A long-distance drone is disclosed having a canard wing configuration with a cabin (270) attached to a left main wing (213) and a right main wing (214). There is a left forewing (211) and a right forewing (212) connected together to form a single-piece forewing. There is a left linear support (220) connecting the left forewing (211) to the left main wing (213), and a right linear support (221) connecting the right forewing (212) to the right main wing (214). A plurality of propellers is disposed on the left and the right linear supports (220, 221).


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    Title :

    HYBRID VTOL FIXED-WING AERIAL VEHICLE


    Additional title:

    HYBRIDES VTOL-LUFTFAHRZEUG MIT STARREN FLÜGELN
    VÉHICULE AÉRIEN À AILES FIXES VTOL HYBRIDE


    Contributors:
    YU TIAN (author)

    Publication date :

    2023-03-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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