JP2011220673A5 - - Google Patents

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Publication number
JP2011220673A5
JP2011220673A5 JP2011084134A JP2011084134A JP2011220673A5 JP 2011220673 A5 JP2011220673 A5 JP 2011220673A5 JP 2011084134 A JP2011084134 A JP 2011084134A JP 2011084134 A JP2011084134 A JP 2011084134A JP 2011220673 A5 JP2011220673 A5 JP 2011220673A5
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JP
Japan
Prior art keywords
fuel injection
injection nozzles
fuel
transition duct
stage turbine
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JP2011084134A
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English (en)
Japanese (ja)
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JP2011220673A (ja
JP5236769B2 (ja
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Priority claimed from US12/758,296 external-priority patent/US8082739B2/en
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Publication of JP2011220673A publication Critical patent/JP2011220673A/ja
Publication of JP2011220673A5 publication Critical patent/JP2011220673A5/ja
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Publication of JP5236769B2 publication Critical patent/JP5236769B2/ja
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JP2011084134A 2010-04-12 2011-04-06 燃料ステージングによる燃焼器出口温度プロファイル制御及び関連方法 Active JP5236769B2 (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US12/758,296 US8082739B2 (en) 2010-04-12 2010-04-12 Combustor exit temperature profile control via fuel staging and related method
US12/758,296 2010-04-12

Publications (3)

Publication Number Publication Date
JP2011220673A JP2011220673A (ja) 2011-11-04
JP2011220673A5 true JP2011220673A5 (enExample) 2012-07-26
JP5236769B2 JP5236769B2 (ja) 2013-07-17

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ID=44260276

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2011084134A Active JP5236769B2 (ja) 2010-04-12 2011-04-06 燃料ステージングによる燃焼器出口温度プロファイル制御及び関連方法

Country Status (4)

Country Link
US (1) US8082739B2 (enExample)
EP (1) EP2375167B1 (enExample)
JP (1) JP5236769B2 (enExample)
CN (1) CN102235670B (enExample)

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JP5180807B2 (ja) 2008-12-24 2013-04-10 三菱重工業株式会社 1段静翼の冷却構造、及びガスタービン
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US9354618B2 (en) 2009-05-08 2016-05-31 Gas Turbine Efficiency Sweden Ab Automated tuning of multiple fuel gas turbine combustion systems
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