发明名称 SYSTEM AND METHOD FOR CONTROLLING FUEL FLOW TO TURBINE COMPONENT
摘要 PROBLEM TO BE SOLVED: To provide a system and a method for controlling a fuel flow to a turbine component. SOLUTION: This system (200) and the method (300) can monitor one or more parameters associated with the fuel flow to the turbine component. The fuel flow may be modeled based at least in a part on the one or more monitored parameters. The fuel flow may be adjusted to a target flow based at least in a part on the modeling of the fuel flow. COPYRIGHT: (C)2011,JPO&INPIT
申请公布号 JP2010261440(A) 申请公布日期 2010.11.18
申请号 JP20100098366 申请日期 2010.04.22
申请人 GENERAL ELECTRIC CO <GE> 发明人 SNIDER DAVID AUGUST
分类号 F02C9/28;F02C9/00;F02C9/40 主分类号 F02C9/28
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