发明名称 TWO-STAGE FUEL PUMP FOR GAS TURBINES
摘要 A two-stage system for delivering fuel to a gas turbine including a first stage variable pump for serving as a primary source of fuel, a second stage fixed pump for selectively supplementing the variable pump, a bypass valve connected to the fixed pump for loading and unloading the fixed pump and a regulator valve assembly connected to the variable pump and the bypass valve for controlling operation of the variable pump and the bypass valve. Preferably, the two-stage system also includes a control valve connected to the regulator valve assembly for setting a pressure differential across the regulator valve assembly and, thereby, loading and unloading the fixed pump.
申请公布号 WO2007044020(A2) 申请公布日期 2007.04.19
申请号 WO2005US41523 申请日期 2005.11.15
申请人 GOODRICH PUMP & ENGINE CONTROL SYSTEMS, INC.;DESAI, MIHIR, C. 发明人 DESAI, MIHIR, C.
分类号 F02C7/236 主分类号 F02C7/236
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