The invention provides a heat dissipation structure for an electric vertical take-off and landing aircraft and the electric vertical take-off and landing aircraft. The heat dissipation structure comprises a machine body (1); the motor (2) is connected to the machine body (1); the lifting paddle (3) is driven by the motor (2); the motor controller (4) is arranged in the machine body (1) and is used for adjusting the rotating speed of the motor (2); and the ventilation assembly (5) is connected to the machine body (1), so that airflow generated by the lifting paddle (3) can flow through the motor controller (4) and flow out of the machine body (1) so as to cool the motor controller (4). By the adoption of the technical scheme, air resistance can be reduced, and meanwhile heat dissipation is more efficient.

    提供了一种用于电动垂直起降飞行器的散热结构及电动垂直起降飞行器。该散热结构包括:机体(1);电机(2),该电机(2)连接到所述机体(1);升桨(3),该升桨(3)由所述电机(2)驱动;电机控制器(4),该电机控制器(4)设于所述机体(1)的内部,用于对所述电机(2)的转速进行调节;以及通风组件(5),该通风组件(5)连接到所述机体(1),使所述升桨(3)产生的气流能够流过所述电机控制器(4)并流出所述机体(1),以对所述电机控制器(4)进行冷却。通过采用上述技术方案,能够在减小空气阻力的同时,更加高效地散热。


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    Title :

    Heat dissipation structure and electric vertical take-off and landing aircraft


    Additional title:

    散热结构及电动垂直起降飞行器


    Contributors:
    CHEN XIUXIAN (author) / WANG CHUNQIANG (author) / WANG DONGFANG (author) / JIANG HUAYI (author) / DANG TIEHONG (author) / DONG MING (author)

    Publication date :

    2022-05-06


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    H05K PRINTED CIRCUITS , Gedruckte Schaltungen / B64C AEROPLANES , Flugzeuge / B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT



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