Gas turbine engine fuel control system

F - Mech Eng,Light,Heat,Weapons – 02 – C

Patent

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60/181

F02C 9/36 (2006.01)

Patent

CA 1293131

ABSTRACT OF THE DISCLOSURE A gas turbine engine fuel control has spill valve responsive to an input control signal, for spilling fuel from a supply passage. A pressurising valve controls flow from the supply passage to the engine, in response to the pressure in the supply passage. A throttle valve in series with the pressurising valve maintains the pressure difference across the pressurising valve substantially constant. A selector valve is operable to shut both the pressurising valve and a shut-off element in the throttle valve.

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