共查询到16条相似文献,搜索用时 187 毫秒
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频率相关自由阻尼层复合材料加筋板动力分析 总被引:1,自引:0,他引:1
采用子空间迭代法和精细积分对敷设粘弹性阻尼层的含损伤复合材料加筋板结构进行了频率和动力响应分析。分析中对层合板和层合梁采用了Adams应变能法与Raleigh阻尼模型相结合的阻尼矩阵构造方法;对表面粘弹性阻尼材料则考虑了材料性质和耗散系数对激振频率与温度的依赖性,建立了频率相关粘弹性材料阻尼矩阵的计算方法。通过有限元分析,分别研究了敷设自由阻尼层无损伤和含分层损伤复合材料加筋板的自振频率和模态特征,并根据幅频曲线讨论了阻尼材料模量、耗散系数和阻尼层厚度等因素对结构响应的影响,提出的计算方法对通过合理选择阻尼层材料与几何参数来有效地控制加筋板结构的振动特性,具有一定的参考价值。 相似文献
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粘弹性自由层阻尼管的有限元建模与试验研究 总被引:1,自引:1,他引:0
U型管是工业应用中的常见结构,也是振动破坏的多发部件.分析了局部黏附粘弹性沥青阻尼层U型管结构的动力特性.考虑弯曲成形过程中的厚度与截面形状变化,建立了自由层阻尼管的有限元精确模型,采用迭代法计算粘弹性结构的固有频率,进而采用模态应变能法,求得各阶模态附加的阻尼比.通过对有限元结果和试验结果的比较,验证所建立的有限元模型的正确性.最后,基于正交试验表,对阻尼层的粘贴宽度,厚度,位置等进行了试验研究,指出三种因素的对结构固有频率和阻尼比的影响,为复杂管道的减振设计提供了参考依据. 相似文献
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计算粘弹结构动力学参数的新模态应变能方法 总被引:1,自引:0,他引:1
粘弹结构在噪声与振动控制领域已得到广泛应用,然而准确地计算粘弹结构的动力学参数一直存在困难,模态应变能法及其修正方法常用作近似计算。在分析模态应变能方法和已有修正方法的原理及其相互关系的基础上,提出一种基于损耗因子幅值的新模态应变能方法,用于计算粘弹结构的损耗因子与固有频率。新方法的修正因子随粘弹结构对应模态阶次损耗因子幅值变化。取可等价为粘弹性夹层梁/板的四参数原型系统和新型高阻尼航天载荷隔振器为算例,通过与已有方法的对比分析了新方法的准确性。 相似文献
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卫星飞轮安装支架的粘弹性阻尼减振设计 总被引:2,自引:0,他引:2
应用粘弹性约束阻尼减振技术对某卫星飞轮组件安装支架结构进行振动抑制处理。约束阻尼技术能在不对结构作大的修改的前提下,提高结构的阻尼能力。首先建立原型支架结构的有限元模型,计算了其动态特性。分析了支架结构关键模态的应变能分布规律,确定出约束阻尼处理的铺敷位置。采用参数优化方法,比较了不同约束层厚度、不同阻尼层厚度设计情况下的结构阻尼性能,在满足附加重量和工艺限制要求的前提下,确定出阻尼减振设计方案。最后,将阻尼前后支架结构的加速度频率响应结果进行了对比,验证了在飞轮安装支架上应用粘弹性阻尼减振的合理性和有效性。 相似文献
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《Composites Part B》2007,38(2):159-171
The viscoelastic damping model of the cylindrical hybrid panels with co-cured, free and constrained layers has been developed and investigated by using the refined finite element method based on the layerwise shell theory. The transverse shear and normal strains and the curved geometry are exactly taken into account in the present layerwise shell model, which can depict the zig-zag in-plane and out-of-plane displacements. The damped natural frequencies, modal loss factors and frequency response functions of cylindrical viscoelastic hybrid panels are compared with those of the base composite panel without a viscoelastic layer. The difference in the free vibration and damping of the thin and thick composite laminates and the viscoelastic sandwiched beam between full and partial layerwise theories is verified by comparison with the published results. Various damping characteristics of cylindrical hybrid panels with free viscoelastic layer, constrained layer damping, and co-cured sandwich laminates are investigated. Present results show that the full layerwise damping model accurately predicted the vibration and damping of the cylindrical hybrid panels with viscoelastic layers. 相似文献
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M. A. Trindade A. Benjeddou R. Ohayon 《International journal for numerical methods in engineering》2001,51(7):855-864
An electromechanically coupled finite element model has been presented in Part 1 of this paper in order to handle active–passive damped multilayer sandwich beams, consisting of a viscoelastic core sandwiched between layered piezoelectric faces. Its validation is achieved, in the present part, through modal analysis comparisons with numerical and experimental results found in the literature. After its validation, the new finite element is applied to the constrained optimal control of a sandwich cantilever beam with viscoelastic core through a pair of attached piezoelectric actuators. The hybrid damping performance of this five‐layer configuration is studied under viscoelastic layer thickness and actuator length variations. It is shown that hybrid active–passive damping allows to increase damping of some selected modes while preventing instability of uncontrolled ones and that modal damping distribution can be optimized by proper choice of the viscoelastic material thickness. Copyright © 2001 John Wiley & Sons, Ltd. 相似文献
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