DE69525920T2 - Brennstoffeinspritzeinrictung für mit gasförmigem oder flüssigem Brennstoff betriebene Turbine - Google Patents

Brennstoffeinspritzeinrictung für mit gasförmigem oder flüssigem Brennstoff betriebene Turbine

Info

Publication number
DE69525920T2
DE69525920T2 DE69525920T DE69525920T DE69525920T2 DE 69525920 T2 DE69525920 T2 DE 69525920T2 DE 69525920 T DE69525920 T DE 69525920T DE 69525920 T DE69525920 T DE 69525920T DE 69525920 T2 DE69525920 T2 DE 69525920T2
Authority
DE
Germany
Prior art keywords
gaseous
injection device
fuel
turbine operated
fuel injection
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
DE69525920T
Other languages
English (en)
Other versions
DE69525920D1 (de
Inventor
Eric Roy Norster
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.)
Siemens AG
Original Assignee
Alstom Power UK Holdings Ltd
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 Alstom Power UK Holdings Ltd filed Critical Alstom Power UK Holdings Ltd
Application granted granted Critical
Publication of DE69525920D1 publication Critical patent/DE69525920D1/de
Publication of DE69525920T2 publication Critical patent/DE69525920T2/de
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
    • F23R3/286—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
    • F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN  A CARRIER GAS OR AIR 
    • F23C7/00—Combustion apparatus characterised by arrangements for air supply
    • F23C7/002—Combustion apparatus characterised by arrangements for air supply the air being submitted to a rotary or spinning motion
    • 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
    • F23D14/20—Non-premix gas burners, i.e. in which gaseous fuel is mixed with combustion air on arrival at the combustion zone
    • 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
    • F23D14/46—Details, e.g. noise reduction means
    • F23D14/72—Safety devices, e.g. operative in case of failure of gas supply
    • F23D14/74—Preventing flame lift-off
    • 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
    • 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 
    • F23C2202/00—Fluegas recirculation
    • F23C2202/40—Inducing local whirls around flame
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2204/00—Burners adapted for simultaneous or alternative combustion having more than one fuel supply
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2206/00—Burners for specific applications
    • F23D2206/10—Turbines
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
    • F23D—BURNERS
    • F23D2207/00—Ignition devices associated with burner
    • 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
    • F23D2900/00016—Preventing or reducing deposit build-up on burner parts, e.g. from carbon

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Spray-Type Burners (AREA)
DE69525920T 1995-01-13 1995-12-06 Brennstoffeinspritzeinrictung für mit gasförmigem oder flüssigem Brennstoff betriebene Turbine Expired - Lifetime DE69525920T2 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9500627A GB2297151B (en) 1995-01-13 1995-01-13 Fuel injector arrangement for gas-or liquid-fuelled turbine

Publications (2)

Publication Number Publication Date
DE69525920D1 DE69525920D1 (de) 2002-04-25
DE69525920T2 true DE69525920T2 (de) 2002-09-19

Family

ID=10767960

Family Applications (1)

Application Number Title Priority Date Filing Date
DE69525920T Expired - Lifetime DE69525920T2 (de) 1995-01-13 1995-12-06 Brennstoffeinspritzeinrictung für mit gasförmigem oder flüssigem Brennstoff betriebene Turbine

Country Status (5)

Country Link
US (1) US5761906A (de)
EP (1) EP0722065B1 (de)
JP (1) JP3863210B2 (de)
DE (1) DE69525920T2 (de)
GB (1) GB2297151B (de)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017114362A1 (de) * 2017-06-28 2019-01-03 Man Diesel & Turbo Se Brennkammer einer Gasturbine, Gasturbine und Verfahren zum Betreiben derselben

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US6354072B1 (en) 1999-12-10 2002-03-12 General Electric Company Methods and apparatus for decreasing combustor emissions
US6374615B1 (en) 2000-01-28 2002-04-23 Alliedsignal, Inc Low cost, low emissions natural gas combustor
GB2368386A (en) * 2000-10-23 2002-05-01 Alstom Power Nv Gas turbine engine combustion system
US6669115B2 (en) * 2002-02-07 2003-12-30 Tai-Yen Sun Vortex twin-fluid nozzle with self-cleaning pintle
US6935116B2 (en) * 2003-04-28 2005-08-30 Power Systems Mfg., Llc Flamesheet combustor
JP3940705B2 (ja) * 2003-06-19 2007-07-04 株式会社日立製作所 ガスタービン燃焼器及びその燃料供給方法
JP4626251B2 (ja) * 2004-10-06 2011-02-02 株式会社日立製作所 燃焼器及び燃焼器の燃焼方法
CN100504175C (zh) * 2006-04-13 2009-06-24 中国科学院工程热物理研究所 燃气轮机低热值燃烧室喷嘴结构与燃烧方法
DE102006042124B4 (de) * 2006-09-07 2010-04-22 Man Turbo Ag Gasturbinenbrennkammer
US8096132B2 (en) * 2008-02-20 2012-01-17 Flexenergy Energy Systems, Inc. Air-cooled swirlerhead
EP2107306A1 (de) * 2008-03-31 2009-10-07 Siemens Aktiengesellschaft Verbrennergehäuse
EP2169312A1 (de) 2008-09-25 2010-03-31 Siemens Aktiengesellschaft Abgestufter Wirbler zur dynamischen Steuerung
ATE540265T1 (de) * 2009-04-06 2012-01-15 Siemens Ag Drallvorrichtung, brennkammer und gasturbine mit verbessertem drall
EP2246617B1 (de) * 2009-04-29 2017-04-19 Siemens Aktiengesellschaft Brenner für Gasturbinenmotor
US20110091829A1 (en) * 2009-10-20 2011-04-21 Vinayak Barve Multi-fuel combustion system
JP4894947B2 (ja) * 2010-09-21 2012-03-14 株式会社日立製作所 燃焼器及び燃焼器の燃焼方法
EP2489939A1 (de) * 2011-02-18 2012-08-22 Siemens Aktiengesellschaft Brennkammer mit einem Wandabschnitt und einem Randelement
US9134031B2 (en) 2012-01-04 2015-09-15 General Electric Company Combustor of a turbomachine including multiple tubular radial pathways arranged at multiple circumferential and axial locations
EP2629008A1 (de) 2012-02-15 2013-08-21 Siemens Aktiengesellschaft Abgeneigte Brennstoffeinspritzung von Brennstoff in einen Wirbelschlitz
US10288291B2 (en) 2014-08-15 2019-05-14 General Electric Company Air-shielded fuel injection assembly to facilitate reduced NOx emissions in a combustor system
US10698628B2 (en) 2015-06-09 2020-06-30 Ultrata, Llc Infinite memory fabric hardware implementation with memory
US9803552B2 (en) 2015-10-30 2017-10-31 General Electric Company Turbine engine fuel injection system and methods of assembling the same
US11149941B2 (en) * 2018-12-14 2021-10-19 Delavan Inc. Multipoint fuel injection for radial in-flow swirl premix gas fuel injectors
CN110631017B (zh) * 2019-10-29 2020-11-27 深圳市佳运通电子有限公司 低氮燃烧器用双旋薄壁火形燃烧头

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JP2638394B2 (ja) * 1992-06-05 1997-08-06 日本ファーネス工業株式会社 低ＮＯｘ燃焼法
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Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102017114362A1 (de) * 2017-06-28 2019-01-03 Man Diesel & Turbo Se Brennkammer einer Gasturbine, Gasturbine und Verfahren zum Betreiben derselben

Also Published As

Publication number Publication date
GB2297151A (en) 1996-07-24
GB9500627D0 (en) 1995-03-08
JPH08233270A (ja) 1996-09-10
US5761906A (en) 1998-06-09
GB2297151B (en) 1998-04-22
JP3863210B2 (ja) 2006-12-27
DE69525920D1 (de) 2002-04-25
EP0722065B1 (de) 2002-03-20
EP0722065A2 (de) 1996-07-17
EP0722065A3 (de) 1997-06-04

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Legal Events

Date Code Title Description
8364 No opposition during term of opposition
8328 Change in the person/name/address of the agent

Representative=s name: DERZEIT KEIN VERTRETER BESTELLT

8327 Change in the person/name/address of the patent owner

Owner name: SIEMENS AG, 80333 MUENCHEN, DE