System and method for controlling fuel flow to a gas turbine engine
First Claim
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1. A system for delivering fuel from a fuel source to a gas turbine engine combustor, comprising:
- a fuel supply line having an inlet coupled to the fuel source and an outlet coupled to the combustor;
a metering valve positioned in flow-series in the supply line;
a bypass flow line coupled between an inlet of the metering valve and the fuel supply line inlet for bypassing a portion of the fuel in the supply line back to the inlet;
a bypass valve positioned in flow-series in the bypass flow line; and
a controller operable to selectively adjust one of the metering valve and the bypass valve to control fuel flow rate from the fuel source to the combustor.
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Abstract
A system for controlling the flow of fuel to a gas turbine engine is operable in at least two modes. In a first mode, the flow rate of fuel supplied from a fuel source to the combustors of the turbine engine is controlled by modulating the position of a metering valve. A controller determines the controllability of the metering valve and, if it is determined to be non-controllable, then the system is operated in the second mode. In the second mode, the flow rate of fuel supplied to the combustors is controlled by modulating the position of a bypass valve.
32 Citations
19 Claims
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1. A system for delivering fuel from a fuel source to a gas turbine engine combustor, comprising:
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a fuel supply line having an inlet coupled to the fuel source and an outlet coupled to the combustor;
a metering valve positioned in flow-series in the supply line;
a bypass flow line coupled between an inlet of the metering valve and the fuel supply line inlet for bypassing a portion of the fuel in the supply line back to the inlet;
a bypass valve positioned in flow-series in the bypass flow line; and
a controller operable to selectively adjust one of the metering valve and the bypass valve to control fuel flow rate from the fuel source to the combustor. - View Dependent Claims (2, 3, 4, 5, 6, 7, 8, 9, 10, 11, 12, 13)
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14. A controller for controlling the flow rate of fuel from a pressurized fuel source to a gas turbine engine combustor via a metering valve, comprising:
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a first valve driver circuit portion operable to generate a first valve driver signal;
a second valve driver circuit portion operable to generate a second valve driver signal;
at least one processor operable to determine whether the metering valve is controllable or non-controllable and, based on the determination, to enable one of the first and second valve driver circuits and disable the other. - View Dependent Claims (15, 16, 17, 18, 19)
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Specification