Gas turbine combustion chamber high speed combustion temperature sensor uses phase advance filter stage to predict temperature from sensor measurements

摘要

A gas turbine (1) combustion chamber (3) high speed combustion temperature sensor (10) has a detector (8) with high speed recorder (11A) predicting the temperature from the sensor delay using phase advance (11A) and retard (11B), delay (12), temperature change (13) and disturbance (14) filters.