The invention discloses a power device of an electric manned aircraft and the electric manned aircraft. The power device comprises a plurality of motor sets and a plurality of battery packs corresponding to the motor sets. One motor group comprises a plurality of motors, one battery pack comprises a plurality of batteries, and each battery in the battery pack is independently connected with the corresponding motor group so as to supply power to the plurality of motors in the motor group. According to the power device of the electric manned aircraft and the electric manned aircraft, the independent batteries in the battery pack are used for supplying power to the multiple motors in the motor set, the electric quantity of the multiple batteries in the battery pack can be balanced, the voltage difference of the multiple batteries is kept relatively stable, and normal and stable operation of the batteries is ensured.

    本申请公开了一种电动载人飞行器的动力装置和电动载人飞行器。动力装置包括多个电机组和与多个电机组对应的多个电池组。其中,一个电机组包括多个电机,一个电池组包括多个电池,电池组中的每个电池均独立与对应的电机组连接以向电机组内多个电机供电。本申请公开的电动载人飞行器的动力装置和电动载人飞行器中,通过使用电池组中单独的电池向电机组中的多个电机供电,能够平衡电池组中多个电池的电量,使得多个电池的电压差保持相对稳定,确保电池正常、稳定地运行。


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    Titel :

    Power device of electric manned aircraft and electric manned aircraft


    Weitere Titelangaben:

    电动载人飞行器的动力装置和电动载人飞行器


    Beteiligte:
    ZHAO DELI (Autor:in) / QUAN HONGFEI (Autor:in) / LI JIE (Autor:in) / WU HUIKANG (Autor:in)

    Erscheinungsdatum :

    2021-06-22


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64C AEROPLANES , Flugzeuge



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