Means for calculating turbine inlet temperature of a gas...

G - Physics – 01 – M

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G01M 15/00 (2006.01) F02C 9/28 (2006.01)

Patent

CA 1108761

MEANS FOR CALCULATING TURBINE INLET TEMPERATURE OF A GAS TURBINE ENGINE Abstract of the Disclosure 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. -1-

282017

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