DETECTING COMBUSTION ANOMALIES IN GAS TURBINES USING AUDIO OUTPUT
In one embodiment, a turbine system (10) includes a combustion system (20) comprising a plurality of combustion cans (23), a number of sensors (22), each of the number of sensors (22) coupled to a respective combustion can (23) of the number of combustion cans (23), and a controller (24). The contro...
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Sprache: | eng ; fre ; ger |
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Zusammenfassung: | In one embodiment, a turbine system (10) includes a combustion system (20) comprising a plurality of combustion cans (23), a number of sensors (22), each of the number of sensors (22) coupled to a respective combustion can (23) of the number of combustion cans (23), and a controller (24). The controller (24) includes a memory (26, 27) storing one or more processor-executable routines and a processor (28, 29) configured to access and execute the one or more routines encoded by the memory (26, 27). The one or more routines, when executed cause the processor (28, 29) to receive one or more signals from the number of sensors (22), convert the one or more signals to audio output (34), and output the converted audio output (34) via one or more audio output devices (30, 31). |
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