NO931169D0 - Kappe for brenner med lavt nox-utslipp - Google Patents
Kappe for brenner med lavt nox-utslippInfo
- Publication number
- NO931169D0 NO931169D0 NO931169A NO931169A NO931169D0 NO 931169 D0 NO931169 D0 NO 931169D0 NO 931169 A NO931169 A NO 931169A NO 931169 A NO931169 A NO 931169A NO 931169 D0 NO931169 D0 NO 931169D0
- Authority
- NO
- Norway
- Prior art keywords
- burner
- cover
- nox emissions
- low nox
- emissions
- Prior art date
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C3/00—Gas-turbine plants characterised by the use of combustion products as the working fluid
- F02C3/14—Gas-turbine plants characterised by the use of combustion products as the working fluid characterised by the arrangement of the combustion chamber in the plant
-
- 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
-
- 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
-
- 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
- F23R3/50—Combustion chambers comprising an annular flame tube within an annular casing
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Turbine Rotor Nozzle Sealing (AREA)
- Spray-Type Burners (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US85900592A | 1992-03-30 | 1992-03-30 |
Publications (3)
Publication Number | Publication Date |
---|---|
NO931169D0 true NO931169D0 (no) | 1993-03-29 |
NO931169L NO931169L (no) | 1993-10-01 |
NO300343B1 NO300343B1 (no) | 1997-05-12 |
Family
ID=25329741
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO931169A NO300343B1 (no) | 1992-03-30 | 1993-03-29 | Brennerhetteenhet med lavt NOx-utslipp |
Country Status (8)
Country | Link |
---|---|
US (1) | US5357745A (no) |
EP (1) | EP0564181B1 (no) |
JP (1) | JPH0618040A (no) |
KR (1) | KR930019991A (no) |
CN (1) | CN1080383A (no) |
CA (1) | CA2092947A1 (no) |
DE (1) | DE69306025T2 (no) |
NO (1) | NO300343B1 (no) |
Families Citing this family (49)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5415000A (en) * | 1994-06-13 | 1995-05-16 | Westinghouse Electric Corporation | Low NOx combustor retro-fit system for gas turbines |
GB2295887A (en) * | 1994-12-08 | 1996-06-12 | Rolls Royce Plc | Combustor assembly |
GB2339468B (en) * | 1998-07-11 | 2002-04-24 | Alstom Gas Turbines Ltd | Gas-turbine engine combustion system |
US6427446B1 (en) * | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
KR100395118B1 (ko) * | 2000-12-22 | 2003-08-21 | 한전기공주식회사 | 연소기 캡 분해조립방법 |
JP4709433B2 (ja) * | 2001-06-29 | 2011-06-22 | 三菱重工業株式会社 | ガスタービン燃焼器 |
US6672073B2 (en) * | 2002-05-22 | 2004-01-06 | Siemens Westinghouse Power Corporation | System and method for supporting fuel nozzles in a gas turbine combustor utilizing a support plate |
US6910336B2 (en) * | 2003-02-18 | 2005-06-28 | Power Systems Mfg. Llc | Combustion liner cap assembly attachment and sealing system |
US6923002B2 (en) * | 2003-08-28 | 2005-08-02 | General Electric Company | Combustion liner cap assembly for combustion dynamics reduction |
US6951109B2 (en) | 2004-01-06 | 2005-10-04 | General Electric Company | Apparatus and methods for minimizing and/or eliminating dilution air leakage in a combustion liner assembly |
US7827797B2 (en) | 2006-09-05 | 2010-11-09 | General Electric Company | Injection assembly for a combustor |
US8438853B2 (en) * | 2008-01-29 | 2013-05-14 | Alstom Technology Ltd. | Combustor end cap assembly |
US20090223227A1 (en) * | 2008-03-05 | 2009-09-10 | General Electric Company | Combustion cap with crown mixing holes |
US8104291B2 (en) * | 2008-03-27 | 2012-01-31 | General Electric Company | Combustion cap floating collar using E-seal |
US20100050640A1 (en) * | 2008-08-29 | 2010-03-04 | General Electric Company | Thermally compliant combustion cap device and system |
US8087228B2 (en) * | 2008-09-11 | 2012-01-03 | General Electric Company | Segmented combustor cap |
US8091367B2 (en) * | 2008-09-26 | 2012-01-10 | Pratt & Whitney Canada Corp. | Combustor with improved cooling holes arrangement |
US20100089022A1 (en) * | 2008-10-14 | 2010-04-15 | General Electric Company | Method and apparatus of fuel nozzle diluent introduction |
US8567199B2 (en) * | 2008-10-14 | 2013-10-29 | General Electric Company | Method and apparatus of introducing diluent flow into a combustor |
US20100089020A1 (en) * | 2008-10-14 | 2010-04-15 | General Electric Company | Metering of diluent flow in combustor |
US9121609B2 (en) * | 2008-10-14 | 2015-09-01 | General Electric Company | Method and apparatus for introducing diluent flow into a combustor |
US8528336B2 (en) * | 2009-03-30 | 2013-09-10 | General Electric Company | Fuel nozzle spring support for shifting a natural frequency |
US20100263384A1 (en) * | 2009-04-17 | 2010-10-21 | Ronald James Chila | Combustor cap with shaped effusion cooling holes |
US8495881B2 (en) * | 2009-06-02 | 2013-07-30 | General Electric Company | System and method for thermal control in a cap of a gas turbine combustor |
US8373089B2 (en) * | 2009-08-31 | 2013-02-12 | General Electric Company | Combustion cap effusion plate laser weld repair |
US20110100016A1 (en) * | 2009-11-02 | 2011-05-05 | David Cihlar | Apparatus and methods for fuel nozzle frequency adjustment |
US8272224B2 (en) * | 2009-11-02 | 2012-09-25 | General Electric Company | Apparatus and methods for fuel nozzle frequency adjustment |
US8381526B2 (en) * | 2010-02-15 | 2013-02-26 | General Electric Company | Systems and methods of providing high pressure air to a head end of a combustor |
RU2534189C2 (ru) * | 2010-02-16 | 2014-11-27 | Дженерал Электрик Компани | Камера сгорания для газовой турбины(варианты) и способ эксплуатации газовой турбины |
US8769955B2 (en) | 2010-06-02 | 2014-07-08 | Siemens Energy, Inc. | Self-regulating fuel staging port for turbine combustor |
US8572979B2 (en) * | 2010-06-24 | 2013-11-05 | United Technologies Corporation | Gas turbine combustor liner cap assembly |
JP5606346B2 (ja) * | 2011-01-27 | 2014-10-15 | 三菱重工業株式会社 | ガスタービン燃焼器 |
US9291102B2 (en) * | 2011-09-07 | 2016-03-22 | Siemens Energy, Inc. | Interface ring for gas turbine fuel nozzle assemblies |
CN103486617B (zh) * | 2012-06-13 | 2015-10-14 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种用于燃气轮机的双燃料低排放燃烧器 |
US9249976B2 (en) | 2012-06-28 | 2016-02-02 | General Electric Company | Method for servicing a combustor cap assembly for a turbine |
US9003803B2 (en) | 2012-08-03 | 2015-04-14 | General Electric Company | Combustor cap assembly |
US9175855B2 (en) | 2012-10-29 | 2015-11-03 | General Electric Company | Combustion nozzle with floating aft plate |
US8756934B2 (en) | 2012-10-30 | 2014-06-24 | General Electric Company | Combustor cap assembly |
US9297533B2 (en) | 2012-10-30 | 2016-03-29 | General Electric Company | Combustor and a method for cooling the combustor |
US9228747B2 (en) * | 2013-03-12 | 2016-01-05 | Pratt & Whitney Canada Corp. | Combustor for gas turbine engine |
WO2015023764A1 (en) * | 2013-08-16 | 2015-02-19 | United Technologies Corporation | Gas turbine engine combustor bulkhead assembly |
US9890954B2 (en) | 2014-08-19 | 2018-02-13 | General Electric Company | Combustor cap assembly |
US9470421B2 (en) | 2014-08-19 | 2016-10-18 | General Electric Company | Combustor cap assembly |
US9964308B2 (en) | 2014-08-19 | 2018-05-08 | General Electric Company | Combustor cap assembly |
RU2656177C1 (ru) * | 2014-11-03 | 2018-05-31 | Сименс Акциенгезелльшафт | Компоновка горелки |
US9835333B2 (en) | 2014-12-23 | 2017-12-05 | General Electric Company | System and method for utilizing cooling air within a combustor |
US10429073B2 (en) | 2015-12-21 | 2019-10-01 | General Electric Company | Combustor cap module and retention system therefor |
US10330204B2 (en) * | 2017-11-10 | 2019-06-25 | Rolls-Royce Deutschland Ltd & Co Kg | Burner seal of a gas turbine and method for manufacturing the same |
CN113669758B (zh) * | 2021-08-26 | 2023-07-11 | 中国联合重型燃气轮机技术有限公司 | 燃烧室罩帽及具有它的燃气轮机 |
Family Cites Families (25)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CH260957A (de) * | 1945-11-20 | 1949-04-15 | Westinghouse Electric Corp | Verbrennungseinrichtung für Gasturbinenanlage. |
US2608057A (en) * | 1949-12-24 | 1952-08-26 | A V Roe Canada Ltd | Gas turbine nozzle box |
US2676460A (en) * | 1950-03-23 | 1954-04-27 | United Aircraft Corp | Burner construction of the can-an-nular type having means for distributing airflow to each can |
US2729938A (en) * | 1951-01-26 | 1956-01-10 | Gen Motors Corp | Combustion chamber crossover tube |
US2801520A (en) * | 1954-08-05 | 1957-08-06 | Axel L Highberg | Removable burner cans |
GB812404A (en) * | 1955-07-28 | 1959-04-22 | Napier & Son Ltd | Internal combustion turbine units |
US2813397A (en) * | 1957-01-02 | 1957-11-19 | United Aircraft Corp | Thermal expansion means for combustion chambers |
GB892949A (en) * | 1959-10-14 | 1962-04-04 | Lucas Industries Ltd | Liquid fuel combustion apparatus |
NL267395A (no) * | 1960-07-22 | |||
US3991562A (en) * | 1975-07-21 | 1976-11-16 | United Technologies Corporation | Combustion chamber assembly having removable center liner |
GB1539035A (en) * | 1976-04-22 | 1979-01-24 | Rolls Royce | Combustion chambers for gas turbine engines |
US4151713A (en) * | 1977-03-15 | 1979-05-01 | United Technologies Corporation | Burner for gas turbine engine |
US4180974A (en) * | 1977-10-31 | 1980-01-01 | General Electric Company | Combustor dome sleeve |
EP0019417B1 (en) * | 1979-05-18 | 1983-01-12 | Rolls-Royce Plc | Combustion apparatus for gas turbine engines |
US4292801A (en) * | 1979-07-11 | 1981-10-06 | General Electric Company | Dual stage-dual mode low nox combustor |
US4573315A (en) * | 1984-05-15 | 1986-03-04 | A/S Kongsberg Vapenfabrikk | Low pressure loss, convectively gas-cooled inlet manifold for high temperature radial turbine |
JPH0660740B2 (ja) * | 1985-04-05 | 1994-08-10 | 工業技術院長 | ガスタービンの燃焼器 |
US5012645A (en) * | 1987-08-03 | 1991-05-07 | United Technologies Corporation | Combustor liner construction for gas turbine engine |
US4843825A (en) * | 1988-05-16 | 1989-07-04 | United Technologies Corporation | Combustor dome heat shield |
US5235478A (en) * | 1989-12-15 | 1993-08-10 | Sony Corporation | Disc drive apparatus with servo tracks offset from data tracks |
US5129231A (en) * | 1990-03-12 | 1992-07-14 | United Technologies Corporation | Cooled combustor dome heatshield |
US5127221A (en) * | 1990-05-03 | 1992-07-07 | General Electric Company | Transpiration cooled throat section for low nox combustor and related process |
US5117637A (en) * | 1990-08-02 | 1992-06-02 | General Electric Company | Combustor dome assembly |
GB9018013D0 (en) * | 1990-08-16 | 1990-10-03 | Rolls Royce Plc | Gas turbine engine combustor |
US5197289A (en) * | 1990-11-26 | 1993-03-30 | General Electric Company | Double dome combustor |
-
1993
- 1993-03-26 EP EP93302348A patent/EP0564181B1/en not_active Expired - Lifetime
- 1993-03-26 DE DE69306025T patent/DE69306025T2/de not_active Expired - Fee Related
- 1993-03-29 KR KR1019930004929A patent/KR930019991A/ko not_active Application Discontinuation
- 1993-03-29 NO NO931169A patent/NO300343B1/no unknown
- 1993-03-29 JP JP5069000A patent/JPH0618040A/ja not_active Withdrawn
- 1993-03-30 CA CA002092947A patent/CA2092947A1/en not_active Abandoned
- 1993-03-30 CN CN93105488A patent/CN1080383A/zh active Pending
-
1994
- 1994-03-15 US US08/214,053 patent/US5357745A/en not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
CN1080383A (zh) | 1994-01-05 |
DE69306025D1 (de) | 1997-01-02 |
CA2092947A1 (en) | 1993-10-01 |
EP0564181A1 (en) | 1993-10-06 |
NO300343B1 (no) | 1997-05-12 |
DE69306025T2 (de) | 1997-05-28 |
KR930019991A (ko) | 1993-10-19 |
EP0564181B1 (en) | 1996-11-20 |
NO931169L (no) | 1993-10-01 |
US5357745A (en) | 1994-10-25 |
JPH0618040A (ja) | 1994-01-25 |
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