A convertible aircraft system is provided that can convert to a helicopter configuration, an airplane configuration, or a gyroplane configuration before, during, or after flight. The convertible aircraft system includes a fuselage, a proximal flight assembly, a distal flight assembly, a support spar, and a tail assembly. The fuselage is the main structural body of the present invention. The proximal flight assembly and the distal flight assembly are the flight system of the present invention. The support spar provides an axis of rotation and a pole support for the proximal flight assembly and the distal flight assembly. The tail assembly provides stability during flight of the present invention. In more detail, the tail assembly may comprise at least one vertical stabilizer, at least one horizontal stabilizer, and at least one rudder in order to provide stability during flight of the present invention.


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    Titel :

    Convertible aircraft system


    Beteiligte:
    LI XINGKANG (Autor:in) / REN HENG (Autor:in) / LI QIANG (Autor:in) / LI XINGJIAN (Autor:in)

    Erscheinungsdatum :

    17.10.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



    Convertible Aircraft System

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    Berkowitz, S.M. / Barnaby, R.S. / Colcord, W.H. | Engineering Index Backfile | 1949


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    ZIMENSKAYA ELLINA VLADIMIROVNA | Europäisches Patentamt | 2017

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    Klemin, A. | Engineering Index Backfile | 1949