Pratt-Whitney Canada Corp

Ehsan Farvardin

Gabriel St-Laurent

Benjamin Z Seaman

Benoit Trudel

Sri Krishna Subramanian

Velda Wong

Nicolas Marchand

An assembly for an aircraft propulsion system includes a case assembly, at least one seal, a first pressure sensor, and a computing system. The case assembly forms a cavity. The at least one seal is disposed on the case assembly. The at least one seal is configured to seal the cavity. The first pressure sensor is in fluid communication with the cavity. The first pressure sensor is configured to measure a first pressure within the cavity. The computing system is in signal communication with the first pressure sensor. The computing system includes a processor in communication with a non-transitory memory storing instructions, which instructions when executed by the processor, cause the processor to compare the first pressure to a pressure threshold value to identify a wear condition of the at least one seal.

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Longueuil, Canada

Ehsan Farvardin