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绕定轴转动的主动约束层阻尼板的振动控制研究 被引量:3

VIBRATION CONTROL OF ROTATING PLATES WITH ACTIVE CONSTRAINED LAYER DAMPING TREATMENT
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摘要 对贴有主动约束层阻尼的转动悬臂板的动力学建模及振动控制问题进行了研究。悬臂板绕定轴以不同的定常角速度作面内转动,基于Kirchhoff复合板理论,利用Lagrange与有限元结合的方式导出了系统的运动微分方程。随后用静力分析验证了压电层作为主动约束层的作动效用,并给出了转动ACLD板的瞬态响应和稳态响应的数值仿真结果,对固定和转动情况下贴有PZT、PCLD和ACLD板的振动控制效果作了比较分析,结果表明ACLD可以作为一种有效的方式对转动悬臂板进行振动抑制。所得结果可以为转动柔性结构的系统辨识及其振动控制提供理论依据。 The dynamic modeling and vibration control of a rotating cantilever plate with fully covered active constrained layer damping (ACLD) treatment are investigated. The cantilever plate is rotating at different constant angular speeds about its normal axis in horizontal plane. The model is based on the Kirchhoff classical laminate theory. Lagrange formulation in conjunction with finite element method (FEM) is developed to drive the differential equations of motion. Static stress analysis is provided to verify the actuator’s effects of piezoelectric active constrained layer. Then the numerical simulation results of transient responses and steady state responses of rotating ACLD plate system are presented. In particular, the effects of different kinds of vibration suppressions including PZT (piezo-treated), PCLD (passive constrained layer damping) and ACLD applied to non-rotating and rotating plate system are investigated. Comparisons with the performance of PZT and conventional PCLD clearly demonstrate the merit of the ACLD as an effective means for suppressing the vibration of the rotating cantilever plates. The results of the study will be useful for system identification and vibration suppression of rotating flexible structures.
出处 《振动与冲击》 EI CSCD 北大核心 2008年第8期138-143,共6页 Journal of Vibration and Shock
基金 国家自然科学基金资助项目(No.10672099)
关键词 转动悬臂板 振动控制 Lagrange公式 主动约束层阻尼 vibration control lagrange formulation active constrained layer damping rotating cantilever plate
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参考文献13

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同被引文献20

  • 1王彦琴,盛美萍,孙进才.变截面梁式动力吸振器的宽带吸振机理[J].振动工程学报,2004,17(4):473-476. 被引量:10
  • 2宛敏红,王敏庆,行晓亮,范玉岭.梁式动力吸振器用于抑制薄板振动的研究[J].噪声与振动控制,2007,27(1):27-30. 被引量:8
  • 3关玉璞,陈伟,高德平.航空发动机叶片外物损伤研究现状[J].航空学报,2007,28(4):851-857. 被引量:77
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