Fuel control

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

Patent

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60/181

F02C 9/16 (2006.01) F02C 9/28 (2006.01)

Patent

CA 1233651

Abstract Fuel Control A reduced fuel flow to a gas turbine engine experiencing impending overspend operating conditions is provided through a line (250) which bypasses the main shutoff valve (70) of the engine's fuel control (20). A transfer valve (260) disposed in the bypass line actuates the shutoff valve in response to such overspend conditions while opening the normally closed bypass line. A flow restictor (275) and the fuel control's main pressure regulating valve (210) combine to maintain the reduced fuel flow at a predetermined valve.

492940

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