MEANS FOR CALCULATING TURBINE INLET TEMPERATURE OF A GAS TURBINE ENGINE

摘要

MEANS FOR CALCULATING TURBINE INLET TEMPERATURE OF A GAS TURBINE ENGINE Turbine inlet temperature of a gas turbine engine is calculated from compressor discharge temperature, total and static pressures and total fuel metered to the engine by combining a sensed engine temperature with a derived fuel/air ratio and from the empirical burner can temperature rise equation solving for the turbine inlet temperature value.