Rotating shroud for rotator blade systems

    公开(公告)号:US11407493B2

    公开(公告)日:2022-08-09

    申请号:US17464499

    申请日:2021-09-01

    Inventor: Morteza Gharib

    Abstract: 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.

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