发明名称 Fuel control system for a gas turbine engine
摘要 The system comprises a main fuel controller which varies the fuel flow to the engine in accordance with the engine pressure ratio and an idling fuel control arranged to control to a constant value of engine HP rotor speed. In the embodiment a variable bleed orifice 52 is allowed to reduce the control pressure which operates the main fuel valve 19. <IMAGE>
申请公布号 GB2093918(A) 申请公布日期 1982.09.08
申请号 GB19820001195 申请日期 1982.01.18
申请人 ROLLS ROYCE LTD 发明人
分类号 F02C9/28;(IPC1-7):F02C9/28 主分类号 F02C9/28
代理机构 代理人
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