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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    Title :

    FAIL-SAFE TAIL ROTOR SYSTEM


    Additional title:

    AUSFALLSICHERES HECKROTORSYSTEM
    SYSTÈME DE ROTOR DE QUEUE À SÉCURITÉ INTÉGRÉE


    Contributors:

    Publication date :

    2024-10-02


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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