An aerial vehicle includes a fuselage supporting a pair of wings, with each of wings having a pair of booms attached thereto. A tilt rotor is positioned at each of the forward ends of each of the booms, to provide the aerial vehicle with at least four tilt rotors. A fixed rotor is positioned at and secured to the aft (or trailing) ends of each of the booms, to provide the aerial vehicle with at least four fixed rotors.


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    Titel :

    TILT ROTOR VERTICAL TAKE-OFF AND LANDING AERIAL VEHICLE


    Beteiligte:
    VILLA IAN ANDREAS (Autor:in) / KAWECKI JACEK (Autor:in) / DOHERTY JALEN CHRISTIAN (Autor:in) / NARU RYAN (Autor:in) / MOORE MARK (Autor:in) / GARY ALEX MICHAEL (Autor:in) / CHASE ADAM (Autor:in) / DERKACH MATTHEW WILLIAM (Autor:in) / HABAN PHILIPP (Autor:in)

    Erscheinungsdatum :

    19.09.2024


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen



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