Simulated parameter control for gas turbine engine

G - Physics – 05 – B

Patent

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354/1, 354/24

G05B 9/02 (2006.01) F02C 9/46 (2006.01)

Patent

CA 1120156

Abstract of the Disclosure For a failure of a sensor utilized in the controls for a gas turbine engine, calculations from other parameters based on the thermodynamics of the cycle serve to simulate the value otherwise manifested by the failed sensor. -1-

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