The invention provides a cantilever unmanned aerial vehicle liquid cooling system, which comprises a liquid pump, a liquid cooling pipe and a calculation module, and is characterized in that the liquid pump is arranged on a fuselage of a cantilever unmanned aerial vehicle and drives cooling liquid to be injected into the liquid cooling pipe; the liquid cooling pipe is arranged on a cantilever of the cantilever unmanned aerial vehicle and is connected with the liquid pump and a propeller motor of the cantilever unmanned aerial vehicle, and the propeller motor adopts liquid immersion type or spraying type liquid cooling; and the calculation module collects the motor power of the propeller motor, calculates target power according to the motor power, and adjusts the liquid pump power of the liquid pump according to the target power. The immersion liquid cooling motor is adopted, the temperature of a motor coil is effectively reduced through direct contact of cooling liquid and a heating source, and stability of the unmanned aerial vehicle in the operation process is guaranteed.

    本申请提供一种悬臂无人机液冷系统,其中所述系统包括:液体泵、液冷管以及计算模块,其中,所述液体泵,布置在悬臂无人机的机身,驱动冷却液注入所述液冷管;所述液冷管,布置在悬臂无人机的悬臂,连接所述液体泵与所述悬臂无人机的螺旋桨电机,且所述螺旋桨电机采用浸液式或喷淋式液冷;所述计算模块,采集所述螺旋桨电机的电机功率,根据所述电机功率计算目标功率,并根据所述目标功率调整所述液体泵的液体泵功率。采用的浸液式液冷电机,通过冷却液与发热源的直接接触,有效降低电机线圈温度,保证无人机在运行过程中的稳定。


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    Title :

    Cantilever unmanned aerial vehicle liquid cooling system


    Additional title:

    一种悬臂无人机液冷系统


    Contributors:
    WANG ZIQUAN (author)

    Publication date :

    2025-02-18


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64U / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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