An unmanned aerial vehicle load mounting structure disclosed by the present invention comprises a fuselage, a load and a locking assembly, the load can be mounted on the fuselage through the locking assembly, the fuselage is provided with a first switching circuit board, the first switching circuit board is in communication connection with a function module on the fuselage, the load is provided with a second switching circuit board, and the second switching circuit board is in communication connection with the function module on the fuselage. The second switching circuit board is in communication connection with a functional module on the load, the first switching circuit board is provided with a first connecting terminal, and the second switching circuit board is provided with a second connecting terminal. And the first connecting terminal and the second connecting terminal are in plug-in fit so as to realize communication connection between the machine body and the function module on the load. According to the load connection structure provided in the scheme, communication connection between the function module on the load and the function module on the machine body can be rapidly achieved while the load and the machine body are fixed, the load can be controlled through the control module on the load, and the power source located on the machine body can supply power to work.

    本发明公开一种无人机负载安装结构,包括机身、负载以及锁持组件,负载可通过锁持组件安装在机身上,机身上设置有第一转接电路板,第一转接电路板与机身上的功能模块通信连接,负载上设置有第二转接电路板,第二转接电路板与负载上的功能模块通信连接,第一转接电路板上设置有第一连接端子,第二转接电路板上设置有第二连接端子,当负载安装与机身,第一连接端子与第二连接端子插接配合以实现机身与负载上的功能模块之间的通信连接。本方案中提供的负载连接结构,在实现负载与机身的固定的同时能够快速实现负载上的功能模块与机身上的功能模块的通讯连接,使得负载可通过上的控制模块进行控制,且可由位于机身上的电源进行供电而进行工作。


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    Title :

    Unmanned aerial vehicle load mounting structure and unmanned aerial vehicle


    Additional title:

    一种无人机负载安装结构及无人机


    Contributors:
    LI ZHIYONG (author) / DING ZUOJUN (author)

    Publication date :

    2023-06-16


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge / B64U / H01R Elektrisch leitende Verbindungen , ELECTRICALLY-CONDUCTIVE CONNECTIONS



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