The invention discloses a rotor stator built-in type magnetic suspension rotor and an aircraft thereof, and solves the technical problems that an existing rotor is heavy due to the structure that a rotor is wrapped by a stator, and the heat dissipation performance and the dustproof performance are poor. The device comprises a rotor stator, a rotor rotor, an axial supporting module, a radial limiting module and a rotation driving module, one end of the rotor rotor is connected with a rotor paddle, the other end of the rotor rotor is opened to form a rotor stator containing space, the rotor stator is located in the containing space, the axial supporting module comprises a first supporting assembly and a second supporting assembly, and the radial limiting module comprises a radial limiting module and a radial limiting module. An air gap is formed between the rotor wing stator and the rotor wing rotor in the axial direction; the second supporting assemblies are arranged on the sides, close to the rotor wing rotors, of the rotor wing stators correspondingly. The radial limiting module is used for forming an air gap between the rotor wing stator and the rotor wing rotor in the radial direction; and the rotation driving module is used for driving the rotor wing rotor and the rotor wing paddle to rotate. The motor has the advantages of light weight, good heat dissipation and dust prevention effects, low noise and the like.
本发明公开了一种旋翼定子内置式的磁悬浮旋翼及其飞行器,解决了现有的旋翼由于定子包裹转子的结构使得旋翼较重,且散热性和防尘性能差技术问题。本发明包括:旋翼定子、旋翼转子、轴向支撑模块、径向限位模块与旋转驱动模块,旋翼转子的一端连接有旋翼桨,旋翼转子的另一端开口形成旋翼定子容纳空间,旋翼定子位于所述容纳空间中,轴向支撑模块包括第一支撑组件和第二支撑组件,用于使旋翼定子和旋翼转子之间在轴向上形成气隙;旋翼定子靠近所述旋翼转子的一侧均设置有所述第二支撑组件;径向限位模块用于使旋翼定子和旋翼转子之间在径向上形成气隙;旋转驱动模块用于驱动旋翼转子和旋翼桨转动。本发明具有重量轻、散热和防尘效果好、噪音小等优点。
Magnetic suspension rotor with built-in rotor stator and aircraft thereof
一种旋翼定子内置式的磁悬浮旋翼及其飞行器
2024-08-30
Patent
Electronic Resource
Chinese
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