NO176116C - Brennkammer og fremgangsmåte for lav NOx-emisjon i en gassturbin - Google Patents
Brennkammer og fremgangsmåte for lav NOx-emisjon i en gassturbinInfo
- Publication number
- NO176116C NO176116C NO910418A NO910418A NO176116C NO 176116 C NO176116 C NO 176116C NO 910418 A NO910418 A NO 910418A NO 910418 A NO910418 A NO 910418A NO 176116 C NO176116 C NO 176116C
- Authority
- NO
- Norway
- Prior art keywords
- combustion chamber
- gas turbine
- nox emission
- low nox
- emission
- Prior art date
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
- F23R3/30—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply comprising fuel prevapourising 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
-
- 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
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/474,394 US5117636A (en) | 1990-02-05 | 1990-02-05 | Low nox emission in gas turbine system |
Publications (4)
Publication Number | Publication Date |
---|---|
NO910418D0 NO910418D0 (no) | 1991-02-04 |
NO910418L NO910418L (no) | 1991-08-06 |
NO176116B NO176116B (no) | 1994-10-24 |
NO176116C true NO176116C (no) | 1995-02-01 |
Family
ID=23883334
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO910418A NO176116C (no) | 1990-02-05 | 1991-02-04 | Brennkammer og fremgangsmåte for lav NOx-emisjon i en gassturbin |
Country Status (7)
Country | Link |
---|---|
US (1) | US5117636A (de) |
EP (1) | EP0441542B1 (de) |
JP (1) | JPH0769057B2 (de) |
KR (1) | KR950013648B1 (de) |
CN (1) | CN1050890C (de) |
DE (1) | DE69101794T2 (de) |
NO (1) | NO176116C (de) |
Families Citing this family (50)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5274991A (en) * | 1992-03-30 | 1994-01-04 | General Electric Company | Dry low NOx multi-nozzle combustion liner cap assembly |
US5309710A (en) * | 1992-11-20 | 1994-05-10 | General Electric Company | Gas turbine combustor having poppet valves for air distribution control |
FR2717250B1 (fr) * | 1994-03-10 | 1996-04-12 | Snecma | Système d'injection à prémélange. |
US5454221A (en) * | 1994-03-14 | 1995-10-03 | General Electric Company | Dilution flow sleeve for reducing emissions in a gas turbine combustor |
US5669218A (en) * | 1995-05-31 | 1997-09-23 | Dresser-Rand Company | Premix fuel nozzle |
GB9929601D0 (en) * | 1999-12-16 | 2000-02-09 | Rolls Royce Plc | A combustion chamber |
WO2003093664A1 (en) * | 2000-06-28 | 2003-11-13 | Power Systems Mfg. Llc | Combustion chamber/venturi cooling for a low nox emission combustor |
US6427446B1 (en) * | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
US6430932B1 (en) | 2001-07-19 | 2002-08-13 | Power Systems Mfg., Llc | Low NOx combustion liner with cooling air plenum recesses |
DE50204080D1 (de) | 2002-04-29 | 2005-10-06 | Agfa Gevaert Nv | Strahlungsempfindliches Gemisch, damit hergestelltes Aufzeichnungsmaterial, und Verfahren zur Herstellung einer Druckplatte |
US7314699B2 (en) | 2002-04-29 | 2008-01-01 | Agfa Graphics Nv | Radiation-sensitive mixture and recording material produced therewith |
US6928822B2 (en) * | 2002-05-28 | 2005-08-16 | Lytesyde, Llc | Turbine engine apparatus and method |
US6772595B2 (en) | 2002-06-25 | 2004-08-10 | Power Systems Mfg., Llc | Advanced cooling configuration for a low emissions combustor venturi |
US6832482B2 (en) | 2002-06-25 | 2004-12-21 | Power Systems Mfg, Llc | Pressure ram device on a gas turbine combustor |
CN100354565C (zh) * | 2002-10-10 | 2007-12-12 | Lpp燃烧有限责任公司 | 汽化燃烧用液体燃料的系统及其使用方法 |
US6865892B2 (en) * | 2002-12-17 | 2005-03-15 | Power Systems Mfg, Llc | Combustion chamber/venturi configuration and assembly method |
US7284378B2 (en) | 2004-06-04 | 2007-10-23 | General Electric Company | Methods and apparatus for low emission gas turbine energy generation |
US7093441B2 (en) * | 2003-10-09 | 2006-08-22 | United Technologies Corporation | Gas turbine annular combustor having a first converging volume and a second converging volume, converging less gradually than the first converging volume |
JP2006105534A (ja) * | 2004-10-07 | 2006-04-20 | Niigata Power Systems Co Ltd | ガスタービン燃焼器 |
US7308793B2 (en) * | 2005-01-07 | 2007-12-18 | Power Systems Mfg., Llc | Apparatus and method for reducing carbon monoxide emissions |
US7389643B2 (en) * | 2005-01-31 | 2008-06-24 | General Electric Company | Inboard radial dump venturi for combustion chamber of a gas turbine |
JP2007147125A (ja) * | 2005-11-25 | 2007-06-14 | Mitsubishi Heavy Ind Ltd | ガスタービン燃焼器 |
US7716931B2 (en) * | 2006-03-01 | 2010-05-18 | General Electric Company | Method and apparatus for assembling gas turbine engine |
US8156743B2 (en) * | 2006-05-04 | 2012-04-17 | General Electric Company | Method and arrangement for expanding a primary and secondary flame in a combustor |
US7878798B2 (en) * | 2006-06-14 | 2011-02-01 | John Zink Company, Llc | Coanda gas burner apparatus and methods |
US7895841B2 (en) * | 2006-07-14 | 2011-03-01 | General Electric Company | Method and apparatus to facilitate reducing NOx emissions in turbine engines |
US8707704B2 (en) * | 2007-05-31 | 2014-04-29 | General Electric Company | Method and apparatus for assembling turbine engines |
US20090019854A1 (en) * | 2007-07-16 | 2009-01-22 | General Electric Company | APPARATUS/METHOD FOR COOLING COMBUSTION CHAMBER/VENTURI IN A LOW NOx COMBUSTOR |
US8096133B2 (en) * | 2008-05-13 | 2012-01-17 | General Electric Company | Method and apparatus for cooling and dilution tuning a gas turbine combustor liner and transition piece interface |
US7874157B2 (en) * | 2008-06-05 | 2011-01-25 | General Electric Company | Coanda pilot nozzle for low emission combustors |
US8887390B2 (en) | 2008-08-15 | 2014-11-18 | Dresser-Rand Company | Method for correcting downstream deflection in gas turbine nozzles |
FR2941287B1 (fr) * | 2009-01-19 | 2011-03-25 | Snecma | Paroi de chambre de combustion de turbomachine a une seule rangee annulaire d'orifices d'entree d'air primaire et de dilution |
US7712314B1 (en) * | 2009-01-21 | 2010-05-11 | Gas Turbine Efficiency Sweden Ab | Venturi cooling system |
US20100192587A1 (en) * | 2009-02-03 | 2010-08-05 | William Kirk Hessler | Combustor assembly for use in a gas turbine engine and method of assembling same |
US20100319353A1 (en) * | 2009-06-18 | 2010-12-23 | John Charles Intile | Multiple Fuel Circuits for Syngas/NG DLN in a Premixed Nozzle |
US20110167828A1 (en) * | 2010-01-08 | 2011-07-14 | Arjun Singh | Combustor assembly for a turbine engine that mixes combustion products with purge air |
US8646277B2 (en) * | 2010-02-19 | 2014-02-11 | General Electric Company | Combustor liner for a turbine engine with venturi and air deflector |
US20110225974A1 (en) * | 2010-03-22 | 2011-09-22 | General Electric Company | Multiple Zone Pilot For Low Emission Combustion System |
US8931280B2 (en) | 2011-04-26 | 2015-01-13 | General Electric Company | Fully impingement cooled venturi with inbuilt resonator for reduced dynamics and better heat transfer capabilities |
US8955329B2 (en) | 2011-10-21 | 2015-02-17 | General Electric Company | Diffusion nozzles for low-oxygen fuel nozzle assembly and method |
GB201202907D0 (en) * | 2012-02-21 | 2012-04-04 | Doosan Power Systems Ltd | Burner |
JP6326205B2 (ja) * | 2013-07-30 | 2018-05-16 | 三菱日立パワーシステムズ株式会社 | 燃料ノズル、燃焼器、及びガスタービン |
US9752458B2 (en) | 2013-12-04 | 2017-09-05 | General Electric Company | System and method for a gas turbine engine |
CN105805943A (zh) * | 2016-04-22 | 2016-07-27 | 广东三水大鸿制釉有限公司 | 一种热风烤窑装置及其使用方法 |
CN108506935B (zh) * | 2018-05-28 | 2024-08-30 | 杭州浙大天元科技有限公司 | 基于燃气内循环的低NOx燃气燃烧器及降低排放的方法 |
CN116265810A (zh) * | 2021-12-16 | 2023-06-20 | 通用电气公司 | 利用成形冷却栅栏的旋流器反稀释 |
CN114486273B (zh) * | 2021-12-27 | 2024-08-30 | 国网浙江省电力有限公司电力科学研究院 | 一种园区灵活性改造机组氢混燃烧试验装置 |
US11835236B1 (en) | 2022-07-05 | 2023-12-05 | General Electric Company | Combustor with reverse dilution air introduction |
CN115523510B (zh) * | 2022-09-02 | 2023-10-13 | 哈尔滨工程大学 | 一种预混程度可调的氢燃料低排放燃烧室头部 |
CN115638420A (zh) * | 2022-12-06 | 2023-01-24 | 无锡国联环保科技股份有限公司 | 一种用于流化床污泥焚烧炉的助燃装置和方法 |
Family Cites Families (16)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH367662A (fr) * | 1959-07-07 | 1963-02-28 | Rover Co Ltd | Groupe à turbine à gaz |
US3851466A (en) * | 1973-04-12 | 1974-12-03 | Gen Motors Corp | Combustion apparatus |
US3905192A (en) * | 1974-08-29 | 1975-09-16 | United Aircraft Corp | Combustor having staged premixing tubes |
US3958413A (en) * | 1974-09-03 | 1976-05-25 | General Motors Corporation | Combustion method and apparatus |
US3958416A (en) * | 1974-12-12 | 1976-05-25 | General Motors Corporation | Combustion apparatus |
US3946553A (en) * | 1975-03-10 | 1976-03-30 | United Technologies Corporation | Two-stage premixed combustor |
US4030875A (en) * | 1975-12-22 | 1977-06-21 | General Electric Company | Integrated ceramic-metal combustor |
US4420929A (en) * | 1979-01-12 | 1983-12-20 | General Electric Company | Dual stage-dual mode low emission gas turbine combustion system |
US4292801A (en) * | 1979-07-11 | 1981-10-06 | General Electric Company | Dual stage-dual mode low nox combustor |
DE2937631A1 (de) * | 1979-09-18 | 1981-04-02 | Daimler-Benz Ag, 7000 Stuttgart | Brennkammer fuer gasturbinen |
US4413477A (en) * | 1980-12-29 | 1983-11-08 | General Electric Company | Liner assembly for gas turbine combustor |
US4845940A (en) * | 1981-02-27 | 1989-07-11 | Westinghouse Electric Corp. | Low NOx rich-lean combustor especially useful in gas turbines |
GB2116308B (en) * | 1982-03-08 | 1985-11-13 | Westinghouse Electric Corp | Improved low-nox, rich-lean combustor |
US4819438A (en) * | 1982-12-23 | 1989-04-11 | United States Of America | Steam cooled rich-burn combustor liner |
US4984429A (en) * | 1986-11-25 | 1991-01-15 | General Electric Company | Impingement cooled liner for dry low NOx venturi combustor |
US4912931A (en) * | 1987-10-16 | 1990-04-03 | Prutech Ii | Staged low NOx gas turbine combustor |
-
1990
- 1990-02-05 US US07/474,394 patent/US5117636A/en not_active Expired - Lifetime
-
1991
- 1991-01-23 JP JP3021344A patent/JPH0769057B2/ja not_active Expired - Lifetime
- 1991-02-01 EP EP91300808A patent/EP0441542B1/de not_active Expired - Lifetime
- 1991-02-01 DE DE69101794T patent/DE69101794T2/de not_active Expired - Lifetime
- 1991-02-04 NO NO910418A patent/NO176116C/no not_active IP Right Cessation
- 1991-02-04 KR KR1019910001856A patent/KR950013648B1/ko not_active IP Right Cessation
- 1991-02-05 CN CN91100704A patent/CN1050890C/zh not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
EP0441542B1 (de) | 1994-04-27 |
DE69101794T2 (de) | 1994-12-15 |
JPH04214122A (ja) | 1992-08-05 |
US5117636A (en) | 1992-06-02 |
NO910418D0 (no) | 1991-02-04 |
NO176116B (no) | 1994-10-24 |
CN1050890C (zh) | 2000-03-29 |
KR950013648B1 (ko) | 1995-11-13 |
NO910418L (no) | 1991-08-06 |
CN1054823A (zh) | 1991-09-25 |
EP0441542A1 (de) | 1991-08-14 |
DE69101794D1 (de) | 1994-06-01 |
JPH0769057B2 (ja) | 1995-07-26 |
KR910015817A (ko) | 1991-09-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
MK1K | Patent expired |