| 主权项 |
1. A method for determining fuel splits for a gas turbine, the method comprising:
monitoring, with a computing device, an airflow-related parameter of the gas turbine; determining, with the computing device, first and second reference values for the airflow-related parameter based on a combustion reference temperature of the gas turbine, the first reference value being associated with a first load path of the gas turbine and the second reference value being associated with a second load path of the gas turbine; determining, with the computing device, first and second fuel split commands based on the combustion reference temperature, the first fuel split command being associated with the first load path of the gas turbine and the second fuel split command being associated with the second load path of the gas turbine; determining, with the computing device, a fuel split value to be applied within the gas turbine in association with a monitored value of the airflow-related parameter based at least in part on the first and second reference values and the first and second fuel split commands; and applying, with the computing device, the fuel split value within the gas turbine to regulate an amount of fuel supplied to one or more fuel circuits of the gas turbine. |
