A system and method for improving the flight control and efficiency of an aerial vehicle. Many embodiments are directed to a rotor-shroud assembly system where a plurality of rotor blades are connected to the internal side of a shroud and are set up to pivot through the use of a pitching mechanism. The entire assembly is configured to rotate when attached to a motor.


    Access

    Download


    Export, share and cite



    Title :

    Rotating shroud for rotator blade systems


    Contributors:

    Publication date :

    2022-08-09


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



    Rotating Shroud for Rotator Blade Systems

    GHARIB MORTEZA | European Patent Office | 2023

    Free access

    ROTATING SHROUD FOR ROTATOR BLADE SYSTEMS

    GHARIB MORTEZA | European Patent Office | 2022

    Free access

    Rotating Shroud for Rotator Blade Systems

    GHARIB MORTEZA | European Patent Office | 2022

    Free access

    Turbine Blade Platform, Blade Tip and Shroud Heat Transfer

    Dunn, M. G. / Kim, J. / International Society for Air Breathing Engines; Australian Committee | British Library Conference Proceedings | 1995


    Turbine blade platform, blade tip and shroud heat transfer

    Dunn, M.G. / Kim, J. | Tema Archive | 1995