The invention discloses a ducted fan-wing unmanned aerial vehicle capable of taking off and landing vertically and a control method thereof. The ducted fan-wing unmanned aerial vehicle comprises a fuselage, a communication module and a control module. An electronic pod and an undercarriage are arranged below the head of the fuselage, fan wings are symmetrically arranged on the two sides of the fuselage, and the tail of the fuselage is connected with a horizontal tail; ducted fans capable of rotating along a horizontal transverse shaft are symmetrically arranged on the two sides of the horizontal tail; the two fan wings each comprise a plurality of driving assemblies, and every two adjacent driving assemblies are spaced through a partition plate; the driving assembly comprises a rotating shaft arranged between the two partition plates in a penetrating mode and a plurality of cross-flow fans. The cross-flow fans are evenly distributed on the rotating shaft in a cylindrical shape. The rotating shaft is connected with a reduction gear which is sequentially connected with a transmission gear and a motor through a belt.
本发明公开了一种可垂直起降的涵道扇翼无人机及其控制方法,包括机身、通信模块和控制模块;位于所述机身头部的下方设置电子吊舱和起落架,机身两侧对称设置扇翼,机身尾部与平尾相连;平尾两侧对称设置可沿水平横轴旋转的涵道风扇;两个扇翼均包括若干个驱动组件,相邻驱动组件之间通过隔板间隔隔开;驱动组件包括穿设于两个隔板之间的转动轴和若干片横流风扇,若干片横流风扇呈圆柱状均匀分布于转动轴上;转动轴与减速齿轮连接,减速齿轮通过皮带依次与传动齿轮和电动机相连。
Ducted fan-wing unmanned aerial vehicle capable of vertically taking off and landing and control method thereof
一种可垂直起降的涵道扇翼无人机及其控制方法
2021-07-16
Patent
Elektronische Ressource
Chinesisch
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