发明名称 FUEL CONTROL APPARATUS FOR GAS TURBINE ENGINE
摘要 A fuel control apparatus for a gas turbine engine reheat system which includes a plurality of burners has a plurality of variable metering orifices associated with the respective burners and a plurality of servo-responsive throttle valves downstream of the respective orifices. The apparatus includes an arrangement for controlling the servo pressures applied to the throttle valves, this arrangement including a governer driven by the engine and mounted on an internal ring gear. A first valve spool is coupled to the ring gear and is axially movable by the governer. The ring gear includes a coaxial spur gear which meshes with further spur gears forming parts of respective valve spools which control the servo pressures for associated throttle valves.
申请公布号 US3824786(A) 申请公布日期 1974.07.23
申请号 US19720291604 申请日期 1972.09.25
申请人 LUCAS AEROSPACE LTD,GB 发明人 SKINNER R,GB
分类号 F02C9/32;F02K3/08;(IPC1-7):F02K3/08 主分类号 F02C9/32
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