Feasibility Analysis of the Rotor Elastic Support With Piezoelectric Damping

Yuhong Hu, Lin Li, Yaguang Wu, Yu Fan
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Abstract

The squirrel cage is a widely-used elastic support in aeroengine. The combination of the squirrel cage and damping structures, such as squeeze film dampers, can effectively suppress rotor vibration. The squeeze film damper, although providing significant damping, requires a specific auxiliary lubricant supply system, which occupies space and brings additional weight. Piezoelectric materials have the advantages of light weight, high energy density, and wide bandwidth. The electromechanical coupling effect ensures that they can be used as energy transducers, and the corresponding piezoelectric damping has attracted extensive attention. In this study, we propose an elastic support-piezoelectric damper system for rotors by integrating the piezoelectric damping to the squirrel cage. The purpose of this study is to demonstrate the feasibility of the piezoelectric squirrel cage to suppress the vibration of the low pressure rotor of aero-engine from both the aspects of vibration and strength. To do that, the finite element model of a dummy rotor with elastic support-piezoelectric damper system is established first. The polarization direction and the network topology are optimized to reduce the amount of circuit impedance under the premise of ensuring the modal electromechanical coupling factor. An in-house code to simulate the dynamic performance of the rotor with the elastic support-piezoelectric damper system is developed in ANSYS/MATLAB environment. To reduce the computational cost, the following acceleration techniques are adopted: 1) the specific modal synthesis method dedicated to piezoelectric structures is implemented to reduce the dimension of the governing equations; 2) the equivalent linearization method is carried out to transfer the synchronized switch damping (SSD) with nonlinear nature to a frequency-dependent impedance, thus the time-consuming nonlinear solver is avoided. The unbalance response of the rotor is analyzed numerically. The damping effects of two promising piezoelectric damping technologies, i.e. the resonant damping and the SSD, are compared and discussed. Results show that the SSD network can reduce the vibration level of the rotor significantly with good robustness; the number of the SSD control circuit is only the half of the number of squirrel cage bars; the failure strength margin is sufficient.
压电阻尼转子弹性支承的可行性分析
鼠笼是一种应用广泛的航空发动机弹性支承。鼠笼与挤压膜阻尼器等阻尼结构相结合,可有效抑制转子振动。挤压膜阻尼器虽然提供了显著的阻尼,但需要特定的辅助润滑剂供应系统,这占用了空间并带来了额外的重量。压电材料具有重量轻、能量密度高、带宽宽等优点。机电耦合效应保证了它们可以作为能量换能器,相应的压电阻尼引起了广泛的关注。在这项研究中,我们提出了一个弹性支撑压电阻尼系统的转子集成压电阻尼鼠笼。本研究的目的是从振动和强度两个方面论证压电鼠笼抑制航空发动机低压转子振动的可行性。为此,首先建立了弹性支承-压电阻尼系统的仿真转子有限元模型。在保证模态机电耦合系数的前提下,优化极化方向和网络拓扑结构,减少电路阻抗量。在ANSYS/MATLAB环境下编制了转子弹性支承-压电阻尼器系统动态性能仿真程序。为了减少计算成本,采用了以下加速技术:1)采用压电结构特有的模态综合方法,降低控制方程的维数;2)采用等效线性化方法将具有非线性特性的同步开关阻尼(SSD)转化为频率相关的阻抗,从而避免了耗时的非线性求解。对转子的不平衡响应进行了数值分析。比较和讨论了两种有发展前景的压电阻尼技术——谐振阻尼和固态固态阻尼的阻尼效果。结果表明,该网络能显著降低转子的振动水平,具有较好的鲁棒性;SSD控制电路的数量仅为鼠笼条数量的一半;破坏强度裕度是足够的。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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