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.


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    Titel :

    AIRCRAFT ENGINE HAVING SEAL ASSEMBLY DEFINING AN ELECTRICALLY CONDUCTIVE PATH


    Weitere Titelangaben:

    MOTEUR D'AERONEF COMPORTANT UN DISPOSITIF DE JOINT DEFINISSANT UN PARCOURS CONDUCTEUR ELECTRIQUE


    Beteiligte:
    KUDRNA RICHARD (Autor:in) / BRILLANT MELANIE (Autor:in)

    Erscheinungsdatum :

    12.07.2018


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16J Kolben , PISTONS / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT




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