The invention discloses an electromagnetic positive and negative propeller power device of an electric fixed-wing aircraft. The power device comprises an electromagnetic positive and negative propeller structure and a positive and negative propeller control circuit, and the electromagnetic positive and negative propeller structure comprises a variable pitch rod, a torque conversion mechanism, a hollow shaft brushless motor, a bidirectional self-holding electromagnet, a motor mounting seat and a bidirectional self-holding electromagnet mounting seat; a coupler is arranged between the variable pitch rod and the bidirectional self-holding electromagnet, a connecting double-thread screw is arranged between the electromagnet mounting seat and the motor mounting seat, the torque conversion mechanism, the hollow shaft brushless motor and the bidirectional self-holding electromagnet are coaxially arranged, and the torque conversion mechanism is arranged at the front end of a main shaft. By theadoption of the structure, under the condition that motor steering of electric fixed-wing aircrafts including electric unmanned aerial vehicles, electric aircrafts and electric aviation model aircrafts is not changed, reverse thrust deceleration, ground reversing and emergency takeoff stopping of the electric fixed-wing aircrafts can be achieved. The device is convenient to maintain and replace parts, low in cost, compact in structure, small in size, light in weight, high in reliability, easy to operate, remarkable in function, novel and practical.
本发明公开了一种电动固定翼飞机电磁正反桨动力装置,包括电磁正反桨结构和正反桨控制电路,电磁正反桨结构包括为变距杆、变矩机构,空心轴无刷电机、双向自保持电磁铁、电机安装座和双向自保持电磁铁安装座,变距杆和双向自保持电磁铁之间设置有联轴器,电磁铁安装座和电机安装座之间设置有连接双头螺杆,变矩机构、空心轴无刷电机和双向自保持电磁铁三者同轴布置,变矩机构设置在主轴的前端;本发明采用上述结构,能够在不改变电动固定翼飞机包括电动无人机,电动飞机和电动航空模型飞机电机转向的情况下实现电动固定翼飞机的反推减速和地面倒车以及紧急中止起飞。本装置便于维修和更换件,成本低廉,结构紧凑,体积小,重量轻,可靠性高,操作简单,功能显著,新颖实用。
Electromagnetic positive and negative propeller power device of electric fixed-wing aircraft
一种电动固定翼飞机电磁正反桨动力装置
2021-02-12
Patent
Electronic Resource
Chinese
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