A system, and corresponding method, for predicting failure of aircraft wing anti ice valves includes a processor configured to receive sensor inputs from a plurality of components that have a synchronous or an anti-synchronous relationship. The sensor inputs indicate an operational characteristic of the components. Memory records historical data from the sensor inputs and the memory is communicatively connected to the processor. The processor compares the synchronous or anti-synchronous relationship of at least two components in the plurality of components and the processor calculates a tolerance for operation of the at least two components based on historical failure data. The processor identifies component operating times that exceed the tolerance and predicts failure of such a component based on the historical failure data.
METHOD AND SYSTEM FOR PREDICTING WING ANTI-ICE FAILURE
2019-02-21
Patent
Elektronische Ressource
Englisch
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