Nonsynchronous turbine blade vibration monitoring system

G - Physics – 01 – H

Patent

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60/184, 354/26

G01H 11/00 (2006.01) F01D 11/08 (2006.01) G01H 1/00 (2006.01) G01M 1/22 (2006.01)

Patent

CA 1329848

19 ABSTRACT OF THE DISCLOSURE A nonsynchronous turbine blade vibration monitoring system is comprised of a maximum of two sensors circumferentially mounted along the turbine blade row for detecting the actual arrival times of the turbine blades at the sensors. Expected arrival times of the turbine blades at the sensors are determined and then compared to the actual arrival times in order to obtain turbine blade deflection data. Harmonic analysis is then performed on the blade deflection data to determine the level of vibration at each fractional harmonic.

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