发明名称 |
統合制御弁を有するガスタービンエンジン燃焼器アセンブリ |
摘要 |
<p>A combustor assembly for a gas turbine engine includes a combustor endcover having at least one fuel circuit and mounted thereto a plurality of pre-mixers and at least one control valve. The at least one control valve is fluidly connected to the at least one fuel circuit and operatively connected to a controller. The controller selectively operates the at least one control valve to deliver fuel through the at least one fuel circuit to the plurality of pre-mixers in order to achieve an enhanced level of operational flexibility by providing individual combustion chamber control.</p> |
申请公布号 |
JP5676073(B2) |
申请公布日期 |
2015.02.25 |
申请号 |
JP20080216044 |
申请日期 |
2008.08.26 |
申请人 |
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发明人 |
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分类号 |
F02C9/34;F02C7/00;F02C7/228;F02C7/232;F02C9/00;F23R3/00;F23R3/28;F23R3/34 |
主分类号 |
F02C9/34 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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