本发明涉及一种基于弧面翼的仿生扑翼飞行器转向机构,包括:控制模块、舵机、舵机摆臂、两种弧面翼翼肋、弧面翼可弯折翼肋、第一连接杆、第二连接杆,本发明能够仅通过仿生扑翼飞行器的弧面翼机翼的可弯折翼肋的反向运动,实现弧面翼的弯度和迎角的反向变化,从而改变仿生扑翼飞行器两侧机翼扑动过程中产生的升力和推力,形成差值,最终实现仿生扑翼飞行器的转向,并最大程度实现仿生外观,并且整个机构运行平顺,稳定可靠。
The invention relates to a bionic flapping-wing aircraft steering mechanism based on cambered-surface wings, and the bionic flapping-wing aircraft steering mechanism comprises a control module, a steering engine, a steering engine swing arm, two kinds of cambered-surface wing ribs, a bendable cambered-surface wing rib, a first connecting rod and a second connecting rod. According to the bionic flapping-wing aircraft, reverse changes of the camber and the attack angle of the cambered-surface wing are achieved, so that lift force and thrust generated in the flapping process of wings on the two sides of the bionic flapping-wing aircraft are changed, a difference value is formed, finally steering of the bionic flapping-wing aircraft is achieved, the bionic appearance is achieved to the maximum extent, and the whole mechanism runs smoothly, stably and reliably.
一种基于弧面翼的仿生扑翼飞行器转向机构
2024-07-19
Patent
Electronic Resource
Chinese
IPC: | B64C AEROPLANES , Flugzeuge |