The invention discloses a vertical take-off and landing and horizontal flight all-electric aircraft which comprises an aircraft body, wings, power columns, an empennage and a battery, during take-off and landing, a tilting mechanism controls the power columns to be in the vertical direction, a first power device drives propellers to rotate, lift force is provided, and vertical take-off and landing are achieved; the tilting mechanism controls the power columns to gradually turn into the horizontal direction, thrust is provided, horizontal flight is achieved, no runway is needed during vertical take-off and landing, the requirement for take-off and landing environment conditions is lowered, when a certain first power device breaks down and cannot work, the other first power device on the same power column can improve power and keep power balance, and the power balance is kept. And stable, normal and safe flight is ensured.

    本发明公开了一种垂直起降水平飞行全电飞机,包括机身、机翼、动力柱、尾翼和电池,通过在起飞和降落时,倾转机构控制动力柱转为竖直方向,第一动力装置带动螺旋桨转动,提供升力,实现垂直起降,当垂直起飞到预定高度,倾转机构控制动力柱逐渐转为水平方向,提供推力,实现水平飞行,垂直起降时无需跑道,降低了对起降环境条件的要求,当某个第一动力装置出现故障而无法工作时,同一个动力柱上的另一个第一动力装置能提高功率,保持动力的平衡,保证飞行平稳、正常和安全。


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    Titel :

    Vertical take-off and landing and horizontal flight all-electric aircraft


    Weitere Titelangaben:

    垂直起降水平飞行全电飞机


    Beteiligte:
    DENG XIAOLONG (Autor:in) / HOU ZHONGXI (Autor:in) / GUO ZHENG (Autor:in) / MA ZHENYU (Autor:in) / WANG YUJIE (Autor:in) / YANG XIXIANG (Autor:in) / ZHU BINGJIE (Autor:in) / GAO XIANZHONG (Autor:in) / FAN ZHENG (Autor:in)

    Erscheinungsdatum :

    2022-07-01


    Medientyp :

    Patent


    Format :

    Elektronische Ressource


    Sprache :

    Chinesisch


    Klassifikation :

    IPC:    B64C AEROPLANES , Flugzeuge



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