发明名称 METHOD OF OPERATING DUAL-GAS TURBINE FUEL SYSTEM
摘要 <p><P>PROBLEM TO BE SOLVED: To provide a method of operating a system that supplies dual-gas fuel to a single manifold. <P>SOLUTION: The method includes a step of selecting a manifold and fuel flow split, a step of setting a stroke of a high-energy gas control valve 132 based on the fuel split, a step of measuring a primary manifold nozzle pressure ratio, a step of comparing the primary manifold nozzle pressure ratio to a primary manifold specification limit, a step of adjusting a stroke of a primary low-energy gas control valve 130 to maintain the pressure ratio across a primary manifold nozzle outlet 124 within the primary manifold specification limit, a step of measuring a secondary manifold nozzle pressure ratio, a step of comparing the secondary manifold nozzle pressure ratio to a secondary manifold specification limit, and a step of adjusting a stroke of a secondary low-energy gas control valve 134 to maintain the pressure ratio across a secondary manifold nozzle outlet 128 within the secondary manifold specification limit. <P>COPYRIGHT: (C)2010,JPO&INPIT</p>
申请公布号 JP2009270574(A) 申请公布日期 2009.11.19
申请号 JP20090108602 申请日期 2009.04.28
申请人 GENERAL ELECTRIC CO <GE> 发明人 ALEXANDER MICHAEL J;JOSHI RAHUL MOHAN;IASILLO ROBERT J;MORANKAR JITENDRA
分类号 F02C9/40;F02C7/22;F02C9/00;F02C9/28 主分类号 F02C9/40
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