The invention relates to the technical field of aircrafts, and provides a multi-degree-of-freedom ornithopter with a high lift device, which comprises a head, a frame, a fuselage shell, an ornithopter driving mechanism, a worm and gear mechanism, an empennage device and ornithopter mechanisms mounted on two sides of the frame, the rack comprises a front framework structural part, a first framework structural part, a second framework structural part, a middle connecting rod and a tail connecting rod. The machine body shell is sleeved on the rack; the flapping wing driving mechanism comprises a motor, a motor pinion, a motor pinion support, a large straight tooth gear, a small straight tooth gear, a secondary gear and a rocker arm; the flapping wing mechanism comprises an inner wing and an outer wing; the inner side of the inner wing is connected with the rocker arm; the outer side of the inner wing is connected with the outer wing; a high lift device is arranged on the inner wing; the worm and gear mechanism is mounted on the tail connecting rod; and the empennage device is mounted on the tail connecting rod. Stable lift force can be provided for the aircraft, air resistance is reduced, and the flying movement of birds can be better simulated.
本发明涉及飞行器技术领域,提供一种带增升装置的多自由度扑翼飞行器,包括:头部、机架、机身外壳、扑翼驱动机构、蜗轮蜗杆机构、尾翼装置以及安装在机架两侧的扑翼机构;机架包括:前骨架结构件、第一骨架结构件、第二骨架结构件、中间连接杆和尾部连接杆;机身外壳套在机架上;扑翼驱动机构包括:电机、电机小齿轮、电机小齿轮支座、大直齿齿轮、小直齿齿轮、二级齿轮和摇臂;扑翼机构包括:内翼和外翼;内翼的内侧与摇臂连接,内翼的外侧与外翼连接;内翼上设置增升装置;蜗轮蜗杆机构安装在尾部连接杆上;尾翼装置安装在尾部连接杆上。本发明能够为飞行器提供稳定的升力,减小空气阻力,并更好地模仿鸟类的飞行运动。
Multi-degree-of-freedom ornithopter with high lift device
一种带增升装置的多自由度扑翼飞行器
2022-10-18
Patent
Elektronische Ressource
Chinesisch
IPC: | B64C AEROPLANES , Flugzeuge |
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