The invention provides a tailstock type vertical take-off and landing unmanned aerial vehicle. The tailstock type vertical take-off and landing unmanned aerial vehicle comprises a fuselage, wings, a connecting assembly and a ducted propeller variable thrust system. The ducted propeller variable thrust system is located at the tail of the fuselage and connected with the fuselage through the connecting assembly. The ducted propeller variable thrust system is used for generating thrust needed by flight of the unmanned aerial vehicle and changing the direction of the thrust. The ducted propeller variable thrust system comprises a duct, a support, an energy supply piece, a power assembly and a direction adjusting piece. According to the vertical take-off and landing high-speed unmanned aerial vehicle, the ducted propeller variable thrust system is arranged at the tail of the vehicle body, the tailstock type design is achieved, the vertical take-off and landing function of the vertical take-off and landing high-speed unmanned aerial vehicle can be achieved, a take-off and landing runway or accessory devices such as ejection and recovery are not needed, the deployment time is short, and site limitation is avoided; the system can be deployed on hills, mountains and urban streets with complex terrains, and even on small surface ships and submarines.
本发明提供了一种尾座式垂直起降无人机。所述尾座式垂直起降无人机,包括机身、机翼、连接组件以及涵道螺旋桨变推力系统;所述涵道螺旋桨变推力系统位于所述机身尾部,且通过所述连接组件与所述机身连接;所述涵道螺旋桨变推力系统用于产生无人机飞行所需的推力,以及改变所述推力的方向。所述涵道螺旋桨变推力系统包括涵道、支架、供能件、动力组件与方向调节件;本发明采用通过将涵道螺旋桨变推力系统设置在机身的尾部,实现尾座式设计,能够实现垂直起降高速无人机具有垂直起降功能,因此不需要起降跑道,或者弹射和回收等附属装置,部署时间短,不受场地限制,可以部署在地形复杂的丘陵山地和城市街道,甚至是小型水面舰艇和潜艇上。
Tailstock type vertical take-off and landing unmanned aerial vehicle
尾座式垂直起降无人机
2022-12-27
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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