发明名称 TURBINE ENGINE CONTROL SYSTEM
摘要 Fuel flow is scheduled to a plurality of combustion stages by putting a plurality of engine fuel flow governors in parallel with each other and letting the governor which outputs the lowest fuel demand signal be the one which schedules the total-fuel. flow to the engine. Fuel flows to the plurality of combustio n stages are then individually schedulled to achieve the lowest fuel flows consistent with predefined temperature limits for the corresponding stages off combustion.
申请公布号 CA2122148(C) 申请公布日期 2002.07.16
申请号 CA19922122148 申请日期 1992.10.29
申请人 发明人 CORBETT, NICHOLAS CHARLES;LINES, NORMAN PAUL
分类号 F02K9/28;F02C9/28;F23R3/34;(IPC1-7):F02C9/28 主分类号 F02K9/28
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