A coupling is disclosed for connecting a propeller to a motor in an aircraft such as a rotary wing aircraft and the like. The coupling comprises a propeller hub having an inner propeller hub bore defining an axial keyway. A rotatable shaft has an internal shaft bore connected for rotation with the motor. A radial key is slidably located in a radial aperture extending through the rotatable shaft. An actuator is slidably mounted within the internal shaft bore of the rotatable shaft. The radial key is received with the axial keyway for securing the propeller hub to the rotatable shaft. A depression of the actuator retracting the radial key relative to an outer surface of the rotatable shaft for permitting the propeller hub bore to be introduced onto the rotatable shaft.


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    Titel :

    QUICK DISCONNECT COUPLING FOR A PROPELLER


    Weitere Titelangaben:

    SCHNELLLÖSEKUPPLUNG FÜR EINEN PROPELLER
    ACCOUPLEMENT À DÉCONNEXION RAPIDE POUR HÉLICE


    Beteiligte:
    NILSON TIM (Autor:in) / NETHERY DANIEL (Autor:in) / HOLBROOK AUSTIN (Autor:in)

    Erscheinungsdatum :

    08.09.2021


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

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



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