The invention relates to the technical field of unmanned aerial vehicles, and in particular relates to a torch transmission unmanned aerial vehicle. The torch transmission unmanned aerial vehicle comprises a rotor wing unmanned aerial vehicle, a torch tilting mechanism, a battery balance weight system and a torch, the rotor wing unmanned aerial vehicle is of a four-rotor-wing structure, the battery balance weight system is arranged in the rotor wing unmanned aerial vehicle, the torch tilting mechanism is arranged on the outer side of the rotor wing unmanned aerial vehicle, the torch is installed on the torch tilting mechanism, and tilting action is achieved through driving of the torch tilting mechanism. The functions that the unmanned aerial vehicle is high in load ratio, rotor wing downwash airflow does not influence torch flames, and torch postures do not influence the gravity center balancing characteristic of the whole vehicle can be achieved.

    本发明涉及无人机技术领域,特别涉及一种火炬传递无人机。包括旋翼无人机、火炬倾转机构、电池配重系统及火炬,其中旋翼无人机采用四旋翼构型,电池配重系统布置于旋翼无人机内,火炬倾转机构设置于旋翼无人机的外侧,火炬安装在火炬倾转机构上,并且通过火炬倾转机构的驱动实现倾转动作。本发明可实现无人机高载重比、旋翼下洗气流不影响火炬火焰以及火炬姿态不影响整机重心配平特性等功能。


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    Titel :

    Torch transmission unmanned aerial vehicle


    Weitere Titelangaben:

    一种火炬传递无人机


    Beteiligte:
    HE YUQING (Autor:in) / YANG LIYING (Autor:in) / LI SILIANG (Autor:in) / MA LIXIN (Autor:in) / HUANG CHAOXIONG (Autor:in) / CHANG YANCHUN (Autor:in) / ZHANG YUANHANG (Autor:in)

    Erscheinungsdatum :

    2021-02-09


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

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



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