US 3,939,649 AGranted

Fuel control

AssigneeChandler Evans Inc.

InventorRalph P. McCabe

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Abstract

A hydromechanical fuel control for a turboshaft engine includes a gas producer control and an independent power turbine governor in series flow relationship. The basic gas producer control includes an acceleration system, a deceleration system and all speed governor to regulate the fuel flow output of the gas producer control. The acceleration system includes a main metering valve which is positioned by a compressor discharge pressure responsive device and the all speed governor. A speed responsive computer mechanism controls the head across the metering valve. The computer mechanism includes an enrichment valve and a start valve and is connected to the shut-off valve lever for the fuel control in such a manner that the mechanism may be controlled by actuation of this lever. The power turbine governor includes a fuel flow reset governor and a deceleration system to prevent flameouts. The fuel control and power turbine each have separate input levers and meter fuel to the engine in accordance with the lowest demanded fuel flow.

Claims3

Dependent claims

In a fuel control for a gas turbine engine with a gas producer and a power turbine, a power turbine governor comprising:

an inlet for receiving fuel from a gas producer control;
an outlet for delivering fuel to the engine;
conduit means to fluidly interconnect the inlet and the outlet for providing a path for fuel flow;
sensor means to generate an actual speed signal representative of the speed of the power turbine;
speed setting means to generate a set speed signal for the power turbine;
governor valve means responsive to the actual speed signal and the set speed signal to meter fuel flow in the conduit means;
overspeed valve means responsive to the actual speed signal to present a restriction to fuel flow in the conduit means upstream of the governor valve means when an overspeed condition of the power turbine arises;
and
regulator means to maintain a substantially constant differential pressure between locations in the conduit means upstream of the overspeed valve means and downstream of the governor valve means by bypassing fuel, the overspeed valve means not presenting a substantial restriction to fuel flow until an overspeed condition arises, whereby the regulator means maintains a substantially constant differential pressure across the governor valve means during normal operation and governing and whereby the overspeed valve means causes the regulator means to bypass more fuel when an overspeed condition arises to thereby reduce fuel flow to the governor valve means.

6 more elements

In a fuel control for a gas turbine engine with a gas producer having a compressor and a power turbine, a power turbine governor comprising:

an inlet for receiving fuel from a gas producer control;
an outlet for delivering fuel to the engine;
conduit means to fluidly interconnect the inlet and the outlet for providing a path for fuel flow;
sensor means to generate an actual speed signal representative of the speed of the power turbine;
speed setting means to generate a set speed signal for the power turbine;
governor valve means responsive to the actual speed signal and the set speed signal to meter fuel flow in the conduit means;
regulator means to maintain a substantially constant differential pressure between first and second locations in the conduit means respectively upstream and downstream of the governor valve means;
and
deceleration valve means sensitive to the pressure discharged by the compressor to provide a flow path in parallel with the conduit means to bypass flow around the governor valve means to insure a minimum fuel flow to compressor discharge pressure ratio during deceleration, the differential pressure across the deceleration valve means being the same as that across the governor valve means.

6 more elements

Dependencies are inferred from the claim text.