A reconfigurable hybrid Vertical Takeoff and Landing (VTOL) vehicle includes a turntable bearing coupling a conventional wing to a fuselage. The fuselage, designed to couple to and release a cargo pod from its undercarriage, is configured to accept a high wing juncture such that the wing can rotate from a flight configuration to a transport configuration. The transport configuration aligns the wing with the fuselage sufficient to enable the hybrid VTOL vehicle to fit within a standard intermodal container or transport aircraft.


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    Titel :

    RECONFIGURABLE HYBRID VTOL SYSTEM


    Beteiligte:
    WEEKES TERIK (Autor:in) / BELARDO SEAN (Autor:in) / MERRILL DAVID (Autor:in) / COPE CLINT (Autor:in) / HILLS SHANE (Autor:in)

    Erscheinungsdatum :

    2021-04-15


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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