The present invention provides an aircraft described as an Airborne Urban Mobility Vehicle with VTOL (Vertical Take-Off and Landing) capability. The aircraft has a 5 fuselage freely pivoted between lateral arms of a yoke; the arms of the yoke extending fore and aft and, at or towards the extremities of the arms: the respective fore portions are linked laterally together by an aerofoil; and the respective aft portions are linked laterally together by an aerofoil; and at least one of the fore and aft aerofoils having mounted thereon one or more propulsion units.


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    Titel :

    TANDEM WING TAIL-SITTING AIRCRAFT WITH TILTING BODY


    Beteiligte:
    DIDEY ARNAUD (Autor:in)

    Erscheinungsdatum :

    08.10.2020


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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