ES2058667T3 - Camara de combustion de una turbina de gas. - Google Patents
Camara de combustion de una turbina de gas.Info
- Publication number
- ES2058667T3 ES2058667T3 ES90108684T ES90108684T ES2058667T3 ES 2058667 T3 ES2058667 T3 ES 2058667T3 ES 90108684 T ES90108684 T ES 90108684T ES 90108684 T ES90108684 T ES 90108684T ES 2058667 T3 ES2058667 T3 ES 2058667T3
- Authority
- ES
- Spain
- Prior art keywords
- burners
- chamber
- combustion chamber
- gas turbine
- combustion
- 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
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
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/40—Mixing tubes or chambers; Burner heads
- F23D11/402—Mixing chambers downstream of the nozzle
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23D—BURNERS
- F23D17/00—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel
- F23D17/002—Burners for combustion conjointly or alternatively of gaseous or liquid or pulverulent fuel gaseous or liquid fuel
-
- 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
- F23R3/02—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
-
- 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
- F23R3/42—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
-
- 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
- F23C2900/00—Special features of, or arrangements for combustion apparatus using fluid fuels or solid fuels suspended in air; Combustion processes therefor
- F23C2900/07002—Premix burners with air inlet slots obtained between offset curved wall surfaces, e.g. double cone burners
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Engine Equipment That Uses Special Cycles (AREA)
- Combustion Of Fluid Fuel (AREA)
- Combustion Methods Of Internal-Combustion Engines (AREA)
Abstract
EN UNA CAMARA DE COMBUSTION (A) EN FORMA DE UNA CAMARA CIRCULAS, SE ENCUENTRAN, A LO LARGO DE LA PARED FRONTAL (10) EN FORMA DE ANILLA, UNA SERIE DE QUEMADORES PREVIOS (B, C). LOS QUEMADORES PREVIOS GRANDES (B), QUE FORMAN LOS QUEMADORES PRINCIPALES DE LA CAMARA DE COMBUSTION (A) Y LOS QUEMADORES PREVIOS PEQUEÑOS (C), QUE SON LOS QUEMADORES PILOTO DE LA CAMARA (A), ESTAN COLOCADOS DE FORMA ALTERNA Y CON DISTANCIAS UNIFORMES, A LO LARGO DE LA PARED FORNTAL (10), DONDE DESEMBOCAN EN EL ESPACIO DE COMBUSTION DE LA CAMARA (A). ENTRE LOS QUEMADORES GRANDES (B) Y LOS PEQUEÑOS (C) SE ENCUENTRAN VARIAS TOBERAS DE AIRE (D) DIRIGIDAS HACIA EL ESPACIO DE COMBUSTION DE LA CAMARA (A).
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CH2099/89A CH680084A5 (es) | 1989-06-06 | 1989-06-06 |
Publications (1)
Publication Number | Publication Date |
---|---|
ES2058667T3 true ES2058667T3 (es) | 1994-11-01 |
Family
ID=4225860
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
ES90108684T Expired - Lifetime ES2058667T3 (es) | 1989-06-06 | 1990-05-09 | Camara de combustion de una turbina de gas. |
Country Status (10)
Country | Link |
---|---|
US (1) | US5154059A (es) |
EP (1) | EP0401529B1 (es) |
JP (1) | JP3075732B2 (es) |
AT (1) | ATE108011T1 (es) |
CH (1) | CH680084A5 (es) |
DE (1) | DE59006282D1 (es) |
ES (1) | ES2058667T3 (es) |
HU (1) | HUT56923A (es) |
PL (1) | PL165109B1 (es) |
RU (1) | RU2002165C1 (es) |
Families Citing this family (26)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0481111B1 (de) * | 1990-10-17 | 1995-06-28 | Asea Brown Boveri Ag | Brennkammer einer Gasturbine |
GB2257781B (en) * | 1991-04-30 | 1995-04-12 | Rolls Royce Plc | Combustion chamber assembly in a gas turbine engine |
CH684963A5 (de) * | 1991-11-13 | 1995-02-15 | Asea Brown Boveri | Ringbrennkammer. |
FR2683891B1 (fr) * | 1991-11-20 | 1995-03-24 | Snecma | Turbomachine comportant un dispositif pour diminuer l'emission d'oxydes d'azote. |
DE4411624A1 (de) * | 1994-04-02 | 1995-10-05 | Abb Management Ag | Brennkammer mit Vormischbrennern |
DE4412315B4 (de) * | 1994-04-11 | 2005-12-15 | Alstom | Verfahren und Vorrichtung zum Betreiben der Brennkammer einer Gasturbine |
DE4429539C2 (de) * | 1994-08-19 | 2002-10-24 | Alstom | Verfahren zur Drehzahlregelung einer Gasturbine bei Lastabwurf |
DE4429757A1 (de) * | 1994-08-22 | 1996-02-29 | Abb Management Ag | Brennkammer |
US5479773A (en) * | 1994-10-13 | 1996-01-02 | United Technologies Corporation | Tangential air entry fuel nozzle |
DE19523094A1 (de) * | 1995-06-26 | 1997-01-02 | Abb Management Ag | Brennkammer |
US5896739A (en) * | 1996-12-20 | 1999-04-27 | United Technologies Corporation | Method of disgorging flames from a two stream tangential entry nozzle |
US6176087B1 (en) * | 1997-12-15 | 2001-01-23 | United Technologies Corporation | Bluff body premixing fuel injector and method for premixing fuel and air |
DE19948674B4 (de) * | 1999-10-08 | 2012-04-12 | Alstom | Verbrennungseinrichtung, insbesondere für den Antrieb von Gasturbinen |
DE10000415A1 (de) * | 2000-01-07 | 2001-09-06 | Alstom Power Schweiz Ag Baden | Verfahren und Vorrichtung zur Unterdrückung von Strömungswirbeln innerhalb einer Strömungskraftmaschine |
DE10049203A1 (de) * | 2000-10-05 | 2002-05-23 | Alstom Switzerland Ltd | Verfahren zur Brennstoffeinleitung in einen Vormischbrenner |
US6360776B1 (en) | 2000-11-01 | 2002-03-26 | Rolls-Royce Corporation | Apparatus for premixing in a gas turbine engine |
DE10205839B4 (de) * | 2002-02-13 | 2011-08-11 | Alstom Technology Ltd. | Vormischbrenner zur Verminderung verbrennungsgetriebener Schwingungen in Verbrennungssystemen |
DE10219354A1 (de) * | 2002-04-30 | 2003-11-13 | Rolls Royce Deutschland | Gasturbinenbrennkammer mit gezielter Kraftstoffeinbringung zur Verbesserung der Homogenität des Kraftstoff-Luft-Gemisches |
US6931853B2 (en) * | 2002-11-19 | 2005-08-23 | Siemens Westinghouse Power Corporation | Gas turbine combustor having staged burners with dissimilar mixing passage geometries |
US7097448B2 (en) * | 2004-05-07 | 2006-08-29 | Peter Chesney | Vortex type gas lamp |
DE102007043626A1 (de) | 2007-09-13 | 2009-03-19 | Rolls-Royce Deutschland Ltd & Co Kg | Gasturbinenmagerbrenner mit Kraftstoffdüse mit kontrollierter Kraftstoffinhomogenität |
US8122725B2 (en) * | 2007-11-01 | 2012-02-28 | General Electric Company | Methods and systems for operating gas turbine engines |
FR2950109B1 (fr) * | 2009-09-17 | 2012-07-27 | Turbomeca | Turbomoteur a arbres paralleles |
CA2786597A1 (en) | 2010-01-06 | 2011-07-14 | The Outdoor Greatroom Company LLLP | Fire container assembly |
EP2685163B1 (en) * | 2012-07-10 | 2020-03-25 | Ansaldo Energia Switzerland AG | Premix burner of the multi-cone type for a gas turbine |
RU2561754C1 (ru) | 2014-02-12 | 2015-09-10 | Открытое акционерное общество "Газпром" | Кольцевая камера сгорания газотурбинного двигателя и способ её эксплуатации |
Family Cites Families (11)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR944310A (fr) * | 1946-01-09 | 1949-04-01 | Bendix Aviat Corp | Brûleurs |
US3267676A (en) * | 1965-06-23 | 1966-08-23 | Curtiss Wright Corp | Fuel burner structure |
US3512359A (en) * | 1968-05-24 | 1970-05-19 | Gen Electric | Dummy swirl cup combustion chamber |
DE2223093A1 (de) * | 1972-05-12 | 1973-11-22 | Gen Electric | Brenner und brennstoffinjektor |
US3834159A (en) * | 1973-08-03 | 1974-09-10 | Gen Electric | Combustion apparatus |
US4058977A (en) * | 1974-12-18 | 1977-11-22 | United Technologies Corporation | Low emission combustion chamber |
US4194358A (en) * | 1977-12-15 | 1980-03-25 | General Electric Company | Double annular combustor configuration |
GB2043868B (en) * | 1979-03-08 | 1982-12-15 | Rolls Royce | Gas turbine |
GB2072827A (en) * | 1980-03-29 | 1981-10-07 | Rolls Royce | A tubo-annular combustion chamber |
DE3662462D1 (en) * | 1985-07-30 | 1989-04-20 | Bbc Brown Boveri & Cie | Dual combustor |
CH674561A5 (es) * | 1987-12-21 | 1990-06-15 | Bbc Brown Boveri & Cie |
-
1989
- 1989-06-06 CH CH2099/89A patent/CH680084A5/de not_active IP Right Cessation
-
1990
- 1990-05-09 DE DE59006282T patent/DE59006282D1/de not_active Expired - Fee Related
- 1990-05-09 ES ES90108684T patent/ES2058667T3/es not_active Expired - Lifetime
- 1990-05-09 EP EP90108684A patent/EP0401529B1/de not_active Expired - Lifetime
- 1990-05-09 AT AT90108684T patent/ATE108011T1/de not_active IP Right Cessation
- 1990-06-01 PL PL90285434A patent/PL165109B1/pl unknown
- 1990-06-05 RU SU904830017A patent/RU2002165C1/ru active
- 1990-06-05 HU HU903493A patent/HUT56923A/hu unknown
- 1990-06-05 JP JP02145541A patent/JP3075732B2/ja not_active Expired - Fee Related
-
1992
- 1992-03-16 US US07/851,125 patent/US5154059A/en not_active Expired - Lifetime
Also Published As
Publication number | Publication date |
---|---|
DE59006282D1 (de) | 1994-08-04 |
JPH0320524A (ja) | 1991-01-29 |
JP3075732B2 (ja) | 2000-08-14 |
HUT56923A (en) | 1991-10-28 |
EP0401529A1 (de) | 1990-12-12 |
HU903493D0 (en) | 1990-10-28 |
US5154059A (en) | 1992-10-13 |
CH680084A5 (es) | 1992-06-15 |
EP0401529B1 (de) | 1994-06-29 |
ATE108011T1 (de) | 1994-07-15 |
PL285434A1 (en) | 1991-10-21 |
PL165109B1 (pl) | 1994-11-30 |
RU2002165C1 (ru) | 1993-10-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
FG2A | Definitive protection |
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