ES2123293T3 - Camara de combustion de turbina de gas para combustible dual. - Google Patents

Camara de combustion de turbina de gas para combustible dual.

Info

Publication number
ES2123293T3
ES2123293T3 ES95938173T ES95938173T ES2123293T3 ES 2123293 T3 ES2123293 T3 ES 2123293T3 ES 95938173 T ES95938173 T ES 95938173T ES 95938173 T ES95938173 T ES 95938173T ES 2123293 T3 ES2123293 T3 ES 2123293T3
Authority
ES
Spain
Prior art keywords
fuel
combustion chamber
liquid
gaseous fuel
spray
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
ES95938173T
Other languages
English (en)
Inventor
David T Foss
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 ES2123293T3 publication Critical patent/ES2123293T3/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
    • 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
    • F23R3/28—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
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles For Spraying Of Liquid Fuel (AREA)

Abstract

UNA CAMARA DE COMBUSTION (4) PARA UNA TURBINA DE GAS QUE TIENE UNAS ZONAS DE COMBUSTION PRIMARIA (36) Y SECUNDARIA (37). LA CAMARA DE COMBUSTION TIENE UNA BOQUILLA DE COMBUSTIBLE DUAL COLOCADA EN EL CENTRO (18) QUE PUEDE SUMINISTRAR UNA MEZCLA RICA EN COMBUSTIBLE DE COMBUSTIBLE LIQUIDO O GASEOSO A LA ZONA DE COMBUSTION PRIMARIA. LA CAMARA DE COMBUSTION TIENE TAMBIEN UNAS CLAVIJAS DE PULVERIZACION DE COMBUSTIBLE DE GAS PRIMARIO (62) PARA SUMINISTRAR UNA MEZCLA POBRE DE COMBUSTIBLE GASEOSO A LA ZONA DE COMBUSTION PRIMARIA POR UN PASO DE PREMEZCLADO ANULAR (90, 92) Y UNA BARRAS DE PULVERIZACION DE COMBUSTIBLE DUAL SECUNDARIO (76) PARA SUMINISTRAR UNA MEZCLA POBRE DE COMBUSTIBLE LIQUIDO O GASEOSO A LA ZONA DE COMBUSTION SEGUNDA (37) POR UN PASO DE PREMEZCLADO ANULAR SEGUNDO (68). LAS BARRAS DE PULVERIZACION DE COMBUSTIBLE DUAL (67) ESTAN CONFORMADAS DE FORMA AERODINAMICA Y TIENEN UNOS PASOS (95, 96) PARA DISTRIBUIR UN COMBUSTIBLE LIQUIDO Y GASEOSO A UN NUMERO DE PUERTOS DE DESCARGA DE COMBUSTIBLE. LOS PUERTOS DE DESCARGA DE COMBUSTIBLE GASEOSO (78) ESTAN FORMADOS EN FILAS EN CADA CARA DE LA BARRA DE PULVERIZACION. LOS PUERTOS DE DESCARGA DEL COMBUSTIBLE LIQUIDO (84) ESTAN FORMADOS POR UNA FILA DE BOQUILLAS DE PULVERIZACION COLOCADAS A LO LARGO DEL BORDE INFERIOR DE LA BARRA DE PULVERIZACION.
ES95938173T 1994-11-10 1995-10-18 Camara de combustion de turbina de gas para combustible dual. Expired - Lifetime ES2123293T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/336,892 US5657632A (en) 1994-11-10 1994-11-10 Dual fuel gas turbine combustor

Publications (1)

Publication Number Publication Date
ES2123293T3 true ES2123293T3 (es) 1999-01-01

Family

ID=23318142

Family Applications (1)

Application Number Title Priority Date Filing Date
ES95938173T Expired - Lifetime ES2123293T3 (es) 1994-11-10 1995-10-18 Camara de combustion de turbina de gas para combustible dual.

Country Status (10)

Country Link
US (1) US5657632A (es)
EP (1) EP0791160B1 (es)
JP (1) JPH10508936A (es)
KR (1) KR970707418A (es)
AR (1) AR000095A1 (es)
CA (1) CA2205044A1 (es)
DE (1) DE69505006T2 (es)
ES (1) ES2123293T3 (es)
TW (1) TW339390B (es)
WO (1) WO1996015409A1 (es)

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US6363724B1 (en) 2000-08-31 2002-04-02 General Electric Company Gas only nozzle fuel tip
JP2002349854A (ja) * 2001-05-30 2002-12-04 Mitsubishi Heavy Ind Ltd ガスタービン燃焼器のパイロットノズルおよび供給路変換器
US7603841B2 (en) * 2001-07-23 2009-10-20 Ramgen Power Systems, Llc Vortex combustor for low NOx emissions when burning lean premixed high hydrogen content fuel
US7003961B2 (en) * 2001-07-23 2006-02-28 Ramgen Power Systems, Inc. Trapped vortex combustor
US6694743B2 (en) 2001-07-23 2004-02-24 Ramgen Power Systems, Inc. Rotary ramjet engine with flameholder extending to running clearance at engine casing interior wall
US6640548B2 (en) 2001-09-26 2003-11-04 Siemens Westinghouse Power Corporation Apparatus and method for combusting low quality fuel
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US6691515B2 (en) 2002-03-12 2004-02-17 Rolls-Royce Corporation Dry low combustion system with means for eliminating combustion noise
US6931862B2 (en) * 2003-04-30 2005-08-23 Hamilton Sundstrand Corporation Combustor system for an expendable gas turbine engine
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JP2005309847A (ja) * 2004-04-22 2005-11-04 Sharp Corp データ処理装置
US7464555B2 (en) * 2005-05-05 2008-12-16 Siemens Energy, Inc. Catalytic combustor for integrated gasification combined cycle power plant
US7854120B2 (en) * 2006-03-03 2010-12-21 Pratt & Whitney Canada Corp. Fuel manifold with reduced losses
CA2984063C (en) * 2007-04-23 2024-01-02 New Power Concepts Llc Stirling cycle machine
JP4764392B2 (ja) * 2007-08-29 2011-08-31 三菱重工業株式会社 ガスタービン燃焼器
US8387398B2 (en) * 2007-09-14 2013-03-05 Siemens Energy, Inc. Apparatus and method for controlling the secondary injection of fuel
US7665309B2 (en) 2007-09-14 2010-02-23 Siemens Energy, Inc. Secondary fuel delivery system
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US8176739B2 (en) * 2008-07-17 2012-05-15 General Electric Company Coanda injection system for axially staged low emission combustors
US8661779B2 (en) * 2008-09-26 2014-03-04 Siemens Energy, Inc. Flex-fuel injector for gas turbines
KR100969857B1 (ko) * 2008-11-21 2010-07-13 한국생산기술연구원 연료 연소장치
US20100180599A1 (en) * 2009-01-21 2010-07-22 Thomas Stephen R Insertable Pre-Drilled Swirl Vane for Premixing Fuel Nozzle
US9140454B2 (en) * 2009-01-23 2015-09-22 General Electric Company Bundled multi-tube nozzle for a turbomachine
US8539773B2 (en) * 2009-02-04 2013-09-24 General Electric Company Premixed direct injection nozzle for highly reactive fuels
JP4797079B2 (ja) * 2009-03-13 2011-10-19 川崎重工業株式会社 ガスタービン燃焼器
EP2270398A1 (de) * 2009-06-30 2011-01-05 Siemens Aktiengesellschaft Brenner, insbesondere für Gasturbinen
US8365536B2 (en) * 2009-09-21 2013-02-05 General Electric Company Dual fuel combustor nozzle for a turbomachine
US8613187B2 (en) * 2009-10-23 2013-12-24 General Electric Company Fuel flexible combustor systems and methods
DE102009045950A1 (de) * 2009-10-23 2011-04-28 Man Diesel & Turbo Se Drallerzeuger
US9371989B2 (en) * 2011-05-18 2016-06-21 General Electric Company Combustor nozzle and method for supplying fuel to a combustor
US8601820B2 (en) 2011-06-06 2013-12-10 General Electric Company Integrated late lean injection on a combustion liner and late lean injection sleeve assembly
US9010120B2 (en) 2011-08-05 2015-04-21 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US8919137B2 (en) 2011-08-05 2014-12-30 General Electric Company Assemblies and apparatus related to integrating late lean injection into combustion turbine engines
US20130036743A1 (en) * 2011-08-08 2013-02-14 General Electric Company Turbomachine combustor assembly
US9163841B2 (en) * 2011-09-23 2015-10-20 Siemens Aktiengesellschaft Cast manifold for dry low NOx gas turbine engine
US9140455B2 (en) 2012-01-04 2015-09-22 General Electric Company Flowsleeve of a turbomachine component
US9267690B2 (en) 2012-05-29 2016-02-23 General Electric Company Turbomachine combustor nozzle including a monolithic nozzle component and method of forming the same
CN103486617B (zh) * 2012-06-13 2015-10-14 中国航空工业集团公司沈阳发动机设计研究所 一种用于燃气轮机的双燃料低排放燃烧器
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JP2017524094A (ja) 2014-07-02 2017-08-24 ヌオーヴォ ピニォーネ ソチエタ レスポンサビリタ リミタータＮｕｏｖｏ Ｐｉｇｎｏｎｅ Ｓ．Ｒ．Ｌ． 燃料分配装置、ガスタービンエンジン、および取り付け方法
CN107076411B (zh) * 2014-10-23 2020-06-23 西门子公司 用于涡轮发动机的灵活燃料燃烧系统
US10274201B2 (en) * 2016-01-05 2019-04-30 Solar Turbines Incorporated Fuel injector with dual main fuel injection
EP3403028B1 (en) * 2016-01-15 2021-02-24 Siemens Energy Global GmbH & Co. KG Combustor for a gas turbine
JP6754595B2 (ja) * 2016-03-30 2020-09-16 三菱日立パワーシステムズ株式会社 ガスタービン
US10502425B2 (en) * 2016-06-03 2019-12-10 General Electric Company Contoured shroud swirling pre-mix fuel injector assembly
US10578306B2 (en) 2017-06-16 2020-03-03 General Electric Company Liquid fuel cartridge unit for gas turbine combustor and method of assembly
US10634358B2 (en) 2017-06-16 2020-04-28 General Electric Company System and method for igniting liquid fuel in a gas turbine combustor
US10982593B2 (en) 2017-06-16 2021-04-20 General Electric Company System and method for combusting liquid fuel in a gas turbine combustor with staged combustion
US10655858B2 (en) 2017-06-16 2020-05-19 General Electric Company Cooling of liquid fuel cartridge in gas turbine combustor head end
RU2665009C1 (ru) * 2017-11-22 2018-08-24 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Двухконтурная горелка
US11286884B2 (en) 2018-12-12 2022-03-29 General Electric Company Combustion section and fuel injector assembly for a heat engine
US11073114B2 (en) 2018-12-12 2021-07-27 General Electric Company Fuel injector assembly for a heat engine
US11725818B2 (en) * 2019-12-06 2023-08-15 Raytheon Technologies Corporation Bluff-body piloted high-shear injector and method of using same
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Also Published As

Publication number Publication date
JPH10508936A (ja) 1998-09-02
AR000095A1 (es) 1997-05-21
WO1996015409A1 (en) 1996-05-23
DE69505006T2 (de) 1999-04-22
US5657632A (en) 1997-08-19
DE69505006D1 (de) 1998-10-29
CA2205044A1 (en) 1996-05-23
TW339390B (en) 1998-09-01
EP0791160A1 (en) 1997-08-27
EP0791160B1 (en) 1998-09-23
KR970707418A (ko) 1997-12-01

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