A left micro-resistance arm lever is fixedly connected with a right micro-resistance arm lever, a fulcrum rotating shaft is integrally arranged between the back faces of a left resistance arm crank and a right resistance arm crank, a right resistance point rotating shaft is integrally arranged on the front face of the right resistance arm crank, and a left resistance point rotating shaft is integrally arranged on the front face of the left resistance arm crank. The three rotating shafts are arranged on three different layers respectively, so that the arrangement distance of the three rotating shafts can be shortened infinitely, and the resisting arm of the lever can be shortened infinitely. The micro resistance arm lever drives the horizontal wing and the drooping wing to vibrate up and down to obtain lift force and then drives the U-shaped sinker bar at the tail end of the tail frame to vibrate up and down to impact the balance weight ball, then the balance weight ball drives the tail rod to enable the swing wing to swing up and down, and the swing wing obtains thrust to achieve practical manpower flight. The device has the advantages of being durable and efficient in structure.
本发明公开了一种微阻力臂杠杆人力飞机,左微阻力臂杠杆与右微阻力臂杠杆固定连接,支点转轴整体设置在左右阻力臂曲柄的背面之间,右阻力点转轴整体设置在右阻力臂曲柄正面,左阻力点转轴整体设置在左阻力臂曲柄正面,三个转轴分别设置在三个不同层面使三个转轴的设置距离可以无限缩短,杠杆的阻力臂从而可以无限缩短。微阻力臂杠杆带动水平翼及下垂翼上下振动获得升力,再带动尾架末端U型撞杆上下振动撞击配重球,再由配重球驱动尾杆使摆翼上下摆动,摆翼获得推力实现实用的人力飞行。本发明的优点:结构耐用高效。
Micro-resistance arm lever manpower aircraft
微阻力臂杠杆人力飞机
2024-11-19
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |
European Patent Office | 2022
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