The invention belongs to the technical field of electric aircrafts, and particularly relates to a multi-battery-module electric aircraft power system and an electric aircraft. The multi-battery-moduleelectric aircraft power system comprises a motor, a propeller, a plurality of battery modules, a battery management system and an aircraft power control system. The aircraft power control system is electrically connected with the battery management system, the motor and the plurality of battery modules through buses. The battery management system is electrically connected with the motor. The motor is connected with the propeller. The invention further relates to an electric aircraft with the multi-battery-module power system. According to the aircraft power control system, the battery management system controls the multiple battery modules arranged at different parts of the electric aircraft to supply power to the motor, the motor drives the propeller coaxially connected with the motor torotate to provide flight power, and the aircraft power control system has the characteristics of high safety, good controllability, high carrying capacity, good comfort and high use efficiency.

    本发明属于电动飞机技术领域,具体而言,涉及一种多电池模组电动飞机动力系统和电动飞机,多电池模组电动飞机动力系统包括电机、螺旋桨、多个电池模组、电池管理系统和飞机动力控制系统;所述飞机动力控制系统通过总线与所述电池管理系统、所述电机、多个所述电池模组电连接;所述电池管理系统与所述电机电连接;所述电机与所述螺旋桨相连。本发明还涉及一种具有多电池模组动力系统的电动飞机。本发明的飞机动力控制系统通过电池管理系统控制多个在电动飞机的不同部位部署的电池模组为电机供电,电机带动与之同轴连接的螺旋桨转动提供飞行动力,具有安全性强、操控性好、载运能力强、舒适性好、使用效率高的特点。


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    Title :

    Multi-battery-module electric aircraft power system and electric aircraft


    Additional title:

    多电池模组电动飞机动力系统和电动飞机


    Contributors:
    GAO HONGJIANG (author) / DU MINGHUAN (author)

    Publication date :

    2020-05-22


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

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



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