In view of the complex structure,low efficiency and single action of present aircrafts,a new type of bionic flapping-wing flight mechanism is designed,which can realize 3-DOF flapping,folding and torsion by single motor.According to the biological scale rate,the structure dimension of the flapping wing aircraft is designed,and its mechanism parameters are optimized.The bionic 3D model is constructed by Solid Works and the finite element analysis of the flapping wing aircraft is analyzed based on ANSYS Workbench to gain the total deformation,stress、equivalent strain and dynamic motion parameters of flapping wing aircraft,which provides theoretical support for the optimization of the prototype.
关键词
飞行器/仿生扑翼/结构设计/动力学/有限元分析
Key words
aircraft/bionic flapping wing/structural design/dynamics/finite element analysis
维普
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