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对一种可伸缩机翼实验装置进行结构设计、功能实现和振动实验进行研究.利用三维建模软件优化设计了可伸缩机翼的作动机构,完成对可伸缩机翼结构的总体设计和各个子系统结构设计,基于可伸缩机翼实验装置进行了振动实验研究,详细分析了在不同的外伸速度和收缩速度情况下,可伸缩机翼的横向振动响应,得到有意义的实验结果,对工程应用具有一定的理论指导作用.
The structure design, function realization and vibration experiment of a retractable wing experimental device are studied.Using three-dimensional modeling software to optimize the design of the retractable wing actuating mechanism, to complete the retractable wing structure of the overall design and each Based on the experimental design of the retractable airfoil, the subsystem structure was designed and the vibration experiments were conducted. The lateral vibration response of the retractable wing was analyzed in detail under different conditions of the extension speed and the contraction speed. The experimental results were meaningful. Engineering application has a certain theoretical guidance.