Automatic vent for fuel control

Claim 1

A fuel system for a gas turbine engine having a burner and fuel feeding means including a fuel line interconnecting the fuel control and burner, at least a fuel tank and an alternate fuel tank and means for sequentially placing either fuel tank on line so as to interconnect with said fuel control, fuel pumping means in said fuel line interconnected to alternately either of said fuel tanks, in combination with said fuel control which has a minimum pressure and shut-off valve between the fuel metering means of the fuel control and said burner so that fuel is admitted to said burner solely upon reaching a predetermined minimum value, means for expunging trapped air captured in said fuel feeding means including a bypass line bypassing a portion of fuel metered by the fuel metering means around the minimum pressure and shut-off valve, means for actuating said fuel control, means including a fixed restriction and a moveable valve responsive to said actuating means in said bypass line for automatically interconnecting said bypass means to lead air around said minimum pressure and shut-off valve to said burner and a windmill bypass line that interconnects fuel downstream of the fuel metering means and the inlet of said pump and being disposed in parallel flow relationship with said minimum pressure and shut-off valve, and a selector valve also responsive to said actuating means for rendering said windmill bypass line operative whenever said minimum pressure and shut-off valve is actuated closed and said bypass line is actuated open to lead ait to said burner.