Gas turbine engine fuel control system
A fuel control system having a combustive energy value evaluator determining a combustive energy value of the fuel, and a controller calculating a desired flow rate based at least on the combustive energy value and controlling a fuel metering device such that the fuel flow rate corresponds to the desired fuel flow rate.
1. A method of controlling a flow of a fuel mixture in a gas turbine engine comprising:
sensing at least one characteristic of the flow indicative of a proportion between two different types of fuel in the fuel mixture;
determining a combustive energy value of the fuel mixture based on the at least one characteristic;
determining a desired fuel flow rate at least based on the combustive energy value; and
controlling a fuel metering device of the engine to obtain the desired fuel flow rate.
2. The method as defined in claim 1 , wherein the desired fuel flow rate is determined at least based on the combustive energy value and on fuel schedules for a reference fuel.
3. The method as defined in claim 1 , further comprising determining at least one equivalent characteristic of a reference fuel corresponding to the combustive energy value, and displaying the at least one equivalent characteristic.
4. The method as defined in claim 3 , wherein the at least one equivalent characteristic of the reference fuel includes an equivalent mass flow of the reference fuel.
5. The method as defined in claim 1 wherein the combustive energy value is the lower heating value.
6. The method as defined in claim 1 , further comprising after start up of the gas turbine engine, sensing fuel and air mass flow of the engine, sensing pressure and temperature at at least one point of a flow path of the engine, and determining an instantaneous value of the combustive energy value based on the fuel mass flow of the engine, the air mass flow of the engine, and the pressure and temperature at the at least one point of the flow path.