DE69412572D1 - Hybridbrenner einer Gasturbine - Google Patents

Hybridbrenner einer Gasturbine

Info

Publication number
DE69412572D1
DE69412572D1 DE69412572T DE69412572T DE69412572D1 DE 69412572 D1 DE69412572 D1 DE 69412572D1 DE 69412572 T DE69412572 T DE 69412572T DE 69412572 T DE69412572 T DE 69412572T DE 69412572 D1 DE69412572 D1 DE 69412572D1
Authority
DE
Germany
Prior art keywords
gas turbine
hybrid burner
burner
hybrid
turbine
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 - Fee Related
Application number
DE69412572T
Other languages
English (en)
Other versions
DE69412572T2 (de
Inventor
David Thomas Foss
Diane Marie Marshall
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 DE69412572D1 publication Critical patent/DE69412572D1/de
Publication of DE69412572T2 publication Critical patent/DE69412572T2/de
Anticipated expiration legal-status Critical
Expired - Fee Related 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
    • F02C1/00—Gas-turbine plants characterised by the use of hot gases or unheated pressurised gases, as the working fluid
    • 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
    • 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
    • F23R3/34—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
    • 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
    • F23C2900/07001—Air swirling vanes incorporating fuel injectors

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
DE69412572T 1993-12-03 1994-11-28 Hybridbrenner einer Gasturbine Expired - Fee Related DE69412572T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US08/161,023 US5408825A (en) 1993-12-03 1993-12-03 Dual fuel gas turbine combustor

Publications (2)

Publication Number Publication Date
DE69412572D1 true DE69412572D1 (de) 1998-09-24
DE69412572T2 DE69412572T2 (de) 1999-04-29

Family

ID=22579478

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69412572T Expired - Fee Related DE69412572T2 (de) 1993-12-03 1994-11-28 Hybridbrenner einer Gasturbine

Country Status (6)

Country Link
US (1) US5408825A (de)
EP (1) EP0656512B1 (de)
JP (1) JPH07190372A (de)
KR (1) KR950019073A (de)
CA (1) CA2137200A1 (de)
DE (1) DE69412572T2 (de)

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DE19610930A1 (de) * 1996-03-20 1997-09-25 Abb Research Ltd Brenner für einen Wärmeerzeuger
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US5865024A (en) * 1997-01-14 1999-02-02 General Electric Company Dual fuel mixer for gas turbine combustor
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JP4581542B2 (ja) * 2004-08-02 2010-11-17 日本精工株式会社 回転支持装置
US7370466B2 (en) * 2004-11-09 2008-05-13 Siemens Power Generation, Inc. Extended flashback annulus in a gas turbine combustor
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EP2179222B2 (de) * 2007-08-07 2021-12-01 Ansaldo Energia IP UK Limited Brenner für eine brennkammer einer turbogruppe
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US20090165435A1 (en) 2008-01-02 2009-07-02 Michal Koranek Dual fuel can combustor with automatic liquid fuel purge
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JP5172468B2 (ja) * 2008-05-23 2013-03-27 川崎重工業株式会社 燃焼装置および燃焼装置の制御方法
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US9126210B1 (en) 2008-08-12 2015-09-08 Board Of Supervisors Of Louisiana State University And Agricultural And Mechanical College Efficient premixing fuel-air nozzle system
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US8677760B2 (en) * 2010-01-06 2014-03-25 General Electric Company Fuel nozzle with integrated passages and method of operation
EP2362142A1 (de) * 2010-02-19 2011-08-31 Siemens Aktiengesellschaft Brenneranordnung
US20110225973A1 (en) * 2010-03-18 2011-09-22 General Electric Company Combustor with Pre-Mixing Primary Fuel-Nozzle Assembly
US8418469B2 (en) 2010-09-27 2013-04-16 General Electric Company Fuel nozzle assembly for gas turbine system
US9010119B2 (en) 2010-11-03 2015-04-21 General Electric Company Premixing nozzle
RU2456510C1 (ru) * 2011-02-18 2012-07-20 Федеральное государственное унитарное предприятие "Центральный институт авиационного моторостроения имени П.И. Баранова" Камера сгорания непрерывного действия
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
EP2551470A1 (de) * 2011-07-26 2013-01-30 Siemens Aktiengesellschaft Verfahren zum Hochfahren einer stationären Gasturbine
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
US9140455B2 (en) 2012-01-04 2015-09-22 General Electric Company Flowsleeve of a turbomachine component
JP5618337B2 (ja) * 2012-02-28 2014-11-05 三菱日立パワーシステムズ株式会社 ガスタービン燃焼器
US9366432B2 (en) 2012-05-17 2016-06-14 Capstone Turbine Corporation Multistaged lean prevaporizing premixing fuel injector
US10378456B2 (en) * 2012-10-01 2019-08-13 Ansaldo Energia Switzerland AG Method of operating a multi-stage flamesheet combustor
US10800525B2 (en) 2013-05-20 2020-10-13 The Boeing Company Efficient low carbon emission airplane integrating jet fuel and cryogenic fuel systems
US9493246B2 (en) 2013-09-12 2016-11-15 The Boeing Company Cryogenic fuel tanks for use in aircraft structures
US10731861B2 (en) 2013-11-18 2020-08-04 Raytheon Technologies Corporation Dual fuel nozzle with concentric fuel passages for a gas turbine engine
US20150159877A1 (en) * 2013-12-06 2015-06-11 General Electric Company Late lean injection manifold mixing system
US10184664B2 (en) 2014-08-01 2019-01-22 Capstone Turbine Corporation Fuel injector for high flame speed fuel combustion
CN104315541B (zh) * 2014-09-26 2019-01-18 北京华清燃气轮机与煤气化联合循环工程技术有限公司 燃烧室值班级喷嘴及使用该喷嘴的方法
JP6664389B2 (ja) * 2014-10-23 2020-03-13 シーメンス アクチエンゲゼルシヤフトＳｉｅｍｅｎｓ Ａｋｔｉｅｎｇｅｓｅｌｌｓｃｈａｆｔ タービンエンジン用のフレキシブルな燃料燃焼システム
US9964043B2 (en) 2014-11-11 2018-05-08 General Electric Company Premixing nozzle with integral liquid evaporator
JP6799056B2 (ja) 2015-08-26 2020-12-09 ゼネラル・エレクトリック・カンパニイ 燃料ノズル組立体及び、燃料ノズル組立体を含む燃焼器を備えるガスタービンエンジン
WO2017121872A1 (en) * 2016-01-15 2017-07-20 Siemens Aktiengesellschaft Combustor for a gas turbine
US10228140B2 (en) * 2016-02-18 2019-03-12 General Electric Company Gas-only cartridge for a premix fuel nozzle
US10502425B2 (en) * 2016-06-03 2019-12-10 General Electric Company Contoured shroud swirling pre-mix fuel injector assembly
US10859264B2 (en) 2017-03-07 2020-12-08 8 Rivers Capital, Llc System and method for combustion of non-gaseous fuels and derivatives thereof
BR112019018466A2 (pt) 2017-03-07 2020-04-14 8 Rivers Capital Llc sistema e método para a operação de um combustor de combustível flexível para uma turbina de gás
US10655858B2 (en) 2017-06-16 2020-05-19 General Electric Company Cooling of liquid fuel cartridge in gas turbine combustor head end
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
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WO2020021456A1 (en) 2018-07-23 2020-01-30 8 Rivers Capital, Llc System and method for power generation with flameless combustion
US10935245B2 (en) * 2018-11-20 2021-03-02 General Electric Company Annular concentric fuel nozzle assembly with annular depression and radial inlet ports
US11149941B2 (en) * 2018-12-14 2021-10-19 Delavan Inc. Multipoint fuel injection for radial in-flow swirl premix gas fuel injectors
US11156164B2 (en) 2019-05-21 2021-10-26 General Electric Company System and method for high frequency accoustic dampers with caps
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US11326521B2 (en) 2020-06-30 2022-05-10 General Electric Company Methods of igniting liquid fuel in a turbomachine
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Also Published As

Publication number Publication date
EP0656512A1 (de) 1995-06-07
CA2137200A1 (en) 1995-06-04
JPH07190372A (ja) 1995-07-28
DE69412572T2 (de) 1999-04-29
KR950019073A (ko) 1995-07-22
US5408825A (en) 1995-04-25
EP0656512B1 (de) 1998-08-19

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee