摘要
为了提高黏弹性约束阻尼结构模型仿真精度,提出一种考虑频变特性的约束阻尼结构建模方法,并开展了试验验证.首先,对ZN-3黏弹性材料进行动态试验测试,基于最小二乘法获取黏弹性材料模量和损耗因子表达式;其次,根据ZN-3黏弹性材料损耗因子关系表达式,基于考虑频变特性的修正模态应变能法,求解了约束阻尼结构的固有频率和模态损耗因子;最后,以贴敷黏弹性阻尼材料的悬臂约束阻尼薄板为例,从理论与试验两方面校验,结果表明,考虑频变特性的约束阻尼结构有限元模型具有较高精度,与试验测试结果比较误差在5%以内,验证了建模方法的准确性.
In order to improve the simulation accuracy of viscoelastic constrained damping structure model,a modeling method of constrained damping structure considering frequency-dependent characteristics was proposed and then a test was performed for verification.Firstly,the dynamic test of ZN-3 viscoelastic material was carried out,and the expressions of modulus and loss factor of viscoelastic material were obtained using the least squares method.Secondly,according to the expression of loss factor of ZN-3 viscoelastic material,the natural frequency and modal loss factor of constrained damping structure were solved using the modified modal strain energy method considering frequency-dependent characteristics.Finally,the cantilever constrained damping structure attaching the viscoelastic damping material was chosen and verified from both theory and test,whose results showed that the finite element model considering frequency-dependent characteristics has higher accuracy and the error of model to test is within 5%,which verifies the accuracy of the modeling method.
作者
罗忠
郭思伟
于长帅
何凤霞
LUO Zhong;GUO Si-wei;YU Chang-shuai;HE Feng-xia(School of Mechanical Engineering&Automation,Northeastern University,Shenyang 110819,China;Key Laboratory of Vibration and Control of Aero-Propulsion Systems,Ministry of Education,Northeastern University,Shenyang 110819,China)
出处
《东北大学学报(自然科学版)》
EI
CAS
CSCD
北大核心
2021年第7期966-971,979,共7页
Journal of Northeastern University(Natural Science)
基金
国家自然科学基金资助项目(11872148,U1908217)
中央高校基本科研业务费专项资金资助项目(N2003012,N2003013,N180703018).
关键词
黏弹性材料
频变特性
约束阻尼结构
最小二乘法
有限元模型
viscoelastic material
frequency-dependent characteristics
constrained damping structure
least squares method
finite element model