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Analysis of the characteristics of a squeeze film damper by three-dimensional Navier-Stokes equations: A numerical approach and experimental validation.

机译:通过三维Navier-Stokes方程分析挤压膜阻尼器的特性:一种数值方法和实验验证。

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摘要

The squeeze film damper is widely used in turbomachinery due to its ability to reduce vibration, help transition through the critical speed (resonance) and diminish the force transmitted to the support frame. Instead of the commonly used Reynolds equation modeling technique, this dissertation employed the three-dimensional Navier-Stokes equations. These equations are coupled with a homogeneous cavitation model, Gumbel (π-film) or full Sommerfeld (2π-film) cavitation strategies in dealing with the flow field and pressure development in a squeeze film damper. The characteristics of the pressure distribution, velocity field, dynamic force and the associated damping and inertia coefficients were investigated by the parametric studies using either lubricant properties such as the gas concentration, viscosity and density or damper geometry.;The equation of motion for a rigid or flexible rotor model was employed in the stability analysis for the rotor-damper operating system. The dynamic coefficients were introduced into the equations to determine the rotor trajectory and stability through the source term. By analyzing the eccentricity, rotor deflection and transmissibility response, this dissertation has pointed to a methodology of finding the ‘preferred range’ of both one- and two-phase squeeze film dampers. Further, parametric studies on the rotor-damper system evaluate the effects of the lubricant dynamic viscosity, density, gaseous or vaporous cavitation, gas concentration, static eccentricity, whirling speed, rotor flexibility, retainer spring stiffness, the lumped mass distribution and the amount of imbalance. These parameters are necessary in optimizing the design of a damper.;Except for the analysis based on the equations of motion, the direct numerical simulation for the determination of the journal orbit was performed by the coupling of flow, grid deformation and stress module in CFD-ACE+. The close match of the two sets of results strengthened the confidence of the simulation results.;The experimental portion of this study was designed to validate qualitatively and quantitatively the numerical simulations in pressure distribution, cavitation visualization and the damper vibration. The damper vibration was measured by means of proximity sensors located circumferentially around the supporting frame; the pressure evolution was measured by pressure transducers and the gaseous and vaporous cavitation was visualized by both a digital camera with strobotac lighting and a high speed (5000fps) camera. The experimental results corroborated the theoretical analysis.
机译:挤压膜阻尼器由于具有减少振动,帮助过渡到临界速度(共振)并减小传递到支撑框架的力的能力而被广泛应用于涡轮机械。代替常用的雷诺方程建模技术,本文采用三维Navier-Stokes方程。这些方程式与均质气蚀模型,Gumbel(π膜)或完整的Sommerfeld(2π膜)气蚀策略相结合,用于处理挤压膜阻尼器中的流场和压力发展。通过参数研究使用润滑剂特性(例如气体浓度,粘度和密度或阻尼器几何形状)来研究压力分布,速度场,动态力以及相关的阻尼和惯性系数的特征。在转子-阻尼器操作系统的稳定性分析中采用了柔性转子模型。通过源项将动态系数引入方程式,以确定转子的轨迹和稳定性。通过分析偏心距,转子挠度和传递响应,本文指出了一种寻找一相和两相挤压膜阻尼器“最佳范围”的方法。此外,对转子-阻尼器系统的参数研究评估了润滑剂动态粘度,密度,气态或气态空化,气体浓度,静态偏心率,回旋速度,转子挠性,保持器弹簧刚度,集总质量分布和润滑脂数量的影响。不平衡。这些参数对于优化减振器的设计是必不可少的。除了基于运动方程的分析之外,通过CFD中的流动,网格变形和应力模块的耦合对确定轴颈轨道进行直接数值模拟。 -ACE +。两组结果的紧密匹配增强了仿真结果的可信度。;本研究的实验部分旨在定性和定量地验证压力分布,气穴可视化和阻尼器振动方面的数值模拟。减振器的振动是通过围绕支撑框架沿周向定​​位的接近传感器进行测量的;通过压力传感器测量压力的变化,并通过具有strobotac照明的数码相机和高速(5000fps)相机可视化气态和气态的气蚀现象。实验结果证实了理论分析。

著录项

  • 作者

    Xing, Changhu.;

  • 作者单位

    The University of Akron.;

  • 授予单位 The University of Akron.;
  • 学科 Engineering Mechanical.
  • 学位 Ph.D.
  • 年度 2009
  • 页码 445 p.
  • 总页数 445
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

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