ES2123842T3 - Sistema perfeccionado de combustion para turbinas de gas con bajas emisiones de contaminantes. - Google Patents

Sistema perfeccionado de combustion para turbinas de gas con bajas emisiones de contaminantes.

Info

Publication number
ES2123842T3
ES2123842T3 ES95101731T ES95101731T ES2123842T3 ES 2123842 T3 ES2123842 T3 ES 2123842T3 ES 95101731 T ES95101731 T ES 95101731T ES 95101731 T ES95101731 T ES 95101731T ES 2123842 T3 ES2123842 T3 ES 2123842T3
Authority
ES
Spain
Prior art keywords
combustion
burners
combustion system
perfected
pollutants
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
ES95101731T
Other languages
English (en)
Inventor
Luciano Bonciani
Gianni Ceccherini
Roberto Modi
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.)
Nuovo Pignone Holding SpA
Nuovo Pignone SpA
Original Assignee
Nuovopignone Industrie Meccaniche e Fonderia SpA
Nuovo Pignone SpA
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 Nuovopignone Industrie Meccaniche e Fonderia SpA, Nuovo Pignone SpA filed Critical Nuovopignone Industrie Meccaniche e Fonderia SpA
Application granted granted Critical
Publication of ES2123842T3 publication Critical patent/ES2123842T3/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
    • 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
    • F23R3/28—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
    • 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
    • F23R3/36—Supply of different fuels
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2214/00—Cooling

Abstract

SISTEMA DE COMBUSTION CON BAJAS EMISIONES CONTAMINANTES PARA TURBINA DE GAS, DEL TIPO PREMEZCLADO, DONDE UNA SERIE DE QUEMADORES PARALELOS (24), AUTONOMAMENTE ALIMENTADOS CON COMBUSTIBLE ADICIONAL, ESTA CIRCUNFERENCIALMENTE DISPUESTO ALREDEDOR DEL DIFUSOR DE CONJUNCION (3) DE LA CAMARA DE PREMEZCLA CON LA CAMARA DE COMBUSTION, PARA CREAR EN LA ZONA DE COMBUSTION INMEDIATAMENTE ANTERIOR AL DIFUSOR UNA SERIE CORRESPONDIENTE DE LLAMAS ADICIONALES PARA LA ESTABILIZACION DE LA LLAMA PRINCIPAL, EL AIRE DE COMBUSTION PARA DICHOS QUEMADORES QUE SE DERIVA DESDE EL AIRE DE REFRIGERACION (10) DE LA CABEZA CONICA DE DICHA CAMARA DE COMBUSTION, QUE ES ENVIADO A LOS QUEMADORES A TRAVES DE CUCHILLAS GIRADAS PARA OFRECER UN MOVIMIENTO SUSTANCIALMENTE HELICOIDAL AL AIRE.
ES95101731T 1994-03-04 1995-02-09 Sistema perfeccionado de combustion para turbinas de gas con bajas emisiones de contaminantes. Expired - Lifetime ES2123842T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ITMI940386A IT1273369B (it) 1994-03-04 1994-03-04 Sistema perfezionato combustione a basse emissioni inquinanti per turbine a gas

Publications (1)

Publication Number Publication Date
ES2123842T3 true ES2123842T3 (es) 1999-01-16

Family

ID=11368055

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95101731T Expired - Lifetime ES2123842T3 (es) 1994-03-04 1995-02-09 Sistema perfeccionado de combustion para turbinas de gas con bajas emisiones de contaminantes.

Country Status (7)

Country Link
US (1) US5660044A (es)
EP (1) EP0670456B1 (es)
JP (1) JP3696645B2 (es)
AT (1) ATE173809T1 (es)
DE (1) DE69506142T2 (es)
ES (1) ES2123842T3 (es)
IT (1) IT1273369B (es)

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EP0918190A1 (de) * 1997-11-21 1999-05-26 Abb Research Ltd. Brenner für den Betrieb eines Wärmeerzeugers
DE59807856D1 (de) 1998-01-23 2003-05-15 Alstom Switzerland Ltd Brenner für den Betrieb eines Wärmeerzeugers
EP0987493B1 (de) * 1998-09-16 2003-08-06 Abb Research Ltd. Brenner für einen Wärmeerzeuger
US6279323B1 (en) * 1999-11-01 2001-08-28 General Electric Company Low emissions combustor
ITMI20012781A1 (it) * 2001-12-21 2003-06-21 Nuovo Pignone Spa Assieme migliorato di camera di pre miscelamento e di camera di combustione, a basse emissioni inquinanti per turbine a gas con combustibile
US7093445B2 (en) * 2002-05-31 2006-08-22 Catalytica Energy Systems, Inc. Fuel-air premixing system for a catalytic combustor
GB2390150A (en) * 2002-06-26 2003-12-31 Alstom Reheat combustion system for a gas turbine including an accoustic screen
ITMI20032621A1 (it) * 2003-12-30 2005-06-30 Nuovo Pignone Spa Sistema di combustione a basse emissioni inquinanti
US8881531B2 (en) * 2005-12-14 2014-11-11 Rolls-Royce Power Engineering Plc Gas turbine engine premix injectors
TWI375053B (en) * 2006-02-28 2012-10-21 Nippon Catalytic Chem Ind Phase difference film
US20070204624A1 (en) * 2006-03-01 2007-09-06 Smith Kenneth O Fuel injector for a turbine engine
EP1999410B1 (de) 2006-03-27 2015-12-02 Alstom Technology Ltd Brenner für den betrieb eines wärmeerzeugers
US8156743B2 (en) * 2006-05-04 2012-04-17 General Electric Company Method and arrangement for expanding a primary and secondary flame in a combustor
US8387394B2 (en) 2007-07-09 2013-03-05 Siemens Aktiengesellschaft Gas-turbine burner
KR100862374B1 (ko) 2007-11-13 2008-10-13 한국기계연구원 과열방지 가스터빈 시스템
KR100890823B1 (ko) 2007-11-13 2009-03-30 한국기계연구원 가스터빈 시스템
US8122700B2 (en) * 2008-04-28 2012-02-28 United Technologies Corp. Premix nozzles and gas turbine engine systems involving such nozzles
US7578130B1 (en) * 2008-05-20 2009-08-25 General Electric Company Methods and systems for combustion dynamics reduction
US8371101B2 (en) * 2009-09-15 2013-02-12 General Electric Company Radial inlet guide vanes for a combustor
GB0920094D0 (en) 2009-11-17 2009-12-30 Alstom Technology Ltd Reheat combustor for a gas turbine engine
CN101709884B (zh) * 2009-11-25 2012-07-04 北京航空航天大学 一种预混预蒸发燃烧室
CN101799174B (zh) * 2010-01-15 2012-09-12 北京航空航天大学 主燃级切向供油的预混预蒸发燃烧室
US8739404B2 (en) 2010-11-23 2014-06-03 General Electric Company Turbine components with cooling features and methods of manufacturing the same
CN102878580B (zh) * 2012-09-12 2015-04-22 中国科学院工程热物理研究所 一种燃气轮机贫预混燃烧室
CN102889617B (zh) * 2012-09-12 2014-10-15 北京航空航天大学 一种采用径向成膜主燃级的预混预蒸发燃烧室
JP6318443B2 (ja) * 2013-01-22 2018-05-09 三菱日立パワーシステムズ株式会社 燃焼器、及び回転機械
CN103185355B (zh) * 2013-02-28 2015-07-15 北京航空航天大学 一种多点轴向双级空气辅助雾化喷嘴主燃级的预混预蒸发低污染燃烧室
EP3084307B1 (en) 2013-12-19 2018-10-24 United Technologies Corporation Dilution passage arrangement for gas turbine engine combustor
EP3026347A1 (en) * 2014-11-25 2016-06-01 Alstom Technology Ltd Combustor with annular bluff body
RU2015156419A (ru) 2015-12-28 2017-07-04 Дженерал Электрик Компани Узел топливной форсунки, выполненный со стабилизатором пламени предварительно перемешанной смеси

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Also Published As

Publication number Publication date
DE69506142D1 (de) 1999-01-07
ITMI940386A0 (it) 1994-03-04
EP0670456B1 (en) 1998-11-25
IT1273369B (it) 1997-07-08
DE69506142T2 (de) 1999-06-17
US5660044A (en) 1997-08-26
JPH07305846A (ja) 1995-11-21
EP0670456A1 (en) 1995-09-06
JP3696645B2 (ja) 2005-09-21
ATE173809T1 (de) 1998-12-15
ITMI940386A1 (it) 1995-09-05

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