Method and system to determine composition of fuel entering combustor
Disclosed is a method and system for determining composition of a fuel entering a combustor. The method includes determining a temperature of the fuel entering the combustor, calculating a first estimated total fuel flow utilizing fuel properties and fuel nozzle effective area (A e ), and calculating a second estimated total fuel flow utilizing an aero-thermal cycle model analysis. The first estimated total fuel flow is compared to the second estimated total fuel flow and a lower heating value of the fuel is determined from a difference between the first estimated total fuel flow and the second estimated total fuel flow. A method and system for controlling a gas turbine includes calculating effects of the fuel composition on performance of the gas turbine and comparing one or more performance parameters to one or more parameter limits. One or more machine controls of the gas turbine are changed based on the results of the comparison.
1. A method for determining composition of a fuel entering a combustor comprising:
determining a temperature of the fuel entering the combustor;
inputting the temperature of the fuel, at least one fuel property and a fuel injector nozzle effective area (A e ) into a fuel system model;
calculating a first estimated total fuel flow utilizing the fuel system model;
calculating a second estimated total fuel flow utilizing an aero-thermal cycle model;
comparing the first estimated total fuel flow to the second estimated total fuel flow; and
determining a lower heating value of the fuel from a difference between the first estimated total fuel flow and the second estimated total fuel flow, thereby determining an identifier of fuel composition.
2. The method of claim 1 wherein the temperature of the fuel entering the combustor is determined by measuring the temperature of the fuel at an exit of at least one injector nozzle in the combustor.
3. The method of claim 1 including determining proportions of one or more constituents in the fuel.
4. The method of claim 3 wherein the proportions of one or more constituents are determined by inputting the lower heating value into a relative constituent model.
5. The method of claim 3 wherein the proportions of one or more constituents are determined by utilizing one or more constituent sensors to measure quantities of one or more constituents.
6. The method of claim 3 wherein the proportions of one or more constituents are determined by:
utilizing one or more constituent sensors to determine a quantity of at least one constituent of the one or more constituents;
inputting the quantity of the at least on constituent into a relative constituent model; and
determining the relative quantities of remaining desired constituents by inputting the lower heating value into the relative constituent model.
7. A system for determining fuel composition entering a combustor including:
at least one temperature sensor for measuring a temperature of a fuel entering the combustor;
an engine model for outputting a first estimated total fuel flow based on a baseline fuel composition;
a fuel system model for outputting a second estimated total fuel flow based on the fuel temperature; and
a comparator for determining a lower heating value of the fuel by comparing the first estimated total fuel flow to the second estimated total fuel flow, thereby determining an identifier of fuel composition.
8. The system of claim 7 further comprising a relative constituent model capable of determining relative proportions of constituents in the fuel based on the lower heating value.
9. The system of claim 7 further comprising one or more constituent sensors to measure quantities of one or more constituents.