ES2037217T3 - Sistema de control de combustible en turbinas de gases. - Google Patents

Sistema de control de combustible en turbinas de gases.

Info

Publication number
ES2037217T3
ES2037217T3 ES198888302809T ES88302809T ES2037217T3 ES 2037217 T3 ES2037217 T3 ES 2037217T3 ES 198888302809 T ES198888302809 T ES 198888302809T ES 88302809 T ES88302809 T ES 88302809T ES 2037217 T3 ES2037217 T3 ES 2037217T3
Authority
ES
Spain
Prior art keywords
fuel
filter
control system
main combustion
fuel control
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
ES198888302809T
Other languages
English (en)
Inventor
Barry Donald Miles
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.)
Rolls Royce PLC
Original Assignee
Rolls Royce PLC
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 Rolls Royce PLC filed Critical Rolls Royce PLC
Application granted granted Critical
Publication of ES2037217T3 publication Critical patent/ES2037217T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/22—Fuel supply systems
    • F02C7/228—Dividing fuel between various burners
    • 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
    • F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
    • F02C9/26—Control of fuel supply
    • F02C9/32—Control of fuel supply characterised by throttling of fuel
    • F02C9/34—Joint control of separate flows to main and auxiliary burners

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feeding And Controlling Fuel (AREA)
  • Processes For Solid Components From Exhaust (AREA)
  • Output Control And Ontrol Of Special Type Engine (AREA)

Abstract

SISTEMA DE COMBUSTIBLE PARA UN MOTOR DE TURBINA DE GAS EN LA QUE SE ENCUENTRA DISPUESTO UN FILTRO 20 CON SU SALIDA CONECTADA AL SISTEMA DE CONTROL DE COMBUSTIBLE 24 QUE CONTROLA EL FLUJO DE COMBUSTIBLE A LAS CAMARAS DE COMBUSTION PRINCIPALES 26 DEL MOTOR. UN CONDUCTO DE DERIVACION 25, QUE TIENE UNA VALVULA DE DESCARGA DE PRESION 29, DERIVA EL FILTRO 20 Y SE CONECTA A LA ENTRADA DE UN SISTEMA DE CONTROL DE COMBUSTIBLE 23 QUE CONTROLA EL FLUJO DE COMBUSTIBLE A LOS QUEMADORES DE RECALENTAMIENTO 28 DEL MOTOR. UN CONDUCTO DE CONEXION CONECTA LA SALIDA DEL FILTRO AL SISTEMA DE CONTROL DE COMBUSTIBLE DE RECALENTAMIENTO. EN LA OPERACION NORMAL, EL COMBUSTIBLE FILTRADO SE SUMINISTRA A LOS DOS SISTEMAS DE CONTROL DE COMBUSTIBLE 24, 27 Y NO HAY FLUJO EN EL CONDUCTO DE DERIVACION DEL FILTRO 25. COMO EL FILTRO 20 SE OBSTRUYE PROGRESIVAMENTE, EL COMBUSTIBLE FILTRADO SE SUMINISTRA A LA CAMARA DE COMBUSTION PRINCIPAL 26 INDEPENDIENTEMENTE DE SI SE REQUIERE O NO EL RECALENTAMIENTO. CUANDO SE SELECCIONA ELRECALENTAMIENTO, Y EL FILTRO 20 ESTA DEMASIADO OBSTRUIDO PARA CUBRIR LA DEMANDA DE FLUJO, LA VALVULA DE DESAHOGO 29 SE ABRE PARA SUMINISTRAR COMBUSTIBLE SIN FILTRAR A LOS QUEMADORES DE RECALENTAMIENTO. EN EL CASO INDESEABLE DE QUE EL FILTRO 20 SE OBSTRUYA TANTO QUE SE VUELVA INCAPAZ DE SUMINISTRAR COMBUSTIBLE FILTRADO A LA CAMARA DE COMBUSTION PRINCIPAL 236, ENTONCES SE SUMINISTRARA COMBUSTIBLE SIN FILTRAR A LA CAMARA DE COMBUSTION PRINCIPAL A TRAVES DEL CONDUCTO DE CONEXION 30.
ES198888302809T 1987-04-10 1988-03-30 Sistema de control de combustible en turbinas de gases. Expired - Lifetime ES2037217T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB878708595A GB8708595D0 (en) 1987-04-10 1987-04-10 Gas turbine fuel control system

Publications (1)

Publication Number Publication Date
ES2037217T3 true ES2037217T3 (es) 1993-06-16

Family

ID=10615598

Family Applications (1)

Application Number Title Priority Date Filing Date
ES198888302809T Expired - Lifetime ES2037217T3 (es) 1987-04-10 1988-03-30 Sistema de control de combustible en turbinas de gases.

Country Status (6)

Country Link
US (1) US4827714A (es)
EP (1) EP0286299B1 (es)
JP (1) JPS63263227A (es)
DE (1) DE3877608T2 (es)
ES (1) ES2037217T3 (es)
GB (1) GB8708595D0 (es)

Families Citing this family (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4932205A (en) * 1989-02-27 1990-06-12 Allied-Signal Inc. Bypass valve and visual indicator for a fuel system
GB2282186B (en) * 1993-09-08 1997-09-24 Rolls Royce Plc Engine fuel metering system
US7185485B2 (en) * 2003-05-29 2007-03-06 Honeywell International Inc. Method and system for failure accommodation of gas generator fuel metering system
GB0408886D0 (en) * 2004-04-22 2004-05-26 Rolls Royce Plc Fuel metering unit
CN101111715A (zh) * 2005-01-31 2008-01-23 普罗米修西（私人）有限公司 燃烧器具
US20090301054A1 (en) * 2008-06-04 2009-12-10 Simpson Stanley F Turbine system having exhaust gas recirculation and reheat
US9297306B2 (en) * 2008-09-11 2016-03-29 General Electric Company Exhaust gas recirculation system, turbomachine system having the exhaust gas recirculation system and exhaust gas recirculation control method
US8381530B2 (en) * 2009-04-28 2013-02-26 General Electric Company System and method for controlling combustion dynamics
US10378443B2 (en) * 2017-02-02 2019-08-13 United Technologies Corporation Bypass valve system state indication

Family Cites Families (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB733529A (en) * 1952-07-24 1955-07-13 Gen Motors Corp Improvements in gas turbine engine fuel supply systems incorporating fuel flow control devices
GB787795A (en) * 1955-05-26 1957-12-18 Gen Motors Corp Improvements in gas turbine fuel systems
US3360199A (en) * 1965-05-04 1967-12-26 Gen Motors Corp Fuel nozzle fuel proportioning system utilizing a fuel pressure responsive valve
GB1110249A (en) * 1967-01-27 1968-04-18 Rolls Royce Filter device
US3658249A (en) * 1970-10-21 1972-04-25 Gen Motors Corp Apparatus and method for burning contaminated fuel
GB1555736A (en) * 1977-03-31 1979-11-14 Rolls Royce Fuel system for gas turbine engieens
GB8329218D0 (en) * 1983-11-02 1983-12-07 Ffowcs Williams J E Reheat combustion system for gas turbine engine

Also Published As

Publication number Publication date
JPS63263227A (ja) 1988-10-31
DE3877608T2 (de) 1993-06-03
EP0286299A2 (en) 1988-10-12
DE3877608D1 (de) 1993-03-04
EP0286299B1 (en) 1993-01-20
EP0286299A3 (en) 1989-12-27
US4827714A (en) 1989-05-09
GB8708595D0 (en) 1987-05-13

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