The electric vertical take-off and landing aircraft comprises an aircraft body (2), a plurality of battery packs (1), a plurality of propellers (3) and a plurality of motors (4), the battery packs (1) are distributed at different positions of the aircraft body (2) and supply power to the motors (4) respectively, and the motors (4) drive the propellers (3) respectively so that take-off, landing and flying of the aircraft can be achieved. In the electric vertical take-off and landing aircraft, the plurality of battery packs are distributed at different parts of the aircraft and are close to the motors, and a single battery pack only supplies power to one or two specific motors. Even if a certain battery pack fails, other battery packs can still operate normally to supply power to the motors, and the rest motors drive the propellers to rotate, so that the flight safety of the aircraft is ensured.

    提供了一种电动垂直起降飞行器,其包括机体(2)、多个电池包(1)、多个螺旋桨(3)、多个电机(4),所述多个电池包(1)分布在所述机体(2)的不同位置,分别给所述多个电机(4)供电,由所述多个电机(4)分别驱动所述多个螺旋桨(3),以实现所述飞行器的起降及飞行。在本申请的电动垂直起降飞行器中,把多个电池包分布在飞行器的不同部位,且与电机临近,单个电池包仅对特定的一个或两个电机供电。即使某个电池包失效,其他电池包依然可以正常运行,给电机供电,通过剩余电机带动螺旋桨转动,保证飞行器的飞行安全。


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    Title :

    Electric vertical take-off and landing aircraft


    Additional title:

    电动垂直起降飞行器


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

    Publication date :

    2022-03-22


    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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