航空学报 > 2007, Vol. 28 Issue (3): 729-734

直角切口柔性铰链平行四杆机构的屈曲分析

宗光华,余志伟,毕树生,于靖军   

  1. 北京航空航天大学 机械工程及自动化学院
  • 收稿日期:2006-03-17 修回日期:2006-05-19 出版日期:2007-05-10 发布日期:2007-05-10
  • 通讯作者: 宗光华

Buckling Analysis of the Parallel Fourbar Mechanism Rightangle notch Flexure Hinges

ZONG Guang-hua,YU Zhi-wei,BI Shu-sheng,YU Jing-jun   

  1. School of Mechanical Engineering and Automation, Beijing University of Aeronautics and Astronautics
  • Received:2006-03-17 Revised:2006-05-19 Online:2007-05-10 Published:2007-05-10
  • Contact: ZONG Guanghua

摘要:

介绍了研究柔性铰链机构屈曲特性的重要意义。利用材料力学弯曲变形理论的挠曲线近似微分方程建立了计算直角切口柔性铰链平行四杆机构屈曲临界力的数学模型。在简单可靠的实验装置上测试了实际样件的屈曲临界力,并利用商用有限元软件ANSYS 8.0对相应的四杆机构模型进行了非线性屈曲分析。最终结果表明:理论值、实验值以及仿真值都十分接近,但仍存在一定的误差,通过原因分析,证实了存在这种误差的合理性,从而验证了所建数学模型具有较高的参考价值,可以作为柔性铰链平行四杆机构屈曲优化设计的指导理论。

关键词: 屈曲, 临界力, 柔性铰链, 柔性机构, 有限元

Abstract:

The importance of the study on buckling performance was presented. The mathematical model, used to calculate the buckling critical force of compliant parallel four-bar mechanism with right-angle notch flexure hinges, was established with the approximative differential equations of the flexible curve based on the bending theory in strength of materials. The buckling critical force of the sample was tested on the simple and reliable experimental equipment. Meanwhile, the nonlinear buckling analysis was carried out using the finite element model (FEM) method.

Key words: buckling,  , critical , force,  , flexure , hinge,  , compliant , mechanism,  , FEM

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