采用分段式主动约束层阻尼处理的旋转柔性梁的动态建模与振动抑制

IF 2.1 3区 工程技术 Q2 ENGINEERING, AEROSPACE
Yue Wang, Yiming Fang, Liang Li, Dingguo Zhang, W. Liao, Jianshi Fang
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引用次数: 0

摘要

本文采用高阶近似耦合(HOAC)动力学方程对轮毂-横梁系统进行了分段主动约束层阻尼处理(SACLD)。为了改善传统主动约束层阻尼(ACLD)的阻尼特性,粘弹性阻尼层和压电约束层被切割在同一位置。通过增加粘弹性阻尼层的剪切应变来增强结构的阻尼特性。采用有限元法对 SACLD 梁进行离散化处理。SACLD 梁元素间位移的不连续性实现了缺口。基于刚柔耦合动力学理论,研究了 SACLD 旋转梁在不同情况下的动态响应。结果表明,分段方法并不总是有效的。只有在使用适当的材料和尺寸参数时,SACLD 梁才能提供比 ACLD 梁更好的振动抑制效果。此外,还讨论了基底层厚度、压电约束层厚度、粘弹性阻尼层厚度、角速度、粘弹性阻尼层损耗因子和控制增益对 SACLD 处理旋转挠性梁振动的影响。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Dynamic Modeling and Vibration Suppression of a Rotating Flexible Beam with Segmented Active Constrained Layer Damping Treatment
This paper uses high-order approximate coupling (HOAC) dynamics equations for the hub–beam system with segmented active constrained layer damping treatment (SACLD). To improve the damping characteristics of traditional active constrained layer damping (ACLD), the viscoelastic damping layer, and the piezoelectric constraining layer are cut at the same position. The damping characteristics of the structure are enhanced by increasing the shear strain of the viscoelastic damping layer. The finite element method is used to discretize the SACLD beam. The discontinuity of the SACLD beam element-to-element displacement achieves the notch. Based on the theory of rigid–flexible coupling dynamics, the dynamic responses of the SACLD rotating beam under different cases are studied. The results show that the segmentation method is not always effective. A SACLD beam provides better vibration suppression than an ACLD beam only when appropriate material and dimensional parameters are used. The influences of base-layer thickness, piezoelectric constraining layer thickness, viscoelastic damping-layer thickness, angular velocity, the viscoelastic damping-layer loss factor, and control gains on the vibration of the rotating flexible beam with SACLD treatment are also discussed.
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来源期刊
Aerospace
Aerospace ENGINEERING, AEROSPACE-
CiteScore
3.40
自引率
23.10%
发文量
661
审稿时长
6 weeks
期刊介绍: Aerospace is a multidisciplinary science inviting submissions on, but not limited to, the following subject areas: aerodynamics computational fluid dynamics fluid-structure interaction flight mechanics plasmas research instrumentation test facilities environment material science structural analysis thermophysics and heat transfer thermal-structure interaction aeroacoustics optics electromagnetism and radar propulsion power generation and conversion fuels and propellants combustion multidisciplinary design optimization software engineering data analysis signal and image processing artificial intelligence aerospace vehicles'' operation, control and maintenance risk and reliability human factors human-automation interaction airline operations and management air traffic management airport design meteorology space exploration multi-physics interaction.
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