The embodiment of the invention discloses a rotor wing and wing transverse combined tilting rotor wing unmanned aerial vehicle, relates to the technical field of rotor wing aircrafts, can be assembled and disassembled on the ground, and can convert a rotor wing into a tilting state during flight. The unmanned aerial vehicle adopts a transverse arrangement connection mode, one unmanned aerial vehicle is called as a flight module, and the flight module realizes the overall design of the rotor and wing transverse combined tilt rotor unmanned aerial vehicle through the combination of a fuselage with a wing-shaped cross section, a skin and a rotor system. According to the connection mode of the combined tilt-rotor unmanned aerial vehicle, the fuselage on one side of one flight module is connected with the fuselage on one side of the other flight module, the connection mode is interface connection, and the connection device is inserted into the middle of the two interfaces.
本发明实施例公开了一种旋翼与机翼横向组合式倾转旋翼无人机,涉及旋翼飞行器技术领域,能够在地面进行组装和拆卸,在飞行时,可将旋翼变换为倾转状态。本发明中无人机采用横向排列的连接方式,一个无人机称之为一个飞行模块,一个飞行模块是通过横截面为翼型的机身、蒙皮和旋翼系统的组合实现一种旋翼与机翼横向组合式倾转旋翼无人机的总体设计。组合式倾转旋翼无人机的连接方式为:一个飞行模块的一侧机身与另一个飞行模块的一侧机身之间进行连接,连接方式为接口连接,连接装置插入两接口中部。
Rotor wing and wing transverse combined tilting rotor wing unmanned aerial vehicle
旋翼与机翼横向组合式倾转旋翼无人机
2024-05-17
Patent
Electronic Resource
Chinese
IPC: | B64U |
Rotor wing tilting mechanism and unmanned aerial vehicle
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