• CN:11-2187/TH
  • ISSN:0577-6686

机械工程学报 ›› 2026, Vol. 62 ›› Issue (7): 308-323.doi: 10.3901/JME.260380

• 机械动力学 • 上一篇    

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填充泡沫全复合蜂窝芯层三明治结构非线性阻尼特性研究

许卓1, 姚楠1, 顾大卫2, 谭大鹏2, 李晖3, 闻邦椿3   

  1. 1. 东北电力大学机械工程学院 吉林 132011;
    2. 浙江工业大学机械工程学院 杭州 310014;
    3. 东北大学机械工程与自动化学院 沈阳 110819
  • 收稿日期:2025-05-01 修回日期:2025-10-19 发布日期:2026-05-25
  • 作者简介:许卓,男,1986年出生,博士,副教授,硕士研究生导师。主要研究方向为复合结构减振降噪。E-mail:xuzhuo0816@neepu.edu.cn
    顾大卫(通信作者),男,1991年出生,博士,讲师,硕士研究生导师。主要研究方向为机械系统非线性动力学与控制,先进复合结构设计、优化及应用,新能源轮毂电机设计、优化及应用。E-mail:goodavid@zjut.edu.cn
  • 基金资助:
    浙江省自然科学基金探索青年(LQ23E050018)、国家自然科学基金(52405136)和东北大学航空动力装备振动及控制教育部重点实验室研究基金(VCAME202204)资助项目。

Research on the Nonlinear Damping Characteristics of Foam-filled All-composite Honeycomb-core Sandwich Panels

XU Zhuo1, YAO Nan1, GU Dawei2, TAN Dapeng2, LI Hui3, WEN Bangchun3   

  1. 1. School of Mechanical Engineering, Northeast Electric Power University, Jilin 132011;
    2. School of Mechanical Engineering, Zhejiang University of Technology, Hangzhou 310014;
    3. School of Mechanical Engineering and Automation, Northeastern University, Shenyang 110819
  • Received:2025-05-01 Revised:2025-10-19 Published:2026-05-25

摘要: 提出了一种预测填充泡沫全复合蜂窝芯层三明治结构(Foam-filled all-composite honeycomb-core sandwich panels, FF-ACHCSP)非线性阻尼特性理论模型。首先将Reddy高阶剪切变形理论和哈密顿原理结合,建立了结构的理论框架。然后利用有限元的方法,求解了FF-ACHCSP结构的能量方程,同时利用复模量法对非线性阻尼进行表达。最终,整理得到一套完整的理论模型,对FF-ACHCSP结构的固有频率,模态振型,模态阻尼比和频率响应曲线进行求解。为验证理论模型的准确性,研究搭建了振动测试系统,并制备了实验件,对实验件进行振动测试,二者结果吻合良好,证明了理论模型的准确性。最后,为对结构进一步优化,探究了填料密度,蜂窝单元壁厚和壁宽对FF-ACHCSP结构阻尼特性的影响。所提出的理论模型可准确预测FF-ACHCSP结构的阻尼特性,为此种结构的实际应用提供指导性建议。

关键词: 蜂窝芯, 全复合三明治结构, 非线性阻尼, 有限元法

Abstract: A theoretical model for predicting the nonlinear damping characteristics of foam-filled all-composite honeycomb-core sandwich panels (FF-ACHCSP) is presented. Firstly, the theoretical framwork of the structure is established by combining Reddy’s high-order shear theory with Hamilton's principle. Subsequently, the energy equations of the FF-ACHCSP structure are solved by the finite element method, and the nonlinear damping is expressed using the complex modulus method. Finally, a comprehensive theoretical model is developed, enabling the determination of natural frequencies, mode shapes, modal damping ratios, and frequency response curves of the FF-ACHCSP structure. To validate the accuracy of the theoretical model, a vibration testing system is set up, and experimental specimens are prepared for vibration testing. The results from both approaches agree well, confirming the accuracy of the theoretical method. Finally, to further optimize the structure, this study investigates the influence of filler density, honeycomb cell wall thickness, and wall width on the damping characteristics of the FF-ACHCSP structure. The theoretical model proposed accurately predicts the damping characteristics of the FF-ACHCSP structure, providing guiding suggestions for the practical application of this type of structure.

Key words: honeycomb-core, all-composite sandwich panels, nonlinear damping, finite element method

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