A standpipe assembly for a rotorcraft (100) includes a slip ring (204) positioned within the mast (114) of the rotorcraft (100). The slip ring (204) includes a stator (304) rotationally connected to a rotor (302). A flexible coupling (202) is connected to the stator (304) and a standpipe tube (206) is connected to the flexible coupling (202). The flexible coupling (202) is capable of angular, axial, and torsional displacement.


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    Title :

    FLEXIBLE COUPLING FOR STANDPIPE ASSEMBLY


    Additional title:

    FLEXIBLE KOPPLUNG FÜR STANDROHRBAUGRUPPE
    COUPLAGE FLEXIBLE POUR ENSEMBLE DE TUBE VERTICAL


    Contributors:

    Publication date :

    2020-08-05


    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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