A vertical take-off and landing (VTOL) aircraft is provided. The aircraft includes a wing, nacelles supportively disposed at opposite ends of the wing, proprotors respectively attached to each of the nacelles with each of the proprotors being rotatable to generate lift in vertical flight and thrust in horizontal flight and a delta-wing shaped fuselage disposed along the wing between the nacelles.


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    Titel :

    Delta fuselage for vertical take-off and landing (VTOL) aircraft


    Beteiligte:
    ALBER MARK R (Autor:in) / GAYAGOY CHARLES (Autor:in)

    Erscheinungsdatum :

    21.01.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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