A fuselage structure (100) and an unmanned aerial vehicle having same. The fuselage structure (100) comprises: a main fuselage (101); at least two main wings, the two main wings (102) being symmetrically arranged on two sides of the main fuselage (101), and the main wings (102) each being provided with a propeller (1022) and a motor for supplying power to the propeller (1022); an upper vertical tail wing (103), arranged at the upper end of the main fuselage (101); and a lower vertical tail wing (104), arranged at the lower end of the main fuselage (101).


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    Titel :

    Fuselage structure and unmanned aerial vehicle having same


    Beteiligte:
    WEI YANG (Autor:in) / CHUNPENG HE (Autor:in) / ZHILIANG ZHAO (Autor:in) / YI ZHANG (Autor:in) / XINGYANG TAN (Autor:in) / LIANG CHEN (Autor:in) / RUI DU (Autor:in) / PENG HU (Autor:in) / XIAOYUE LAI (Autor:in)

    Erscheinungsdatum :

    05.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Englisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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