发明名称 |
SYSTEM AND METHOD FOR TURBINE COMBUSTOR FUEL ASSEMBLY |
摘要 |
A system includes a turbine fuel supply system. The turbine fuel supply system includes a first turbine fuel mixer configured to mix a first liquid fuel and a first deaerated water to generate a first fuel mixture. The first fuel mixture is configured to combust in a combustor of a gas turbine engine. The turbine fuel supply system also includes a deaerated water flow path configured to route the first deaerated water to the first turbine fuel mixer and a liquid fuel flow path configured to route the first liquid fuel to the first turbine fuel mixer.
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申请公布号 |
US2013098056(A1) |
申请公布日期 |
2013.04.25 |
申请号 |
US201113280237 |
申请日期 |
2011.10.24 |
申请人 |
ZHANG HUA;BEADIE DOUGLAS FRANK;MYERS GEOFFREY DAVID;CODRON FABIEN THIBAULT;ROSS WILLIAM THOMAS;GENERAL ELECTRIC COMPANY |
发明人 |
ZHANG HUA;BEADIE DOUGLAS FRANK;MYERS GEOFFREY DAVID;CODRON FABIEN THIBAULT;ROSS WILLIAM THOMAS |
分类号 |
F02C9/26;F02C3/30 |
主分类号 |
F02C9/26 |
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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