NO20022563L - FremgangsmÕte og innretning for Õ blande brennstoff for Õ begrense utslipp fra brenneren - Google Patents
FremgangsmÕte og innretning for Õ blande brennstoff for Õ begrense utslipp fra brennerenInfo
- Publication number
- NO20022563L NO20022563L NO20022563A NO20022563A NO20022563L NO 20022563 L NO20022563 L NO 20022563L NO 20022563 A NO20022563 A NO 20022563A NO 20022563 A NO20022563 A NO 20022563A NO 20022563 L NO20022563 L NO 20022563L
- Authority
- NO
- Norway
- Prior art keywords
- mixing fuel
- limit burner
- burner emissions
- emissions
- limit
- 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
- F23R3/02—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
- F23R3/286—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
- F23R3/28—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
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US09/871,343 US6484489B1 (en) | 2001-05-31 | 2001-05-31 | Method and apparatus for mixing fuel to decrease combustor emissions |
Publications (3)
| Publication Number | Publication Date |
|---|---|
| NO20022563D0 NO20022563D0 (no) | 2002-05-30 |
| NO20022563L true NO20022563L (no) | 2002-12-02 |
| NO332838B1 NO332838B1 (no) | 2013-01-21 |
Family
ID=25357242
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| NO20022563A NO332838B1 (no) | 2001-05-31 | 2002-05-30 | Fremgangsmate og innretning for a blande brennstoff for a begrense utslipp fra brenneren |
Country Status (6)
| Country | Link |
|---|---|
| US (1) | US6484489B1 (no) |
| EP (1) | EP1262718B1 (no) |
| JP (1) | JP4162429B2 (no) |
| BR (1) | BR0201961B1 (no) |
| DE (1) | DE60237262D1 (no) |
| NO (1) | NO332838B1 (no) |
Families Citing this family (57)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20020162333A1 (en) * | 2001-05-02 | 2002-11-07 | Honeywell International, Inc., Law Dept. Ab2 | Partial premix dual circuit fuel injector |
| US6865889B2 (en) | 2002-02-01 | 2005-03-15 | General Electric Company | Method and apparatus to decrease combustor emissions |
| US6898938B2 (en) * | 2003-04-24 | 2005-05-31 | General Electric Company | Differential pressure induced purging fuel injector with asymmetric cyclone |
| US7121095B2 (en) * | 2003-08-11 | 2006-10-17 | General Electric Company | Combustor dome assembly of a gas turbine engine having improved deflector plates |
| US6976363B2 (en) * | 2003-08-11 | 2005-12-20 | General Electric Company | Combustor dome assembly of a gas turbine engine having a contoured swirler |
| US7062920B2 (en) * | 2003-08-11 | 2006-06-20 | General Electric Company | Combustor dome assembly of a gas turbine engine having a free floating swirler |
| US7104464B2 (en) * | 2003-12-25 | 2006-09-12 | Kawasaki Jukogyo Kabushiki Kaisha | Fuel supply method and fuel supply system |
| US8348180B2 (en) | 2004-06-09 | 2013-01-08 | Delavan Inc | Conical swirler for fuel injectors and combustor domes and methods of manufacturing the same |
| US7581396B2 (en) * | 2005-07-25 | 2009-09-01 | General Electric Company | Mixer assembly for combustor of a gas turbine engine having a plurality of counter-rotating swirlers |
| US20070028595A1 (en) * | 2005-07-25 | 2007-02-08 | Mongia Hukam C | High pressure gas turbine engine having reduced emissions |
| US7565803B2 (en) * | 2005-07-25 | 2009-07-28 | General Electric Company | Swirler arrangement for mixer assembly of a gas turbine engine combustor having shaped passages |
| US20070028618A1 (en) * | 2005-07-25 | 2007-02-08 | General Electric Company | Mixer assembly for combustor of a gas turbine engine having a main mixer with improved fuel penetration |
| US7415826B2 (en) * | 2005-07-25 | 2008-08-26 | General Electric Company | Free floating mixer assembly for combustor of a gas turbine engine |
| US7464553B2 (en) * | 2005-07-25 | 2008-12-16 | General Electric Company | Air-assisted fuel injector for mixer assembly of a gas turbine engine combustor |
| US7878000B2 (en) * | 2005-12-20 | 2011-02-01 | General Electric Company | Pilot fuel injector for mixer assembly of a high pressure gas turbine engine |
| US7762073B2 (en) * | 2006-03-01 | 2010-07-27 | General Electric Company | Pilot mixer for mixer assembly of a gas turbine engine combustor having a primary fuel injector and a plurality of secondary fuel injection ports |
| US8001761B2 (en) * | 2006-05-23 | 2011-08-23 | General Electric Company | Method and apparatus for actively controlling fuel flow to a mixer assembly of a gas turbine engine combustor |
| US20100251719A1 (en) | 2006-12-29 | 2010-10-07 | Alfred Albert Mancini | Centerbody for mixer assembly of a gas turbine engine combustor |
| RU2343356C1 (ru) * | 2007-05-21 | 2009-01-10 | Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" | Кольцевая камера сгорания газотурбинного двигателя и способ ее работы |
| DE102007034737A1 (de) | 2007-07-23 | 2009-01-29 | General Electric Co. | Verfahren und Vorrichtung zur aktiven Steuerung des Brennstoffzustroms zu einer Mischeinheit einer Gasturbinenbrennkammer |
| DE102007038220A1 (de) | 2007-08-13 | 2009-02-19 | General Electric Co. | Pilotmischer für eine Mischeinrichtung einer Gasturbinentriebwerksbrennkammer mit einer primären Brennstoffeinspritzeinrichtung und mehreren sekundären Brennstoffeinspritzanschlüssen |
| DE102007050276A1 (de) * | 2007-10-18 | 2009-04-23 | Rolls-Royce Deutschland Ltd & Co Kg | Magervormischbrenner für ein Gasturbinentriebwerk |
| US7926744B2 (en) * | 2008-02-21 | 2011-04-19 | Delavan Inc | Radially outward flowing air-blast fuel injector for gas turbine engine |
| US8061142B2 (en) | 2008-04-11 | 2011-11-22 | General Electric Company | Mixer for a combustor |
| US8225610B2 (en) * | 2008-12-08 | 2012-07-24 | General Electric Company | Fuel delivery system and method of assembling the same |
| US20100263382A1 (en) | 2009-04-16 | 2010-10-21 | Alfred Albert Mancini | Dual orifice pilot fuel injector |
| US8437941B2 (en) | 2009-05-08 | 2013-05-07 | Gas Turbine Efficiency Sweden Ab | Automated tuning of gas turbine combustion systems |
| US9671797B2 (en) | 2009-05-08 | 2017-06-06 | Gas Turbine Efficiency Sweden Ab | Optimization of gas turbine combustion systems low load performance on simple cycle and heat recovery steam generator applications |
| US9267443B2 (en) | 2009-05-08 | 2016-02-23 | Gas Turbine Efficiency Sweden Ab | Automated tuning of gas turbine combustion systems |
| US9354618B2 (en) | 2009-05-08 | 2016-05-31 | Gas Turbine Efficiency Sweden Ab | Automated tuning of multiple fuel gas turbine combustion systems |
| US8365532B2 (en) * | 2009-09-30 | 2013-02-05 | General Electric Company | Apparatus and method for a gas turbine nozzle |
| US9027350B2 (en) * | 2009-12-30 | 2015-05-12 | Rolls-Royce Corporation | Gas turbine engine having dome panel assembly with bifurcated swirler flow |
| US20110162375A1 (en) * | 2010-01-05 | 2011-07-07 | General Electric Company | Secondary Combustion Fuel Supply Systems |
| US20120151928A1 (en) | 2010-12-17 | 2012-06-21 | Nayan Vinodbhai Patel | Cooling flowpath dirt deflector in fuel nozzle |
| US8726668B2 (en) | 2010-12-17 | 2014-05-20 | General Electric Company | Fuel atomization dual orifice fuel nozzle |
| US9920932B2 (en) | 2011-01-26 | 2018-03-20 | United Technologies Corporation | Mixer assembly for a gas turbine engine |
| US8312724B2 (en) | 2011-01-26 | 2012-11-20 | United Technologies Corporation | Mixer assembly for a gas turbine engine having a pilot mixer with a corner flame stabilizing recirculation zone |
| US8973368B2 (en) | 2011-01-26 | 2015-03-10 | United Technologies Corporation | Mixer assembly for a gas turbine engine |
| US8893500B2 (en) | 2011-05-18 | 2014-11-25 | Solar Turbines Inc. | Lean direct fuel injector |
| US8919132B2 (en) | 2011-05-18 | 2014-12-30 | Solar Turbines Inc. | Method of operating a gas turbine engine |
| JP5044034B2 (ja) * | 2011-07-26 | 2012-10-10 | 川崎重工業株式会社 | ガスタービンエンジンの燃料噴霧装置 |
| US11015808B2 (en) | 2011-12-13 | 2021-05-25 | General Electric Company | Aerodynamically enhanced premixer with purge slots for reduced emissions |
| US9182124B2 (en) | 2011-12-15 | 2015-11-10 | Solar Turbines Incorporated | Gas turbine and fuel injector for the same |
| US20130232978A1 (en) * | 2012-03-12 | 2013-09-12 | Zhongtao Dai | Fuel air premixer for gas turbine engine |
| JP5924618B2 (ja) * | 2012-06-07 | 2016-05-25 | 川崎重工業株式会社 | 燃料噴射装置 |
| CN103423768B (zh) * | 2013-08-09 | 2015-07-29 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种双燃料燃烧室喷嘴自身引气清吹系统 |
| CN105765305B (zh) | 2013-11-27 | 2018-05-08 | 通用电气公司 | 具有流体锁和吹扫设备的燃料喷嘴 |
| CN105829802B (zh) | 2013-12-23 | 2018-02-23 | 通用电气公司 | 具有柔性支承结构的燃料喷嘴 |
| WO2015147934A1 (en) | 2013-12-23 | 2015-10-01 | General Electric Company | Fuel nozzle structure for air-assisted fuel injection |
| CA2938876C (en) | 2014-02-13 | 2019-10-22 | General Electric Company | Anti-coking coatings, processes therefor, and hydrocarbon fluid passages provided therewith |
| US20150285502A1 (en) * | 2014-04-08 | 2015-10-08 | General Electric Company | Fuel nozzle shroud and method of manufacturing the shroud |
| US10502425B2 (en) * | 2016-06-03 | 2019-12-10 | General Electric Company | Contoured shroud swirling pre-mix fuel injector assembly |
| US10738704B2 (en) | 2016-10-03 | 2020-08-11 | Raytheon Technologies Corporation | Pilot/main fuel shifting in an axial staged combustor for a gas turbine engine |
| US11561008B2 (en) | 2017-08-23 | 2023-01-24 | General Electric Company | Fuel nozzle assembly for high fuel/air ratio and reduced combustion dynamics |
| US11480338B2 (en) | 2017-08-23 | 2022-10-25 | General Electric Company | Combustor system for high fuel/air ratio and reduced combustion dynamics |
| US10557630B1 (en) | 2019-01-15 | 2020-02-11 | Delavan Inc. | Stackable air swirlers |
| CN117490098A (zh) * | 2023-11-24 | 2024-02-02 | 哈尔滨工程大学 | 用于宽含氧量工况的分级旋流器结构 |
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| US2551276A (en) | 1949-01-22 | 1951-05-01 | Gen Electric | Dual vortex liquid spray nozzle |
| US2968925A (en) | 1959-11-25 | 1961-01-24 | William E Blevans | Fuel nozzle head for anti-coking |
| US3302399A (en) | 1964-11-13 | 1967-02-07 | Westinghouse Electric Corp | Hollow conical fuel spray nozzle for pressurized combustion apparatus |
| US3474970A (en) | 1967-03-15 | 1969-10-28 | Parker Hannifin Corp | Air assist nozzle |
| US3630024A (en) | 1970-02-02 | 1971-12-28 | Gen Electric | Air swirler for gas turbine combustor |
| US3638865A (en) | 1970-08-31 | 1972-02-01 | Gen Electric | Fuel spray nozzle |
| US3899884A (en) | 1970-12-02 | 1975-08-19 | Gen Electric | Combustor systems |
| US3853273A (en) | 1973-10-01 | 1974-12-10 | Gen Electric | Axial swirler central injection carburetor |
| US3980233A (en) | 1974-10-07 | 1976-09-14 | Parker-Hannifin Corporation | Air-atomizing fuel nozzle |
| US4198815A (en) | 1975-12-24 | 1980-04-22 | General Electric Company | Central injection fuel carburetor |
| US4105163A (en) | 1976-10-27 | 1978-08-08 | General Electric Company | Fuel nozzle for gas turbines |
| US4216652A (en) * | 1978-06-08 | 1980-08-12 | General Motors Corporation | Integrated, replaceable combustor swirler and fuel injector |
| US4567857A (en) | 1980-02-26 | 1986-02-04 | The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration | Combustion engine system |
| US4418543A (en) | 1980-12-02 | 1983-12-06 | United Technologies Corporation | Fuel nozzle for gas turbine engine |
| US4845940A (en) | 1981-02-27 | 1989-07-11 | Westinghouse Electric Corp. | Low NOx rich-lean combustor especially useful in gas turbines |
| US4584834A (en) | 1982-07-06 | 1986-04-29 | General Electric Company | Gas turbine engine carburetor |
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| GB2175993B (en) | 1985-06-07 | 1988-12-21 | Rolls Royce | Improvements in or relating to dual fuel injectors |
| CA1306873C (en) | 1987-04-27 | 1992-09-01 | Jack R. Taylor | Low coke fuel injector for a gas turbine engine |
| JP2518986Y2 (ja) * | 1989-01-20 | 1996-12-04 | 川崎重工業株式会社 | ガスタービンの燃焼器 |
| US5097666A (en) | 1989-12-11 | 1992-03-24 | Sundstrand Corporation | Combustor fuel injection system |
| US5323604A (en) | 1992-11-16 | 1994-06-28 | General Electric Company | Triple annular combustor for gas turbine engine |
| US5435884A (en) | 1993-09-30 | 1995-07-25 | Parker-Hannifin Corporation | Spray nozzle and method of manufacturing same |
| GB9326367D0 (en) * | 1993-12-23 | 1994-02-23 | Rolls Royce Plc | Fuel injection apparatus |
| US5444982A (en) | 1994-01-12 | 1995-08-29 | General Electric Company | Cyclonic prechamber with a centerbody |
| DE69506308T2 (de) | 1994-04-20 | 1999-08-26 | Rolls-Royce Plc | Brennstoffeinspritzdüse für Gasturbinentriebwerke |
| US5584178A (en) | 1994-06-14 | 1996-12-17 | Southwest Research Institute | Exhaust gas combustor |
| US5590529A (en) | 1994-09-26 | 1997-01-07 | General Electric Company | Air fuel mixer for gas turbine combustor |
| US5613363A (en) | 1994-09-26 | 1997-03-25 | General Electric Company | Air fuel mixer for gas turbine combustor |
| JPH08261464A (ja) * | 1995-03-20 | 1996-10-11 | Ishikawajima Harima Heavy Ind Co Ltd | 乱流混合燃料噴射弁 |
| US5822992A (en) | 1995-10-19 | 1998-10-20 | General Electric Company | Low emissions combustor premixer |
| US6047550A (en) | 1996-05-02 | 2000-04-11 | General Electric Co. | Premixing dry low NOx emissions combustor with lean direct injection of gas fuel |
| AU7357298A (en) | 1997-03-26 | 1998-10-20 | San Diego State University Foundation | Fuel/air mixing device for jet engines |
| EP0995066B1 (de) * | 1997-07-17 | 2001-09-26 | Siemens Aktiengesellschaft | Brenneranordnung für eine feuerungsanlage, insbesondere eine gasturbinenbrennkammer |
| US6141967A (en) | 1998-01-09 | 2000-11-07 | General Electric Company | Air fuel mixer for gas turbine combustor |
| US6195607B1 (en) | 1999-07-06 | 2001-02-27 | General Electric Company | Method and apparatus for optimizing NOx emissions in a gas turbine |
| US6363726B1 (en) * | 2000-09-29 | 2002-04-02 | General Electric Company | Mixer having multiple swirlers |
| US6381964B1 (en) * | 2000-09-29 | 2002-05-07 | General Electric Company | Multiple annular combustion chamber swirler having atomizing pilot |
-
2001
- 2001-05-31 US US09/871,343 patent/US6484489B1/en not_active Expired - Lifetime
-
2002
- 2002-05-20 EP EP02253541A patent/EP1262718B1/en not_active Expired - Lifetime
- 2002-05-20 DE DE60237262T patent/DE60237262D1/de not_active Expired - Lifetime
- 2002-05-27 BR BRPI0201961-2A patent/BR0201961B1/pt not_active IP Right Cessation
- 2002-05-30 NO NO20022563A patent/NO332838B1/no not_active IP Right Cessation
- 2002-05-30 JP JP2002156535A patent/JP4162429B2/ja not_active Expired - Fee Related
Also Published As
| Publication number | Publication date |
|---|---|
| NO332838B1 (no) | 2013-01-21 |
| EP1262718B1 (en) | 2010-08-11 |
| JP4162429B2 (ja) | 2008-10-08 |
| US6484489B1 (en) | 2002-11-26 |
| US20020178732A1 (en) | 2002-12-05 |
| BR0201961B1 (pt) | 2011-11-16 |
| EP1262718A3 (en) | 2005-09-07 |
| BR0201961A (pt) | 2003-04-22 |
| NO20022563D0 (no) | 2002-05-30 |
| DE60237262D1 (de) | 2010-09-23 |
| EP1262718A2 (en) | 2002-12-04 |
| JP2003004231A (ja) | 2003-01-08 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| MM1K | Lapsed by not paying the annual fees |