ES2108938T3 - Camara de combustion de premezclado con conductos anulares concentricos. - Google Patents

Camara de combustion de premezclado con conductos anulares concentricos.

Info

Publication number
ES2108938T3
ES2108938T3 ES94302602T ES94302602T ES2108938T3 ES 2108938 T3 ES2108938 T3 ES 2108938T3 ES 94302602 T ES94302602 T ES 94302602T ES 94302602 T ES94302602 T ES 94302602T ES 2108938 T3 ES2108938 T3 ES 2108938T3
Authority
ES
Spain
Prior art keywords
fuel
passages
ring
air
combustion chamber
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
ES94302602T
Other languages
English (en)
Inventor
Anthony Mcwhirter
Eugenio Colautti
David Joseph Amos
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.)
CBS Corp
Original Assignee
Westinghouse Electric Corp
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 Westinghouse Electric Corp filed Critical Westinghouse Electric Corp
Application granted granted Critical
Publication of ES2108938T3 publication Critical patent/ES2108938T3/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
    • F23R3/34—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
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D14/00—Burners for combustion of a gas, e.g. of a gas stored under pressure as a liquid
    • F23D14/02—Premix gas burners, i.e. in which gaseous fuel is mixed with combustion air upstream of the combustion zone
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D23/00—Assemblies of two or more burners
    • 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
    • F23R3/28—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
    • 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
    • F23R3/346—Feeding into different combustion zones for staged combustion
    • 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
    • F23R3/40—Continuous combustion chambers using liquid or gaseous fuel characterised by the use of catalytic means
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2209/00—Safety arrangements
    • F23D2209/20—Flame lift-off / stability
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00008—Burner assemblies with diffusion and premix modes, i.e. dual mode burners
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2900/00—Special features of, or arrangements for burners using fluid fuels or solid fuels suspended in a carrier gas
    • F23D2900/00014—Pilot burners specially adapted for ignition of main burners in furnaces or gas turbines
    • 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
    • F23R2900/00—Special features of, or arrangements for continuous combustion chambers; Combustion processes therefor
    • F23R2900/00002—Gas turbine combustors adapted for fuels having low heating value [LHV]
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Chemical Kinetics & Catalysis (AREA)
  • Toys (AREA)

Abstract

UN SISTEMA DE COMBUSTION DE TURBINA DE GAS (6) QUE TIENE UNA ZONA DE PREMEZCLADO (109 Y UNA ZONA DE COMBUSTION (12) SEPARADAS POR UNA BARRERA DE PLATO (57). UN NUMERO DE PASAJES ANULARES DISPUESTOS CONCENTRICAMENTE, EN LOS CUALES SE INTRODUCEN MEZCLAS POBRES DE AIRE Y COMBUSTIBLE, SE COLOCAN EN LA ZONA DE PREMEZCLADO (10). CADA UNO DE LOS PASAJES ANULARES (23-26) TIENE UN EXTREMO DE DESCARGA (35) EN EL QUE UN NUMERO DE GIRADORES (59) ESTAN DISPUESTOS CIRCUNFERENCIALMENTE PARA PERMITIR QUE LAS MEZCLAS DE AIRE/COMBUSTIBLE FLUYAN A TRAVES DE LOS PASAJES ANULARES (23-26) PARA ENTRAR EN LA ZONA DE COMBUSTION (12), ACTUANDO LOS GIRADORES (59) COMO PORTALLAMAS. UNA ADMISION TOROIDAL DE COMBUSTIBLE (70-73) CORRIENTE ARRIBA DE CADA UNO DE LOS PASAJES ANULARES (23-26) PERMITE QUE SEA CONTROLADO INDIVIDUALMENTE EL INDICE AIRE/COMBUSTIBLE EN CADA UN DE LOS PASAJES ANULARES (23-26). LA TEMPERATURA DE IGNICION DEL SISTEMA DE COMBUSTION (6)SE AUMENTA PROPORCINANDO COMBUSTIBLE SECUENCIALMENTE A CADA PASAJEANULAR (23-26) EN TURNO, SIENDO LOS PASAJES ANULARES MAS AL INTERIOR (23) LOS PRIMEROS EN SER PROVISTOS DE COMBUSTIBLE. UN ENSAMBLAJE PILOTO DE COMBUSTIBLE ESTA DISPUESTO CENTRALMENTE CON RESPECTO A LOS PASAJES ANULARES Y TIENE ASPAS GIRATORIAS Y UN ENCENDEDOR.
ES94302602T 1993-04-15 1994-04-13 Camara de combustion de premezclado con conductos anulares concentricos. Expired - Lifetime ES2108938T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/046,320 US5361586A (en) 1993-04-15 1993-04-15 Gas turbine ultra low NOx combustor

Publications (1)

Publication Number Publication Date
ES2108938T3 true ES2108938T3 (es) 1998-01-01

Family

ID=21942823

Family Applications (1)

Application Number Title Priority Date Filing Date
ES94302602T Expired - Lifetime ES2108938T3 (es) 1993-04-15 1994-04-13 Camara de combustion de premezclado con conductos anulares concentricos.

Country Status (7)

Country Link
US (2) US5361586A (es)
EP (2) EP0620402B1 (es)
JP (1) JPH06323543A (es)
CA (1) CA2121314A1 (es)
DE (2) DE69425836D1 (es)
ES (1) ES2108938T3 (es)
TW (1) TW230233B (es)

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JPH06323543A (ja) 1994-11-25
US5361586A (en) 1994-11-08
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CA2121314A1 (en) 1994-10-16
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