Gas turbine fuel control system
A method of controlling a flow of a fuel mixture of different types of fuel in a gas turbine engine is described which includes determining a combustive energy value of an input of the fuel mixture in the engine, extracting fuel schedule data from a fuel schedule established for a reference fuel, determining a desired fuel mixture flow rate by adapting the fuel schedule data to the fuel mixture based on the combustive energy value, and controlling a fuel metering device of the engine such that the fuel mixture flow rate corresponds to the desired fuel mixture flow rate.
1. A method of controlling a flow of a fuel mixture of different types of fuel in a gas turbine engine, the method comprising:
determining a combustive energy value of an input of the fuel mixture in the gas turbine engine, by calculating the combustive energy value from a proportion of each of the types of fuel in the fuel mixture and from a known combustive energy value of the each of the types of fuel;
extracting fuel schedule data from a fuel schedule established for a reference fuel;
determining a desired fuel mixture flow rate by adapting the fuel schedule data to the fuel mixture based on the combustive energy value; and
controlling a fuel metering device of the gas turbine engine such that a fuel mixture flow rate corresponds to the desired fuel mixture flow rate.
2. The method as defined in claim 1 , wherein the desired fuel mixture fuel flow rate is a required fuel flow rate upon start up of the gas turbine engine, the fuel schedule includes start up fuel data, and the combustive energy value is determined before start up of the gas turbine engine.
3. The method as defined in claim 2 , wherein determining the combustive energy value includes directly sensing the combustive energy value.
4. The method as defined in claim 2 , further comprising sensing the proportion the of each of the types of fuel in the fuel mixture.
5. The method as defined in claim 1 , wherein the desired fuel mixture fuel flow rate is a required fuel flow rate while the gas turbine engine is lit, the method further includes a step of sensing temperature and pressure characteristics of the flow of the fuel mixture and of air within the gas turbine engine to produce engine sensor data, and wherein the fuel schedule data is extracted from the fuel schedule based on the engine sensor data.
6. The method as defined in claim 5 , further comprising sensing one or more of a flow rate of the air in the gas turbine engine, a rise in temperature of the air during combustion, and the fuel mixture flow rate, and wherein determining the combustive energy value is performed by calculating the combustive energy from the sensed one or more of the air flow rate, the rise in temperature and the fuel mixture flow rate.
7. The method as defined in claim 5 , wherein determining the combustive energy value includes directly sensing the combustive energy value.
8. The method as defined in claim 5 , wherein determining the combustive energy value includes sensing the proportion of the each of the types of fuel in the fuel mixture, and calculating the combustive energy value from the sensed proportion and from the combustive energy value of each of the types of fuel.
9. The method as defined in claim 1 , further comprising determining at least one equivalent characteristic of the reference fuel corresponding to the combustive energy value, and displaying the at least one equivalent characteristic.
10. The method as defined in claim 9 , wherein the at least one equivalent characteristic of the reference fuel includes an equivalent mass flow of the reference fuel.
11. The method as defined in claim 1 wherein the combustive energy value is the lower heating value.