An aircraft includes a fuselage including a front portion and a tail, the fuselage having a longitudinal axis, rotation about which is roll rotation, a lateral axis, rotation about which is pitch rotation, and a vertical axis, rotation about which is yaw rotation. The tail is substantially in one horizontal plane and has a lateral cross section shape of an airfoil. The aircraft includes at least one wing coupled to the fuselage, an engine pivotally coupled to the aircraft so that the engine is pivotable in the yaw rotation, and an actuator coupled to the engine arranged to pivot the engine in the yaw rotation.


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    Titel :

    TRANSFORMABLE TYPE VTOL AIRCRAFT


    Beteiligte:
    SHWARTZ SHAUL (Autor:in) / SHWARTZ AVIV (Autor:in)

    Erscheinungsdatum :

    08.05.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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