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.
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 代理人
主权项
地址