The invention discloses a shaftless vector electric rotor wing and a helicopter, and aims to overcome the defects that an existing helicopter is high in control difficulty, complex in structure, high in noise and high in cost. The unmanned aerial vehicle comprises two rotor wing assemblies which are arranged up and down, and a connecting piece is installed between the two rotor wing assemblies; the posture adjusting assembly is installed on the connecting piece to achieve posture adjustment of the rotor wing assembly; wherein the rotor assembly comprises a stator and a rotor, a plurality of magnetic shoes are uniformly distributed on the rotor in the circumferential direction, a plurality of winding iron cores are uniformly distributed on the stator in the circumferential direction, and magnetic poles, facing the winding iron core sides, of every two adjacent magnetic shoes are opposite; the posture adjusting assembly comprises a vector transverse rod and a vector vertical rod, the vector transverse rod is rotationally installed on the connecting piece, the vector vertical rod is rotationally installed on the vector transverse rod, a transverse rod steering engine is installed between the connecting piece and the vector transverse rod, and a vertical rod steering engine is installed between the vector transverse rod and the vector vertical rod. The aircraft can flexibly realize adjustment of various moving postures in the air, and is simple in structure, low in cost and low in noise.
本发明公开了一种无轴矢量电动旋翼及直升机,旨在解决现有的直升机操控难度大,结构复杂,噪音大,成本高的不足。该发明包括两旋翼组件,两旋翼组件上下布设,两旋翼组件之间安装连接件;调姿组件,安装在连接件上实现旋翼组件的姿态调整;其中,旋翼组件包括定子、转子,转子上周向均布安装若干磁瓦,定子上周向均布安装若干绕组铁芯,相邻两磁瓦朝向绕组铁芯侧的磁极相反;调姿组件包括矢量横杆、矢量竖杆,矢量横杆转动安装在连接件上,矢量竖杆转动安装在矢量横杆上,连接件和矢量横杆之间安装横杆舵机,矢量横杆和矢量竖杆之间安装竖杆舵机。飞机可以非常灵活地实现空中的各种运动姿态调整,结构简单,成本低,噪音小。
Shaftless vector electric rotor wing and helicopter
一种无轴矢量电动旋翼及直升机
2023-09-22
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
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