The invention discloses a two-in-one convertible unmanned aerial vehicle, and belongs to the technical field of unmanned aerial vehicles, the two-in-one convertible unmanned aerial vehicle comprises a fuselage and fixed wings, wing mounting parts with variable directions are arranged on the two sides of the fuselage, two rotor rods with rotors and fixed wing connecting parts for detachable mounting of the fixed wings are arranged on the wing mounting parts, and the two rotor rods are arranged in a splayed shape; the coplane of the rotor wings on the two rotor wing rods is parallel to the coplane of the two rotor wing rods, the fixed wing connecting part is located between the two rotor wing rods, the wing face of the fixed wing installed on the fixed wing connecting part is perpendicular to the coplane of the two rotor wing rods, and the coplane of the two rotor wing rods is located on the orientation changing path of the wing installing part. And the plane can be perpendicular to or parallel to the length direction of the plane body. The two modes of the helicopter and the fixed wing can be switched on the same unmanned aerial vehicle by changing the orientation of the wing mounting part and cooperating with the disassembly and assembly of the fixed wing, two different types of unmanned aerial vehicles do not need to be carried, the equipment cost and the space occupancy rate are reduced, and deployment and carrying are convenient.
本发明公开了一种二合一可转换无人机,属于无人机技术领域,包括机身和固定翼,机身的两侧设有朝向可变的机翼安装部,机翼安装部上设有两个自带旋翼的旋翼杆和供固定翼可拆卸安装的固定翼连接部,两个旋翼杆呈八字形排布,两个旋翼杆上的旋翼的共面平行于两个旋翼杆的共面,固定翼连接部位于两个旋翼杆之间,安装于固定翼连接部上的固定翼的翼面垂直于两个旋翼杆的共面,两个旋翼杆的共面在机翼安装部的朝向改变路径上,能够垂直于机身长度方向或平行于机身长度方向。改变机翼安装部的朝向,配合着固定翼的拆装,便可在同一无人机上进行直升机和固定翼两种模式的切换,无需携带两种不同类型的无人机,降低设备成本,空间占用率,方便部署、携带。
Two-in-one convertible unmanned aerial vehicle
一种二合一可转换无人机
2024-04-12
Patent
Electronic Resource
Chinese
IPC: | B64U |
CONVERTIBLE LIFTING PROPELLER FOR UNMANNED AERIAL VEHICLE
European Patent Office | 2017
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