A bushing is disclosed herein. The bushing includes a body having a first end and a second end, a bore formed through the body from the first end to the second end, and a lock tab coupled to the body at a point between the first end and the second end of the body and extending toward the second end of the body, the lock tab extending from the body and into the bore.


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    Titel :

    SELF-LOCKING BUSHINGS


    Beteiligte:

    Erscheinungsdatum :

    13.06.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    F16C SHAFTS , Wellen / B64C AEROPLANES , Flugzeuge



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