Combustion monitor

G - Physics – 06 – F

Patent

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341/17

G06F 15/20 (1980.01)

Patent

CA 1112738

51GA-2463 ABSTRACT OF THE DISCLOSURE An apparatus for monitoring whether the combustion system of a gas turbine is working properly includes an annular array of temperature sensors disposed in the gas turbine to monitor the temperature of the hot gas stream at a plurality of spaced positions, a digital computer, a circuit to input signals indicative of the sensed temperatures of a selected sensor to the digital computer, and a circuit for selecting the temperature sensor to be sampled. The digital computer is programmed to sequentially sample the sensors and computer temperature spread or spreads and to output a shutdown or alarm signal when one of the spreads exceeds a predetermined or calculated amount.

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