The invention belongs to the field of electric propulsion system motor driving, and particularly relates to a motor and controller integrated device for eVTOL. Comprising an integrated heat dissipation fan assembly, a motor assembly and a controller assembly, a motor and controller integrated heat dissipation scheme is adopted, forced air cooling heat dissipation is conducted on the controller through a motor integrated fan, the design of a cooling system is simplified, and the power-to-weight ratio is effectively increased. And meanwhile, the motor controller and the motor adopt coaxial equal-outer-diameter design, and the characteristics of high power density and high volume density are very suitable for being applied to an eVTOL aircraft electric propulsion system.

    本发明属于电推进系统电机驱动领域,具体涉及一种用于eVTOL的电机与控制器一体化装置。包括:集成化散热风扇总成、电机总成以及控制器总成,采用了电机与控制器一体化散热方案,通过利用电机集成风扇为控制器进行强制风冷散热,简化了冷却系统设计,有效提高功重比。同时电机控制器与电机采用同轴等外径设计,高功率密度及高体积密度的特性非常适用于eVTOL飞行器电推进系统的应用。


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    Titel :

    Motor and controller integrated device for eVTOL


    Weitere Titelangaben:

    一种用于eVTOL的电机与控制器一体化装置


    Beteiligte:
    WANG HUIBO (Autor:in) / CAO BOYU (Autor:in) / WU JING (Autor:in) / SUN YUWEI (Autor:in) / SONG ZHENZHEN (Autor:in)

    Erscheinungsdatum :

    04.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    H02K Dynamoelektrische Maschinen , DYNAMO-ELECTRIC MACHINES / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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