The invention provides an electric engine, an electric propulsion device and an aircraft, and relates to the technical field of aircrafts. The electric engine comprises a power motor, a fan and a radiator. The power motor is provided with a liquid cooling flow channel, and the liquid cooling flow channel and the radiator are used for forming a cooling medium circulation loop. The fan is provided with an air inlet side and an air outlet side in the axial direction of the fan, the power motor is located on the air inlet side of the fan, and the radiator is located on the air outlet side of the fan. The fan is provided with an air guide assembly, and the air guide assembly is used for guiding part of airflow on the air inlet side of the fan to the middle area of the fan and blowing the airflow to the radiator from the middle area of the fan. Therefore, the heat dissipation efficiency of the power motor is high, and the working performance of the power motor can be guaranteed.

    本申请提供一种电动发动机、电推进装置及飞行器,涉及飞行器技术领域。该电动发动机包括动力电机、风扇和散热器。动力电机具有液冷流道,液冷流道和散热器用于形成冷却介质循环回路。沿风扇的轴向,风扇具有进风侧和出风侧,动力电机位于风扇的进风侧,散热器位于风扇的出风侧。其中,风扇具有导风组件,导风组件用于将风扇进风侧的部分气流导向风扇的中部区域、并从风扇的中部区域吹向散热器。这样,动力电机的散热效率较高,利于保证动力电机的工作性能。


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    Title :

    Electric engine, electric propulsion device and aircraft


    Additional title:

    电动发动机、电推进装置及飞行器


    Contributors:
    GUO LIANG (author) / LI QING (author) / SONG JIANBO (author) / YI LIJIE (author) / GONG ZHENG (author)

    Publication date :

    2024-12-27


    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 / F04D Strömungsarbeitsmaschinen , NON-POSITIVE-DISPLACEMENT PUMPS / H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES



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