The invention discloses a folding quick-disassembling type multi-rotary wing unmanned aerial vehicle which comprises a stander unit, a flight unit, a replenishment unit and a spray unit, wherein the stander unit comprises a stander main body and an undercarriage; the flight unit comprises a plurality of flight assemblies which are distributed along the peripheral direction of the main stander body; each flight assembly comprises a jib arm, a rotary wing and a drive motor; the jib arm is connected with the stander main body through a folding connection structure which can be folded along a top-bottom direction; the replenishment unit is an integer combined by an energy replenishing part and a feed liquid replenishing part, the replenishment unit can be connected with the stander main body through an assembling and disassembling connection structure, and the assembling and disassembling connection structure comprises a buckle which can be buckled and unbuckled with the connecting part of the stander main body; and the spray unit is connected with the stander main body and connected with the feed liquid replenishing part of the replenishment unit. The folding quick-disassembling type multi-rotary wing unmanned aerial vehicle disclosed by the invention is not only easy to carry and transport, but also short in replenishing time of energy and a sprayed material and high in working efficiency.


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    Title :

    Folding quick-disassembling type multi-rotary wing unmanned aerial vehicle


    Contributors:
    ZHOU ZHIYAN (author) / ZHU QIUYANG (author) / CHEN SHENGDE (author) / ZANG YU (author) / LUO XIWEN (author) / ZANG YING (author) / LI JIYU (author) / LAN YUBIN (author)

    Publication date :

    2015-04-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    English


    Classification :

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



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