The invention relates to a power system of a multi-rotor unmanned aerial vehicle, and the power system comprises a pipe clamping seat which comprises an outer shell and a carbon pipe installation seat installed in the outer shell; the carbon tube mounting seat is provided with a hollow mounting through hole; the carbon tube inner support comprises an inner support tube body and a horizontal positioning boss; the horizontal positioning boss is connected to the outer side of the inner supporting pipe body. The horizontal positioning boss is connected with the carbon tube mounting seat, so that an assembly gap is formed between the inner supporting tube body and the mounting via hole; the end part of the carbon tube is provided with a horizontal positioning groove; the carbon tube is inserted into the assembly gap, and the horizontal positioning groove is clamped with the horizontal positioning boss; after the carbon tube mounting seat, the carbon tube inner support and the carbon tube are connected, the carbon tube is clamped by the carbon tube mounting seat and the carbon tube inner support; the motor is connected to the side face of the pipe clamping base. The stress area of the carbon tube can be increased, so that the carbon tube is uniformly stressed, and the phenomenon of clamping explosion of the carbon tube is avoided.
本申请涉及一种多旋翼无人机的动力系统,包括:管夹座,包括外壳体、以及安装于外壳体内部的碳管安装座;所述碳管安装座设有中空式的安装过孔;碳管内撑,包括内撑管体和水平定位凸台;所述水平定位凸台连接于内撑管体外侧;所述水平定位凸台与碳管安装座连接,使内撑管体与安装过孔之间形成装配间隙;碳管,端部设有水平定位槽;所述碳管插入装配间隙内,且水平定位槽与水平定位凸台卡合;碳管安装座、碳管内撑、碳管三者连接后由碳管安装座、碳管内撑夹紧碳管;电机,连接于管夹座的侧面。本发明能够增大碳管受力面积,使碳管受力均匀,杜绝夹爆碳管的现象。
Power system of multi-rotor unmanned aerial vehicle
一种多旋翼无人机的动力系统
2024-09-13
Patent
Electronic Resource
Chinese
IPC: | B64U |
Multi-rotor unmanned aerial vehicle and multi-rotor unmanned aerial vehicle system
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