The invention discloses a long shaft type vector multi-rotor aircraft structure. Comprising a tilting motor 1, a landing pipe sleeve 2, a lamp strip 3, a rotor 4, a main lifting motor 5, a motor fixing plate 6, a landing carbon pipe 7, a rear tilting steering engine structure 8, an electric speed controller 9, a main control board 10, an upper-layer clamping plate 11, a main rod 12, a lower-layer clamping plate 13, an inclined tee joint 14, a clamping plate pipe clamp 15, an inclined foot stand 16, a regular tee joint 17, a landing carbon rod 18, a steering engine shaft clamping arm 20, a bearing 21, a steering engine 22 and a tilting carbon rod 23. According to the invention, the conversion of the flight mode of the unmanned aerial vehicle and the redistribution of the power device are realized through the movement of the tilting mechanism, and the structural redundancy that a traditional linear multi-rotor unmanned aerial vehicle needs an attitude adjusting rod is avoided.

    本发明公开了一种长轴型矢量多旋翼飞行器结构,包括倾转电机1、降落管套2、灯带3、旋翼4、主升电机5、电机固定板6、降落碳管7、后倾转舵机结构8、电调9、主控板10、上层夹板11、主杆12、下层夹板13、斜三通14、夹板管夹15、斜脚架16、正三通17、落地碳杆18、舵机轴夹臂20、轴承21、舵机22、倾转碳杆23;本发明通过倾转机构的运动实现无人机的飞行模式的转变和动力装置的重新分布,避免了传统直线型多旋翼无人机需要姿态调整杆的结构冗余。


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    Title :

    Long-axis vector multi-rotor aircraft structure


    Additional title:

    一种长轴型矢量多旋翼飞行器结构


    Contributors:
    SHEN YUE (author) / CHU JINCHENG (author) / SHI ZHIXIANG (author) / LIU MINGHUI (author) / ZHANG LINGFEI (author)

    Publication date :

    2022-06-03


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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