The invention relates to the technical field of aircrafts, in particular to an electric vertical take-off and landing aircraft which comprises a lift component 1, a cabin 2, an aircraft take-off and landing support frame 3, a power battery 4, an aircraft contour lamp 5 and a flight control system 6. The electric vertical take-off and landing aircraft can fly or hover and can take off and land vertically. Special airports, runways and parking aprons are not needed, so that the use cost is reduced; through electric driving, the carbon emission is obviously reduced; the structure is simple and compact, weight is light, and manufacturing difficulty is reduced; the rotor wings are internally arranged, so that the safety risk of external personnel is reduced.

    本发明涉及航空器技术领域,具体涉及一种电动垂直起降飞行器,包括:升力组件1、座舱2、飞行器起落支撑架3、动力电池4、飞行器轮廓灯5、飞行控制系统6;所述电动垂直起降飞行器能飞行或悬停,能垂直起降;不需要专门的机场、跑道和停机坪,减少使用成本;电驱动,显著减少碳排放量;结构简单紧凑、重量轻,降低制造难度;旋翼内置,降低外部人员安全风险。


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    Titel :

    Electric vertical take-off and landing aircraft


    Weitere Titelangaben:

    一种电动垂直起降飞行器


    Beteiligte:
    WANG SHUIHAO (Autor:in)

    Erscheinungsdatum :

    14.03.2025


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64U / B64C AEROPLANES , Flugzeuge



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