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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    Titel :

    Drag reduction


    Erscheinungsdatum :

    21.10.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



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