JP2011069607A5 - - Google Patents

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Publication number
JP2011069607A5
JP2011069607A5 JP2010200408A JP2010200408A JP2011069607A5 JP 2011069607 A5 JP2011069607 A5 JP 2011069607A5 JP 2010200408 A JP2010200408 A JP 2010200408A JP 2010200408 A JP2010200408 A JP 2010200408A JP 2011069607 A5 JP2011069607 A5 JP 2011069607A5
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JP
Japan
Prior art keywords
fuel
support
gas turbine
combustion system
manifold
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.)
Granted
Application number
JP2010200408A
Other languages
English (en)
Japanese (ja)
Other versions
JP5715360B2 (ja
JP2011069607A (ja
Filing date
Publication date
Priority claimed from US12/564,293 external-priority patent/US8365533B2/en
Application filed filed Critical
Publication of JP2011069607A publication Critical patent/JP2011069607A/ja
Publication of JP2011069607A5 publication Critical patent/JP2011069607A5/ja
Application granted granted Critical
Publication of JP5715360B2 publication Critical patent/JP5715360B2/ja
Expired - Fee Related legal-status Critical Current
Anticipated expiration legal-status Critical

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JP2010200408A 2009-09-22 2010-09-08 汎用複数ノズル燃焼システム及び方法 Expired - Fee Related JP5715360B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/564,293 2009-09-22
US12/564,293 US8365533B2 (en) 2009-09-22 2009-09-22 Universal multi-nozzle combustion system and method

Publications (3)

Publication Number Publication Date
JP2011069607A JP2011069607A (ja) 2011-04-07
JP2011069607A5 true JP2011069607A5 (enExample) 2013-10-17
JP5715360B2 JP5715360B2 (ja) 2015-05-07

Family

ID=43603639

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2010200408A Expired - Fee Related JP5715360B2 (ja) 2009-09-22 2010-09-08 汎用複数ノズル燃焼システム及び方法

Country Status (5)

Country Link
US (1) US8365533B2 (enExample)
JP (1) JP5715360B2 (enExample)
CN (1) CN102022729B (enExample)
CH (1) CH701878B1 (enExample)
DE (1) DE102010037409A1 (enExample)

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* Cited by examiner, † Cited by third party
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US8322143B2 (en) * 2011-01-18 2012-12-04 General Electric Company System and method for injecting fuel
US8938976B2 (en) * 2011-05-20 2015-01-27 Siemens Energy, Inc. Structural frame for gas turbine combustion cap assembly
US8893382B2 (en) * 2011-09-30 2014-11-25 General Electric Company Combustion system and method of assembling the same
US9188335B2 (en) * 2011-10-26 2015-11-17 General Electric Company System and method for reducing combustion dynamics and NOx in a combustor
US9400104B2 (en) 2012-09-28 2016-07-26 United Technologies Corporation Flow modifier for combustor fuel nozzle tip
US9267689B2 (en) 2013-03-04 2016-02-23 Siemens Aktiengesellschaft Combustor apparatus in a gas turbine engine
US9322558B2 (en) * 2013-06-27 2016-04-26 Siemens Aktiengesellschaft Combustor apparatus in a gas turbine engine
US9494050B2 (en) 2013-09-20 2016-11-15 The Boeing Company Concentric nozzles for enhanced mixing of fluids
US10041679B2 (en) 2015-06-24 2018-08-07 Delavan Inc Combustion systems
US10578021B2 (en) 2015-06-26 2020-03-03 Delavan Inc Combustion systems
US10267524B2 (en) 2015-09-16 2019-04-23 Woodward, Inc. Prefilming fuel/air mixer
US10724740B2 (en) 2016-11-04 2020-07-28 General Electric Company Fuel nozzle assembly with impingement purge
US10634353B2 (en) * 2017-01-12 2020-04-28 General Electric Company Fuel nozzle assembly with micro channel cooling
JP7112342B2 (ja) * 2019-01-25 2022-08-03 三菱重工業株式会社 ガスタービン燃焼器及びガスタービン

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US5274991A (en) * 1992-03-30 1994-01-04 General Electric Company Dry low NOx multi-nozzle combustion liner cap assembly
US5303542A (en) * 1992-11-16 1994-04-19 General Electric Company Fuel supply control method for a gas turbine engine
US5289685A (en) * 1992-11-16 1994-03-01 General Electric Company Fuel supply system for a gas turbine engine
US5323604A (en) * 1992-11-16 1994-06-28 General Electric Company Triple annular combustor for gas turbine engine
DE4411623A1 (de) * 1994-04-02 1995-10-05 Abb Management Ag Vormischbrenner
US5630319A (en) * 1995-05-12 1997-05-20 General Electric Company Dome assembly for a multiple annular combustor
US5682747A (en) * 1996-04-10 1997-11-04 General Electric Company Gas turbine combustor heat shield of casted super alloy
US5901548A (en) * 1996-12-23 1999-05-11 General Electric Company Air assist fuel atomization in a gas turbine engine
US6112971A (en) * 1999-05-12 2000-09-05 General Electric Co. Multi-nozzle combustion end cover vacuum brazing process
US6983605B1 (en) * 2000-04-07 2006-01-10 General Electric Company Methods and apparatus for reducing gas turbine engine emissions
US6415594B1 (en) * 2000-05-31 2002-07-09 General Electric Company Methods and apparatus for reducing gas turbine engine emissions
US6298667B1 (en) * 2000-06-22 2001-10-09 General Electric Company Modular combustor dome
US6405523B1 (en) * 2000-09-29 2002-06-18 General Electric Company Method and apparatus for decreasing combustor emissions
US6453660B1 (en) * 2001-01-18 2002-09-24 General Electric Company Combustor mixer having plasma generating nozzle
US6758045B2 (en) * 2002-08-30 2004-07-06 General Electric Company Methods and apparatus for operating gas turbine engines
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JP3996100B2 (ja) * 2003-07-11 2007-10-24 株式会社日立製作所 ガスタービン用燃焼器及びその運転方法
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JP4015656B2 (ja) * 2004-11-17 2007-11-28 三菱重工業株式会社 ガスタービン燃焼器
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JP4882422B2 (ja) * 2006-02-28 2012-02-22 株式会社日立製作所 ガスタービン燃焼器および燃焼装置の燃焼方法
US7827797B2 (en) * 2006-09-05 2010-11-09 General Electric Company Injection assembly for a combustor
JP4364911B2 (ja) * 2007-02-15 2009-11-18 川崎重工業株式会社 ガスタービンエンジンの燃焼器
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CN101275750B (zh) * 2008-04-25 2010-12-08 北京航空航天大学 一种径向旋流器拐弯区直接喷射预混预蒸发低污染燃烧室
US8113000B2 (en) * 2008-09-15 2012-02-14 Siemens Energy, Inc. Flashback resistant pre-mixer assembly
US8205452B2 (en) * 2009-02-02 2012-06-26 General Electric Company Apparatus for fuel injection in a turbine engine

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