A rotor assembly including a fixed fairing including an interface portion and a hub fairing including a depression. The depression is configured to receive at least a portion of the interface portion. The hub fairing is rotatable relative to the fixed fairing.


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    Title :

    AERODYNAMIC ROTARY INTERFACE



    Publication date :

    2023-12-07


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge






    Forebody Aerodynamic Loads Due to Rotary Motion

    Iwanski, Kenneth / Nelson, Robert | AIAA | 2002