The invention relates to a vertical take-off and landing electric aircraft, and belongs to the technical field of flight equipment. The aircraft comprises a fuselage, and a first electric rotor system is mounted at the tail of the fuselage; first fixed wings and second fixed wings are fixedly arranged on two sides of the fuselage, the first fixed wings are positioned between the middle part of the fuselage and the tail, and the second fixed wings are positioned between the front part of the fuselage and the nose; mounting holes are formed in the first fixed wing and the second fixed wing, and each second electric rotor system is mounted in the corresponding mounting hole; hole openings in the upper end and the lower end of each mounting hole are covered with the cover plates; the driving systems are mounted on the first fixed wing and the second fixed wing, and the power output ends of the driving systems are connected with the cover plate so as to drive the cover plate to open and close the opening of the mounting hole. The aircraft with the structure is more suitable for urban traffic, and direction control is easier.

    本发明涉及一种垂直起降电动飞行器,属于飞行设备技术领域。该飞行器包括机身,机尾安装有第一电动旋翼系统;机身的两侧均固设有第一固定翼和第二固定翼,第一固定翼位于机身的中部和机尾之间,第二固定翼位于机身的前部和机头之间;第二电动旋翼系统,第一固定翼和第二固定翼上均开设有安装孔,每个安装孔中安装均安装有第二电动旋翼系统;盖板,每个安装孔的上下两端孔口处均盖合有盖板;驱动系统,第一固定翼和第二固定翼上均安装有驱动系统,驱动系统的动力输出端与盖板相连以用于驱动盖板启闭安装孔的孔口。该结构的飞行器更加适合城市通行,并且方向控制更加容易。


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    Title :

    Vertical take-off and landing electric aircraft


    Additional title:

    一种垂直起降电动飞行器


    Contributors:
    LI BOWEN (author)

    Publication date :

    2022-11-04


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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