Fuel control
AssigneeUnited Technologies Corporation
InventorKenneth P. Hansen
Life of this patent
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Abstract
Fuel flow to the burner (10) of a gas turbine engine (15) is turned on and off by a minimum pressure valve (60) controlled by a fluid pressure operated sequence valve (110). The sequence valve includes a valve element (125) set by the pressurization thereof with fuel discharged from a pump (35). The setting of the sequence valve element (125) is maintained by a fluid latch also energized by fuel discharged from the pump whereby no complex linkages or electric motors are required for the setting of the sequence valve and the maintenance of such setting.
Claims5
In a fuel control for a gas turbine engine including a burner, fuel being supplied to said burner by a pump through a fluid pressure operated minimum pressure valve opened to allow fuel flow from said pump to said burner and closed to shut off said fuel flow, actuation of said minimum pressure valve being controlled by a sequence valve communicating with said minimum pressure valve by a fluid line, the improvement characterized by:
- said sequence valve being connected to pump discharge pressure by a pump discharge line and including a moveable valve element, the position thereof controlling the pressure in said fluid line, thereby determining the actuation of said minimum pressure valve, and further including a fluid latch comprising a piston connected to said valve element and communicating with said pump discharge pressure at said sequence valve through a fluid passage, pressurization of said piston in a first direction by said fuel maintaining said sequence valve element in a latched condition for maintenance of said minimum pressure valve in an opened condition to sustain fuel flow from said pump to said burner.
Dependencies are inferred from the claim text.