Monitoring system and method for wiring systems

G - Physics – 01 – R

Patent

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Details

G01R 31/02 (2006.01) B64D 45/00 (2006.01) G01R 31/00 (2006.01) G01R 31/08 (2006.01) G01R 31/12 (2006.01)

Patent

CA 2426530

A monitoring system (100) includes at least one partial discharge (pd) sensor (10). The pd sensor is configured to monitor a component (22) of an aircraft wiring system (130) and to acquire a monitoring signal. A method embodiment for monitoring an aircraft wiring system includes acquiring a number of monitoring signals for a number of components of the aircraft wiring system using a number of partial discharge pd sensors. The method further includes conveying the monitoring signals from at least one of the pd sensors to a data acquisition system (40).

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