A lever transmission flapping wing aircraft is characterized in that reciprocating motion is converted into vertical flapping of double wings of the aircraft according to the lever principle, and the lever transmission flapping wing aircraft structurally comprises a supporting frame mechanism, a lever transmission mechanism, a flight bearing mechanism and a flight control mechanism, the lever transmission mechanism comprises a handle 11, pedals 12, a track 13, a main transmission rod 141, an auxiliary transmission rod 142, a two-wing transmission rod 143, a fixed hinge point 144 and a movable hinge point 145, the flight bearing mechanism comprises a front wing and an empennage 25, the front wing comprises a shoulder wing 21, a middle wing 22, a side wing 23 and an aileron 24, and the flight control mechanism comprises a front wing control mechanism, an empennage control mechanism and a gliding control mechanism.
一种杠杆传动扑翼飞行器,其特点是通过杠杆原理,将往复运动转为飞行器双翼的上下扑动,其结构包括支撑框架机构、杠杆传动机构、飞行承重机构、飞行控制机构,支撑框架机构包括轮子和支撑框架,杠杆传动机构包括11手柄、12脚蹬、13轨道、141主传动杆、142副传动杆、143两翼传动杆、144固定铰接点、145可动铰接点,飞行承重机构包括前翼和25尾翼,前翼包括21肩翼、22中翼、23侧翼、24副翼,飞行控制机构包括前翼控制机构、尾翼控制机构、滑翔控制机构。
Lever-driven ornithopter
一种杠杆传动扑翼飞行器
2022-03-29
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |