可伸缩机翼结构设计与振动实验研究
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国家自然科学基金重点资助项目(10732020);国家自然科学基金资助项目(11072008和10802001)


Structural design and vibration experimental investigation of telescoping wings
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    摘要:

    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.

    Abstract:

    A type of experimental apparatus of telescopic wings was designed and the vibration experiments were investigated. The mechanism of the telescopic wings was designed firstly, and the experimental apparatus as a whole and the sub-systems were made. Finally, the vibration experiments of telescopic wings were completed. The transverse vibration responses of the wings were investigated at different extended and contracted velocity. Some useful phenomena and conclusion were obtained based on the experiment solution.

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张伟,张谦,曹东兴.可伸缩机翼结构设计与振动实验研究[J].动力学与控制学报,2011,9(4):326~330; Zhang Wei, Zhang Qian, Cao Dongxing. Structural design and vibration experimental investigation of telescoping wings[J]. Journal of Dynamics and Control,2011,9(4):326-330.

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  • 收稿日期:2011-05-13
  • 最后修改日期:2011-06-23
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