The embodiment of the invention discloses a longitudinal combined type multi-rotor aircraft for a plateau environment, relates to the technical field of modular multi-rotor aircrafts, and can perform corresponding aircraft type structure recombination according to different transportation target weights of the aircraft. Wherein the nose module, the fuselage module group and the rotor units are taken as a main body. And a main control panel and an aviation battery for the operation of the main control panel and the rotor units on the two sides are arranged in the nose module. The main control panel is connected with the fuselage module group and the rotor units through aviation plugs, and the fuselage structure is fixed with the fuselage module group and the rotor units on the two sides through connecting mechanisms. Each rotor wing unit is internally provided with an independent motor and a transmission rod piece. An auxiliary control panel and a corresponding model airplane battery are placed in the fuselage module group, and two sides of each fuselage module can be respectively connected with two rotor wing units. The structure of the aircraft can be conveniently and freely adjusted according to load requirements.

    本发明实施例公开了一种用于高原环境的纵向组合式多旋翼飞行器,涉及模块化多旋翼飞行器技术领域,可以根据飞行器的运输目标重量不同进行相应的机型结构重组。其中以机头模块,机身模块组以及旋翼单元三部分为主体。在机头模块内部放置主控制面板以及供主控制面板以及两侧旋翼单元运转的航空电池。主控制面板通过航空插头连接机身模块组及旋翼单元,机体结构通过连接机构与机身模块组和两侧的旋翼单元进行固定。每个旋翼单元内置独立的电机及传动杆件。机身模块组内部放置副控制面板以及对应的航模电池,每个机身模块两侧也可分别连接两个旋翼单元。可以方便得根据载重需求自由调节飞行器结构。


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    Title :

    Longitudinal combined type multi-rotor aircraft for plateau environment


    Additional title:

    一种用于高原环境的纵向组合式多旋翼飞行器


    Contributors:
    WU YANG (author) / HAN DONG (author) / FENG NIANZHENG (author)

    Publication date :

    2023-08-08


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U



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