A vertical takeoff and landing (VTOL) light aircraft comprising: a tilt-wing comprising port and starboard wings; a power train having: an electric motor coupled to a rotor for providing the aircraft with thrust for flight mounted to each of the port and starboard wings; a battery configured to store electric energy to power the electric motors; an electric generator, and a combustion engine configured to drive the generator to produce electric energy for storage in the battery; and a controller configured to autonomously control the tilt-wing and power train to provide VTOL takeoffs and landing having relatively short hover periods.


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    Titel :

    VERTICAL TAKEOFF AND LANDING LIGHT AIRCRAFT


    Beteiligte:
    SHAFIR YEHUDA (Autor:in)

    Erscheinungsdatum :

    30.01.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge