A damping mechanism configured for use with a coupling of a power transmission assembly is provided including a cylindrical body having a first end and a second opposite end. The first end is configured for attachment to a first component of a power transmission assembly. A groove is formed in an exterior surface of the cylindrical body adjacent the second end. A cylindrical ring generally complementary to the groove is positioned partially within the groove such that a void exists between an inner surface of the cylindrical ring and the cylindrical body within the groove. A viscous material is arranged within the void such that non-concentric movement of the cylindrical ring relative to the cylindrical body causes displacement of the viscous material.


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    Title :

    VISCOUS DAMPER


    Contributors:

    Publication date :

    2017-08-24


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    F16F SPRINGS , Federn / B64C AEROPLANES , Flugzeuge / F16D COUPLINGS FOR TRANSMITTING ROTATION , Nicht schaltbare Kupplungen



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