The invention provides a layout of an unmanned aerial vehicle capable of vertically taking off and landing. The unmanned aerial vehicle comprises a fuselage, wings mounted on two sides of the fuselage, and an undercarriage mounted at the bottom of the fuselage; cavities are formed in the wings; an air inlet communicated with the cavity is formed in the end, away from the fuselage, of each wing; anair extractor is installed in the fuselage; the air extraction end of the air extractor is communicated with the cavities; the air outflow end of the air extractor is connected with an air outflow channel which extends to the exterior of the fuselage and blows air towards the lower surfaces of the wings; mounting plates extending in the axis direction of the fuselage are mounted at the bottoms ofthe wings; and lifting wing power assemblies are mounted at the tops of the two ends of the mounting plates correspondingly; the sides, facing the tail of the fuselage, of the wings are sunken inwards to form air flow grooves; a propulsion wing power assembly is installed at the tail of the fuselage; and at least part of air blown out by the propulsion wing power assembly flows through the air flow grooves. The pneumatic layout is reasonable and can facilitate lifting and advancing.

    本发明提供了一种可垂直起降无人机的布局,包括机身,安装在所述机身两侧的机翼,以及安装在所述机身底部的起落架,所述机翼内部具有空腔,且所述机翼远离所述机身的端部设置有与所述空腔连通的进气口,所述机身内部安装有抽气装置,所述抽气装置的抽气端与所述空腔连通,且所述抽气装置的出气端连接有延伸至所述机身外部并朝所述机翼下表面吹气的出风道;所述机翼底部安装有沿所述机身轴线方向延伸的安装板,所述安装板的两端顶部分别安装有升降翼动力组件;所述机翼朝向所述机身尾部的一侧向内凹陷成风流槽,所述机身尾部安装有推进翼动力组件,所述推进翼动力组件吹出的风至少部分流经所述风流槽。本申请气动布局合理,有助于起升和行进。


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    Title :

    Layout of unmanned aerial vehicle of unmanned aerial vehicle capable of vertically taking off and landing


    Additional title:

    一种可垂直起降无人机的布局


    Contributors:
    WANG CHUAN (author)

    Publication date :

    2020-08-11


    Type of media :

    Patent


    Type of material :

    Electronic Resource


    Language :

    Chinese


    Classification :

    IPC:    B64C AEROPLANES , Flugzeuge



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