An electric aircraft comprises: rotors for providing lift for vertical takeoff and landing of the aircraft; the rotating propellers can incline between a lifting configuration for providing lifting force for vertical takeoff and landing of the aircraft and a propelling configuration for providing forward thrust to the aircraft; the first battery pack is used for supplying power to the first rotor wing and the first rotating propeller; the second battery pack is used for supplying power to the second rotor wing and the second rotating propeller; the first power supply bus is used for electrically connecting the first battery pack to the first rotor wing and the first rotating propeller; and a second power bus electrically connecting the second battery pack to the second rotor and the second rotor paddle, where the second power bus is electrically isolated from the first power bus.

    一种电动飞行器包括:旋翼,所述旋翼用于提供用于所述飞行器的垂直起飞和着陆的升力;转桨,所述转桨能够在用于提供用于所述飞行器的垂直起飞和着陆的升力的提升配置与用于向所述飞行器提供向前推力的推进配置之间倾斜;第一电池组,所述第一电池组用于向第一旋翼和第一转桨供电;第二电池组,所述第二电池组用于向第二旋翼和第二转桨供电;第一电源母线,所述第一电源母线将所述第一电池组电连接到所述第一旋翼和所述第一转桨;以及第二电源母线,所述第二电源母线将所述第二电池组电连接到所述第二旋翼和所述第二转桨,其中所述第二电源母线与所述第一电源母线电隔离。


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    Titel :

    System and method for power distribution in electric aircraft


    Weitere Titelangaben:

    用于电动飞行器中的电力分配的系统和方法


    Beteiligte:

    Erscheinungsdatum :

    23.05.2023


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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