A hybrid VTOL drone is provided and comprises a minimum of four propellers fixedly mounted and disposed onto a frame that includes a pitch shaft, and a wing rotatably mounted to the pitch shaft, wherein the wing is rotatable around a pitch axis along the pitch shaft.


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    Title :

    Drag reduction


    Publication date :

    2020-10-21


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English



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