NO180602C - Senterlegeme for et gassturbinbrennkammer - Google Patents
Senterlegeme for et gassturbinbrennkammerInfo
- Publication number
- NO180602C NO180602C NO925032A NO925032A NO180602C NO 180602 C NO180602 C NO 180602C NO 925032 A NO925032 A NO 925032A NO 925032 A NO925032 A NO 925032A NO 180602 C NO180602 C NO 180602C
- Authority
- NO
- Norway
- Prior art keywords
- combustion chamber
- gas turbine
- center body
- turbine combustion
- center
- 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
- F23R3/02—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
- F23R3/02—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
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)
- Gas Burners (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US07/813,745 US5253478A (en) | 1991-12-30 | 1991-12-30 | Flame holding diverging centerbody cup construction for a dry low NOx combustor |
Publications (4)
Publication Number | Publication Date |
---|---|
NO925032D0 NO925032D0 (no) | 1992-12-29 |
NO925032L NO925032L (no) | 1993-07-01 |
NO180602B NO180602B (no) | 1997-02-03 |
NO180602C true NO180602C (no) | 1997-05-14 |
Family
ID=25213266
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
NO925032A NO180602C (no) | 1991-12-30 | 1992-12-29 | Senterlegeme for et gassturbinbrennkammer |
Country Status (7)
Country | Link |
---|---|
US (1) | US5253478A (zh) |
EP (1) | EP0550218B1 (zh) |
JP (1) | JP3348113B2 (zh) |
KR (1) | KR100239082B1 (zh) |
CN (1) | CN1057152C (zh) |
DE (1) | DE69218576T2 (zh) |
NO (1) | NO180602C (zh) |
Families Citing this family (44)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5487275A (en) * | 1992-12-11 | 1996-01-30 | General Electric Co. | Tertiary fuel injection system for use in a dry low NOx combustion system |
BR9609032A (pt) * | 1995-06-06 | 1999-09-14 | Maxtor Corp | Micro posicionador diferencial para cabeçote mr. |
US5933699A (en) * | 1996-06-24 | 1999-08-03 | General Electric Company | Method of making double-walled turbine components from pre-consolidated assemblies |
US6082111A (en) * | 1998-06-11 | 2000-07-04 | Siemens Westinghouse Power Corporation | Annular premix section for dry low-NOx combustors |
DE69930455T2 (de) * | 1998-11-12 | 2006-11-23 | Mitsubishi Heavy Industries, Ltd. | Gasturbinenbrennkammer |
US6427446B1 (en) * | 2000-09-19 | 2002-08-06 | Power Systems Mfg., Llc | Low NOx emission combustion liner with circumferentially angled film cooling holes |
US6705087B1 (en) * | 2002-09-13 | 2004-03-16 | Siemens Westinghouse Power Corporation | Swirler assembly with improved vibrational response |
US7334410B2 (en) * | 2004-04-07 | 2008-02-26 | United Technologies Corporation | Swirler |
US7137258B2 (en) * | 2004-06-03 | 2006-11-21 | General Electric Company | Swirler configurations for combustor nozzles and related method |
US7574865B2 (en) * | 2004-11-18 | 2009-08-18 | Siemens Energy, Inc. | Combustor flow sleeve with optimized cooling and airflow distribution |
US7389643B2 (en) * | 2005-01-31 | 2008-06-24 | General Electric Company | Inboard radial dump venturi for combustion chamber of a gas turbine |
US7513098B2 (en) * | 2005-06-29 | 2009-04-07 | Siemens Energy, Inc. | Swirler assembly and combinations of same in gas turbine engine combustors |
US7716931B2 (en) * | 2006-03-01 | 2010-05-18 | General Electric Company | Method and apparatus for assembling gas turbine engine |
US8020385B2 (en) * | 2008-07-28 | 2011-09-20 | General Electric Company | Centerbody cap for a turbomachine combustor and method |
DE102008026463A1 (de) * | 2008-06-03 | 2009-12-10 | E.On Ruhrgas Ag | Verbrennungseinrichtung für eine Gasturbinenanlage |
US7874157B2 (en) * | 2008-06-05 | 2011-01-25 | General Electric Company | Coanda pilot nozzle for low emission combustors |
US8397512B2 (en) * | 2008-08-25 | 2013-03-19 | General Electric Company | Flow device for turbine engine and method of assembling same |
US8113000B2 (en) * | 2008-09-15 | 2012-02-14 | Siemens Energy, Inc. | Flashback resistant pre-mixer assembly |
US8056343B2 (en) * | 2008-10-01 | 2011-11-15 | General Electric Company | Off center combustor liner |
KR100969857B1 (ko) * | 2008-11-21 | 2010-07-13 | 한국생산기술연구원 | 연료 연소장치 |
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 |
US20100192582A1 (en) | 2009-02-04 | 2010-08-05 | Robert Bland | Combustor nozzle |
US8607568B2 (en) * | 2009-05-14 | 2013-12-17 | General Electric Company | Dry low NOx combustion system with pre-mixed direct-injection secondary fuel nozzle |
US20100293952A1 (en) * | 2009-05-21 | 2010-11-25 | General Electric Company | Resonating Swirler |
EP2256413A1 (de) * | 2009-05-27 | 2010-12-01 | Siemens Aktiengesellschaft | Brenner, Betriebsverfahren und Montageverfahren |
US9127842B2 (en) * | 2009-05-27 | 2015-09-08 | Siemens Aktiengesellschaft | Burner, operating method and assembly method |
US20100300107A1 (en) * | 2009-05-29 | 2010-12-02 | General Electric Company | Method and flow sleeve profile reduction to extend combustor liner life |
FR2951245B1 (fr) * | 2009-10-13 | 2013-05-17 | Snecma | Dispositif d'injection multi-point pour une chambre de combustion de turbomachine |
US8613187B2 (en) * | 2009-10-23 | 2013-12-24 | General Electric Company | Fuel flexible combustor systems and methods |
US8646277B2 (en) * | 2010-02-19 | 2014-02-11 | General Electric Company | Combustor liner for a turbine engine with venturi and air deflector |
RU2529987C2 (ru) * | 2010-03-25 | 2014-10-10 | Дженерал Электрик Компани | Камера сгорания и способ эксплуатации камеры сгорания |
US20120023951A1 (en) * | 2010-07-29 | 2012-02-02 | Nishant Govindbhai Parsania | Fuel nozzle with air admission shroud |
ES2462974T3 (es) * | 2010-08-16 | 2014-05-27 | Alstom Technology Ltd | Quemador de recalentamiento |
US20120055163A1 (en) * | 2010-09-08 | 2012-03-08 | Jong Ho Uhm | Fuel injection assembly for use in turbine engines and method of assembling same |
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 |
US9279325B2 (en) | 2012-11-08 | 2016-03-08 | General Electric Company | Turbomachine wheel assembly having slotted flanges |
US9303871B2 (en) * | 2013-06-26 | 2016-04-05 | Siemens Aktiengesellschaft | Combustor assembly including a transition inlet cone in a gas turbine engine |
CN104613466B (zh) * | 2015-01-17 | 2017-11-07 | 集美大学 | 一种带有天然气喷管和预燃室的双蜗壳旋流式煤粉燃烧器 |
CN105135479A (zh) * | 2015-09-17 | 2015-12-09 | 中国航空工业集团公司沈阳发动机设计研究所 | 一种中心体组件 |
JP6754595B2 (ja) * | 2016-03-30 | 2020-09-16 | 三菱日立パワーシステムズ株式会社 | ガスタービン |
US20220373182A1 (en) * | 2021-05-21 | 2022-11-24 | General Electric Company | Pilot fuel nozzle assembly with vented venturi |
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 |
Family Cites Families (19)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2627721A (en) * | 1947-01-30 | 1953-02-10 | Packard Motor Car Co | Combustion means for jet propulsion units |
GB742990A (en) * | 1952-10-07 | 1956-01-04 | Shell Refining & Marketing Co | Combustion chamber for gas turbines |
US2933888A (en) * | 1956-11-23 | 1960-04-26 | Africano Alfred | Cooling system for a rocket engine |
US2951339A (en) * | 1959-03-31 | 1960-09-06 | United Aircraft Corp | Combustion chamber swirler |
US3713588A (en) * | 1970-11-27 | 1973-01-30 | Gen Motors Corp | Liquid fuel spray nozzles with air atomization |
US3853273A (en) * | 1973-10-01 | 1974-12-10 | Gen Electric | Axial swirler central injection carburetor |
US4058977A (en) * | 1974-12-18 | 1977-11-22 | United Technologies Corporation | Low emission combustion chamber |
CH626436A5 (en) * | 1977-08-23 | 1981-11-13 | Proizv Ob Nevsky Z | Method of fuel combustion in combustion chambers and annular combustion chamber for its implementation |
US4292801A (en) * | 1979-07-11 | 1981-10-06 | General Electric Company | Dual stage-dual mode low nox combustor |
GB2072827A (en) * | 1980-03-29 | 1981-10-07 | Rolls Royce | A tubo-annular combustion chamber |
GB2134243A (en) * | 1983-01-27 | 1984-08-08 | Rolls Royce | Combustion equipment for a gas turbine engine |
FR2596102B1 (fr) * | 1986-03-20 | 1988-05-27 | Snecma | Dispositif d'injection a vrille axialo-centripete |
US4982570A (en) * | 1986-11-25 | 1991-01-08 | General Electric Company | Premixed pilot nozzle for dry low Nox combustor |
US4984429A (en) * | 1986-11-25 | 1991-01-15 | General Electric Company | Impingement cooled liner for dry low NOx venturi combustor |
CA1306873C (en) * | 1987-04-27 | 1992-09-01 | Jack R. Taylor | Low coke fuel injector for a gas turbine engine |
JPH0684817B2 (ja) * | 1988-08-08 | 1994-10-26 | 株式会社日立製作所 | ガスタービン燃焼器及びその運転方法 |
US4949538A (en) * | 1988-11-28 | 1990-08-21 | General Electric Company | Combustor gas feed with coordinated proportioning |
US4944149A (en) * | 1988-12-14 | 1990-07-31 | General Electric Company | Combustor liner with air staging for NOx control |
US5030871A (en) * | 1990-05-11 | 1991-07-09 | General Electric Company | Reducing harmonic losses in dynamoelectric machine rotors |
-
1991
- 1991-12-30 US US07/813,745 patent/US5253478A/en not_active Expired - Fee Related
-
1992
- 1992-11-28 KR KR1019920022696A patent/KR100239082B1/ko not_active IP Right Cessation
- 1992-12-17 EP EP92311531A patent/EP0550218B1/en not_active Expired - Lifetime
- 1992-12-17 DE DE69218576T patent/DE69218576T2/de not_active Expired - Fee Related
- 1992-12-28 JP JP34755792A patent/JP3348113B2/ja not_active Expired - Fee Related
- 1992-12-29 NO NO925032A patent/NO180602C/no unknown
- 1992-12-30 CN CN92111817A patent/CN1057152C/zh not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
JP3348113B2 (ja) | 2002-11-20 |
JPH05264038A (ja) | 1993-10-12 |
NO180602B (no) | 1997-02-03 |
DE69218576T2 (de) | 1997-10-02 |
NO925032D0 (no) | 1992-12-29 |
US5253478A (en) | 1993-10-19 |
CN1076013A (zh) | 1993-09-08 |
KR100239082B1 (ko) | 2000-01-15 |
DE69218576D1 (de) | 1997-04-30 |
NO925032L (no) | 1993-07-01 |
CN1057152C (zh) | 2000-10-04 |
EP0550218A1 (en) | 1993-07-07 |
KR930013442A (ko) | 1993-07-21 |
EP0550218B1 (en) | 1997-03-26 |
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