The invention discloses a modularized vertical take-off and landing fixed-wing unmanned aerial vehicle. The unmanned aerial vehicle comprises a fuselage, two wings and an empennage, wherein a first propeller for providing horizontal traction force is arranged at a front end of the fuselage, a power supply cabin is arranged at the position, close to the first propeller, of the top of the fuselage, and a control cabin is arranged at the position, close to a rear end, of the top of the fuselage; the bottom of the fuselage is detachably connected with a task hanging bin used for carrying different task modules, and the top of the fuselage is in threaded connection with two antenna rods; the two wings are symmetrically arranged and detachably connected to the two sides of the fuselage, and each wing is provided with a second propeller for providing vertical traction force; and the empennage is detachably connected with a rear end of the fuselage. The unmanned aerial vehicle has advantages of a fixed wing unmanned aerial vehicle and a rotor wing unmanned aerial vehicle, the fuselage, the wings and the empennage can be quickly disassembled and assembled and are easy to store and transport, a task pod can be matched with various task loads, the unmanned aerial vehicle can be used for multiple purposes, and in addition, the empennage can be replaced according to task requirements to adapt to different complex geographical environments.
本发明公开了一种模块化垂直起降固定翼无人机,包括:机身,其前端设有提供水平牵引力的第一螺旋桨,机身顶部靠近第一螺旋桨的位置设有电源舱,机身顶部靠近其后端位置设有控制舱,机身底部可拆卸连接有用于搭载不同任务模块的任务吊仓,机身顶部螺接有两个天线杆;两个机翼,且对称布置并可拆卸连接在机身的两侧,每个机翼上均设有提供垂直牵引力的第二螺旋桨;尾翼,尾翼与机身的后端可拆卸连接。该无人机兼具固定翼和旋翼无人机的优点,并且机身、机翼和尾翼之间均可快速拆装,易于储存和运输,并且任务吊舱可搭配多种任务载荷,能够一机多用,此外,尾翼可根据任务需求进行更换,适应不同的复杂地理环境。
Modularized vertical take-off and landing fixed-wing unmanned aerial vehicle
一种模块化垂直起降固定翼无人机
2021-12-28
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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