The aircraft engine can have an engine casing housing the engine, the engine casing having a shaft aperture; a shaft rotatably mounted to the engine casing, the shaft protruding from the engine casing through the shaft aperture; and a seal assembly extending between the engine casing and the shaft adjacent the shaft aperture, the seal assembly defining an electrically conductive path between the engine casing and the shaft.
AIRCRAFT ENGINE HAVING SEAL ASSEMBLY DEFINING AN ELECTRICALLY CONDUCTIVE PATH
MOTEUR D'AERONEF COMPORTANT UN DISPOSITIF DE JOINT DEFINISSANT UN PARCOURS CONDUCTEUR ELECTRIQUE
2018-07-12
Patent
Electronic Resource
English
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