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
Application number
ES90108684T
Other languages
English (en)
Inventor
Jakob Dr Keller
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
ABB Asea Brown Boveri Ltd
ABB AB
Original Assignee
ABB Asea Brown Boveri Ltd
Asea Brown Boveri AB
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by ABB Asea Brown Boveri Ltd, Asea Brown Boveri AB filed Critical ABB Asea Brown Boveri Ltd
Application granted granted Critical
Publication of ES2058667T3 publication Critical patent/ES2058667T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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

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).
ES90108684T 1989-06-06 1990-05-09 Camara de combustion de una turbina de gas. Expired - Lifetime ES2058667T3 (es)

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)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
ATE124528T1 (de) * 1990-10-17 1995-07-15 Asea Brown Boveri 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
US9170017B2 (en) 2010-01-06 2015-10-27 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)

* Cited by examiner, † Cited by third party
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
EP0210462B1 (de) * 1985-07-30 1989-03-15 BBC Brown Boveri AG Dualbrenner
CH674561A5 (es) * 1987-12-21 1990-06-15 Bbc Brown Boveri & Cie

Also Published As

Publication number Publication date
EP0401529B1 (de) 1994-06-29
PL165109B1 (pl) 1994-11-30
JPH0320524A (ja) 1991-01-29
US5154059A (en) 1992-10-13
CH680084A5 (es) 1992-06-15
JP3075732B2 (ja) 2000-08-14
PL285434A1 (en) 1991-10-21
DE59006282D1 (de) 1994-08-04
ATE108011T1 (de) 1994-07-15
HUT56923A (en) 1991-10-28
RU2002165C1 (ru) 1993-10-30
HU903493D0 (en) 1990-10-28
EP0401529A1 (de) 1990-12-12

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