发明名称 |
Gas turbine engine combustor assembly having integrated control valves |
摘要 |
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.
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申请公布号 |
US7891192(B2) |
申请公布日期 |
2011.02.22 |
申请号 |
US20070892859 |
申请日期 |
2007.08.28 |
申请人 |
GENERAL ELECTRIC COMPANY |
发明人 |
MYERS GEOFFREY DAVID;DAVIS, JR. LEWIS BERKLEY;CITENO JOSEPH |
分类号 |
F02C1/00 |
主分类号 |
F02C1/00 |
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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