The invention discloses a bionic aircraft twisting flapping wing structure with a gliding function, and belongs to the field of bionic aircrafts. A bionic aircraft twisting flapping wing structure with a gliding function comprises two symmetrically arranged vertical plates, and further comprises a connecting plate fixedly connected between the two vertical plates, a double-shaft motor is fixedly installed between the two vertical plates, and two output shafts of the double-shaft motor are both connected with first short shafts; the long shaft is rotationally connected to the tops of the two vertical plates, and second short shafts are fixedly connected to the two ends of the long shaft; different flight actions of the bionic flapping-wing aircraft can be obtained through one power source, the attack angle of the wing plate can be changed at any time according to the flight condition so as to change the flight attitude, the application of a crank rocker mechanism in flapping of the aircraft is expanded, gliding flight of the aircraft is achieved, and the bionic flapping-wing aircraft is suitable for structural design of various flying organisms. And the structure is more compact, and high social and economic popularization value is achieved.
本发明公开了一种具有滑翔功能的仿生飞行器扭转扑翼结构,属于仿生飞行器领域。一种具有滑翔功能的仿生飞行器扭转扑翼结构,包括两个对称设置的竖板,还包括:连接板,固定连接在两个所述竖板之间,其中,两个所述竖板之间固定安装有双轴电机,所述双轴电机的两个输出轴上均连接有第一短轴;长轴,转动连接在两个所述竖板的顶部,其中,所述长轴的两端均固定连接有第二短轴;本发明可以通过一个动力源得到仿生扑翼飞行器不同的飞行动作,可根据飞行状况随时改变翼板攻角从而变换飞行姿态,扩展了曲柄摇杆机构在飞行器扑动中的应用,实现了飞行器的滑翔飞行,适用于各种飞行生物的结构设计,结构更加紧凑,具有较高的社会、经济推广价值。
Bionic aircraft torsion flapping wing structure with gliding function
一种具有滑翔功能的仿生飞行器扭转扑翼结构
2024-01-26
Patent
Elektronische Ressource
Chinesisch
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