00016—Preventing or reducing deposit build-up on burner parts, e.g. from carbon
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feeding And Controlling Fuel (AREA)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB9500627A GB2297151B (en) | 1995-01-13 | 1995-01-13 | Fuel injector arrangement for gas-or liquid-fuelled turbine |
GBGB9519826.3A GB9519826D0 (en) | 1995-09-29 | 1995-09-29 | Gas turbine engine combustor |
Publications (2)
Publication Number | Publication Date |
---|---|
DE69617290D1 true DE69617290D1 (en) | 2002-01-10 |
DE69617290T2 DE69617290T2 (en) | 2002-06-13 |
Family
ID=26306317
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE1996617290 Expired - Lifetime DE69617290T2 (en) | 1995-01-13 | 1996-01-15 | Combustion device for gas turbine engine |
Country Status (3)
Country | Link |
---|---|
EP (1) | EP0728989B1 (en) |
JP (1) | JPH08240129A (en) |
DE (1) | DE69617290T2 (en) |
Families Citing this family (27)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB2332509B (en) | 1997-12-19 | 2002-06-19 | Europ Gas Turbines Ltd | Fuel/air mixing arrangement for combustion apparatus |
EP0931980B1 (en) * | 1998-01-23 | 2003-04-09 | ALSTOM (Switzerland) Ltd | Burner for operating a heat generator |
GB2333832A (en) | 1998-01-31 | 1999-08-04 | Europ Gas Turbines Ltd | Multi-fuel gas turbine engine combustor |
GB2337102A (en) * | 1998-05-09 | 1999-11-10 | Europ Gas Turbines Ltd | Gas-turbine engine combustor |
DE19925328A1 (en) * | 1999-06-02 | 2000-12-07 | Abb Patent Gmbh | Device for igniting the combustion in a combustion chamber of a gas turbine |
US6374615B1 (en) | 2000-01-28 | 2002-04-23 | Alliedsignal, Inc | Low cost, low emissions natural gas combustor |
EP1139020B1 (en) * | 2000-04-01 | 2006-08-23 | Alstom Technology Ltd | Gas turbine engine combustion system |
JP2003035417A (en) | 2001-07-24 | 2003-02-07 | Mitsubishi Heavy Ind Ltd | Pilot nozzle for gas turbine combustion device |
US7284378B2 (en) | 2004-06-04 | 2007-10-23 | General Electric Company | Methods and apparatus for low emission gas turbine energy generation |
GB2432655A (en) * | 2005-11-26 | 2007-05-30 | Siemens Ag | Combustion apparatus |
EP1835231A1 (en) * | 2006-03-13 | 2007-09-19 | Siemens Aktiengesellschaft | Burner in particular for a gas turbine combustor, and method of operating a burner |
JP5023526B2 (en) | 2006-03-23 | 2012-09-12 | 株式会社Ihi | Combustor burner and combustion method |
EP2187128A4 (en) * | 2007-08-10 | 2015-07-29 | Kawasaki Heavy Ind Ltd | COMBUSTION CHAMBER |
US8096132B2 (en) | 2008-02-20 | 2012-01-17 | Flexenergy Energy Systems, Inc. | Air-cooled swirlerhead |
DE102008019117A1 (en) | 2008-04-16 | 2009-10-22 | Man Turbo Ag | Method for operating a premix burner and a premix burner for carrying out the method |
DE102009045950A1 (en) | 2009-10-23 | 2011-04-28 | Man Diesel & Turbo Se | swirl generator |
EP2400222A1 (en) * | 2010-06-28 | 2011-12-28 | Siemens Aktiengesellschaft | A combustion apparatus |
EP2489939A1 (en) * | 2011-02-18 | 2012-08-22 | Siemens Aktiengesellschaft | Combustion chamber with a wall section and a brim element |
RU2485398C1 (en) * | 2011-10-20 | 2013-06-20 | Общество с ограниченной ответственностью "Энерго Эстейт" | Device for fuel burning and method of fuel burning |
JP6035123B2 (en) * | 2012-11-26 | 2016-11-30 | 三菱日立パワーシステムズ株式会社 | Gas turbine combustor |
EP2743581A1 (en) | 2012-12-11 | 2014-06-18 | Siemens Aktiengesellschaft | Air directed fuel injection |
EP3301374A1 (en) * | 2016-09-29 | 2018-04-04 | Siemens Aktiengesellschaft | A pilot burner assembly with pilot-air supply |
DE102017102085A1 (en) * | 2017-02-02 | 2018-08-02 | Max Weishaupt Gmbh | Premixing method, this combustion method using as well as premixing device and burner provided therewith |
US10947902B2 (en) * | 2017-06-13 | 2021-03-16 | Haier Us Appliance Solutions, Inc. | Fuel nozzle, fuel supply assembly thereof, and method of assembling a fuel nozzle |
DE102017114362A1 (en) * | 2017-06-28 | 2019-01-03 | Man Diesel & Turbo Se | Combustion chamber of a gas turbine, gas turbine and method for operating the same |
DE102018125848A1 (en) * | 2018-10-18 | 2020-04-23 | Man Energy Solutions Se | Combustion chamber of a gas turbine, gas turbine and method for operating the same |
US11073114B2 (en) * | 2018-12-12 | 2021-07-27 | General Electric Company | Fuel injector assembly for a heat engine |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3930369A (en) * | 1974-02-04 | 1976-01-06 | General Motors Corporation | Lean prechamber outflow combustor with two sets of primary air entrances |
GB1465689A (en) * | 1974-10-25 | 1977-02-23 | Parkinson Cowan Appliances Ltd | Burners for firing a combustion chamber |
US4261518A (en) * | 1979-06-08 | 1981-04-14 | Union Carbide Corporation | Burner cap for synthesis of hydrogen chloride by combustion |
GB2100409B (en) * | 1981-04-24 | 1984-10-03 | Rolls Royce | Gas turbine engine fuel burners |
GB2104641B (en) * | 1981-07-28 | 1985-02-27 | Cherny Anatoly A | Method and apparatus for feeding fuel into an oxidizing atmosphere during its combustion |
US4609150A (en) * | 1983-07-19 | 1986-09-02 | United Technologies Corporation | Fuel nozzle for gas turbine engine |
EP0276696B1 (en) * | 1987-01-26 | 1990-09-12 | Siemens Aktiengesellschaft | Hybrid burner for premix operation with gas and/or oil, particularly for gas turbine plants |
JP3154163B2 (en) * | 1991-05-23 | 2001-04-09 | 三井造船株式会社 | Gas turbine combustor |
NL9300934A (en) * | 1993-06-01 | 1995-01-02 | Ingbureaugoedkoop B V | Burner head |
US5450724A (en) * | 1993-08-27 | 1995-09-19 | Northern Research & Engineering Corporation | Gas turbine apparatus including fuel and air mixer |
JP2950720B2 (en) | 1994-02-24 | 1999-09-20 | 株式会社東芝 | Gas turbine combustion device and combustion control method therefor |
-
1996
- 1996-01-15 EP EP19960300281 patent/EP0728989B1/en not_active Expired - Lifetime
- 1996-01-15 DE DE1996617290 patent/DE69617290T2/en not_active Expired - Lifetime
- 1996-01-16 JP JP2310896A patent/JPH08240129A/en active Pending
Also Published As
Publication number | Publication date |
---|---|
EP0728989A2 (en) | 1996-08-28 |
JPH08240129A (en) | 1996-09-17 |
EP0728989A3 (en) | 1997-08-20 |
EP0728989B1 (en) | 2001-11-28 |
DE69617290T2 (en) | 2002-06-13 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
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 |