The invention discloses a tilt rotor unmanned aerial vehicle. The rear end of a front fuselage is detachably connected with the front end of a rear fuselage; the upper side of the front fuselage is detachably connected with a central wing; the two ends of the central wing are rotationally connected with outer wings correspondingly. A driving motor is arranged in the outer wing; propellers are arranged on output shafts of the driving motors, tilting steering engines are arranged in the outer wings, rotating shafts of the tilting steering engines are connected with the central wing through firstswinging assemblies, the tilting steering engines drive the two outer wings to be switched between a horizontal rotating state and a vertical rotating state, and two full-motion horizontal tails arearranged at the end, deviating from the front fuselage, of the rear fuselage; and the rotating shafts of the tilting steering engines are horizontally arranged. The purpose is to solve the problem that in the prior art, a fixed wing flight mode and a rotor wing flight mode cannot coexist on the same unmanned aerial vehicle. The tilt rotor unmanned aerial vehicle has the technical effects that vertical take-off and landing and horizontal high-speed direct flight can be achieved, vertical take-off and landing, rotor wing tilting and modular design are achieved, operation is easy, and reliabilityis remarkably improved.
本发明公开了一种倾转旋翼无人机,前机身的后端与后机身的前端可拆卸连接,前机身的上侧可拆卸连接有中央机翼,中央机翼的两端分别转动连接有外机翼,外机翼中设置有驱动电机,驱动电机的输出轴设置有螺旋桨,外机翼内设置有倾转舵机,倾转舵机的转轴通过第一摆动组件与中央机翼连接,倾转舵机带动两个外机翼在水平转动状态和竖直转动状态之间切换,后机身背离前机身的一端设置有两个全动平尾;倾转舵机的转轴水平设置。目的在于解决现有技术中固定翼飞行方式与旋翼飞行方式无法共存在同一无人机上的问题。技术效果:既能垂直起降也能水平高速直飞,实现了垂直起降、倾转旋翼、模块化设计、操作简单且可靠性显著提高。
Tilt rotor unmanned aerial vehicle
一种倾转旋翼无人机
2020-05-19
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
CONTROL METHOD OF TILT ROTOR UNMANNED AERIAL VEHICLE, AND TILT ROTOR UNMANNED AERIAL VEHICLE
Europäisches Patentamt | 2021
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