Turbine blade shroud temperature monitor

G - Physics – 01 – K

Patent

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73/72

G01K 7/38 (2006.01) G01K 1/20 (2006.01) G01K 13/08 (2006.01)

Patent

CA 2003727

ABSTRACT OF THE DISCLOSURE A system for monitoring the temperature of a plurality of turbine blade shroud segments includes indicia carried by each shroud segment. A sensor produces input signals in response to the indicia. A temperature sensor measures the temperature of the sensor producing the input signals. A first circuit, responsive to the temperature sensor, corrects the input signals to compensate for the effects of temperature on the sensor. A second circuit determines the temperature of each shroud segment based on the corrected input signals.

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