According to an aspect, a clevis assembly includes a shackle having two ends, each end respectively including an aperture, a structure connecting the apertures and housing a bearing, and a shearing device that includes a frangible point and is in operable communication with the bearing, where the shearing device is housed in a hollow portion of the structure.


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    Titel :

    FAIL-SAFE TAIL ROTOR SYSTEM


    Beteiligte:
    RAMOTH ROGER H (Autor:in) / YOUNG SCOTT J (Autor:in) / YATES TRAVIS L (Autor:in)

    Erscheinungsdatum :

    01.07.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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