Fuel control system for gas turbine engines
View Patent ↗Fuel control systems for use with a gas turbine engines which accounts for real-time thermodynamic engine effects when attempting to match or track the NDOT Actual rate to the NDOT Demand rate. The fuel control system includes a mechanism for measuring several engine operating parameters and a mechanism for determining an initial engine fuel demand based on the measured engine operating parameters. The control system further includes a mechanism for estimating, during engine operation and based on the measured operating parameters, the amount of heat transferred between fuel combustion gases and the engine metal and estimating an effective fuel flow adjustment based therefrom. The control system disclosed herein also includes a mechanism for determining a final engine fuel demand based on the initial predicted engine fuel demand and the estimated effective fuel flow adjustment.
1. A fuel control method for gas turbines having a compressor and a gas generator, comprising:
a) measuring a plurality of engine operating parameters;
b) determining an initial engine fuel demand based on the plurality of measured engine operating parameters;
c) estimating during engine operation and based on the plurality of measured operating parameters, an amount of heat transferred between fuel combustion gases and engine metal;
d) estimating an effective fuel flow adjustment based on the estimated heat transfer between the combustion gases and the engine metal; and
e) determining a final engine fuel demand based on the initial engine fuel demand and the estimated effective fuel flow adjustment.
2. A fuel control method as recited in claim 1 , wherein the step of measuring a plurality of engine operating parameters includes the steps of measuring the gas generator speed and providing a gas generator speed signal indicative of the actual rotary speed of the gas generator.
3. A fuel control method as recited in claim 2 , wherein the step of determining the initial engine fuel demand includes the use of fuel flow controller which iteratively compares an actual rate of change of gas generator speed which is determined from the gas generator speed signal to a maximum and minimum desired rate of change of gas generator speed.
4. A fuel control method as recited in claim 3 , wherein the maximum and minimum desired rate of change of gas generator speed is determined based on an acceleration/deceleration schedule and is a function of the gas generator speed signal.
5. A fuel control method as recited in claim 1 , wherein the step of measuring a plurality of engine operating parameters includes the steps of measuring engine compressor discharge pressure and providing a compressor discharge pressure signal indicative of the actual engine compressor discharge pressure.
6. A fuel control method as recited in claim 1 , wherein the step of estimating the amount of heat transferred between the fuel combustion gases and the engine metal comprises:
a) estimating an amount of heat generated by engine fuel combustion;
b) estimating an amount of heat generated by engine supply air compression; and
c) estimating gas generator exit gas temperature.
7. A fuel control method as recited in claim 1 , wherein the step of estimating the effective fuel flow adjustment includes determining the effective fuel flow adjustment from the estimated heat transfer, a gas generator efficiency and a heating coefficient of fuel.
8. A fuel control method as recited in claim 7 , wherein the step of estimating the effective fuel flow adjustment further comprises amplifying by amplifier means the effective fuel flow adjustment.
9. A fuel control method as recited in claim 1 , further comprising providing, by means of a fuel metering system, fuel to the engine based on the signal of final engine fuel demand.
10. A fuel control method as recited in claim 9 , wherein the fuel metering device includes a variable displacement vane pump.