An aircraft includes an onboard power supply, an empennage assembly, and a horizontal main wing each connected to a fuselage, and a vertical cross-wing arranged orthogonally with respect to the main wing. Flight control surfaces are arranged on the empennage assembly, vertical cross-wing, and horizontal main wing. A distributed propulsion system includes a first pair of propellers connected to the horizontal main wing and a second pair of propellers connected to the vertical cross-wing. Each of the propellers is connected to and powered by the power supply. Each propeller forms an acute canting angle with respect to an axis of the particular horizontal main wing or the vertical cross-wing to which the propeller is connected. The flight modes may include vertical takeoff and landing (VTOL), hover mode, rapid descent, and forward and backward flight modes. The propellers are unpowered during the rapid descent mode.


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    Titel :

    VTOL AIRCRAFT CAPABLE OF FLYING FORWARD AND BACKWARD


    Beteiligte:
    GEUTHER STEVEN C (Autor:in) / NORTH DAVID D (Autor:in) / DUVALL BRIAN E (Autor:in) / SCHAEFER JACOB R (Autor:in)

    Erscheinungsdatum :

    14.11.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U



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