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Numerical analyzes and experimental investigations on the fully-coupled thermo-elasto-gasdynamic behavior of air foil journal bearings

机译:空气箔轴颈轴承全耦合热弹性动力学行为的数值分析及实验研究

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摘要

Air foil journal bearings are an important component in high-speed, oil-free turbomachin-ery applications. In order to optimize the performance of rotor systems supported by air foil journal bearings, detailed numerical models are needed. In this paper, a fully-coupled thermo-elasto-gasdynamic bearing model is presented. Using this model, the thermo-elasto-gasdynamic behavior of a mechanically preloaded three-pad air foil journal bearing is investigated numerically. Furthermore, experiments are accomplished in order to validate the results obtained with the numerical model. The 3D thermo-elasto-gasdynamic bearing model comprises the description of bump and top foil deflection and the calculation of the pressure and temperature distribution in the air film as well as the temperature distributions in the surrounding structure, namely in the rotor, in the bearing sleeve and in the top and bump foil. The bump and top foil deflection are described by a nonlinear beamshell theory according to Reissner. The model accounts for the contact between the bump and the top foil and between the bump foil and the bearing sleeve. The pressure distribution is calculated by solving the generalized Reynolds equation according to Dowson. Temperature distributions in the air film and in the surrounding structure are obtained from the 3D energy equation and appropriate heat equations. In order to reduce the computational effort of the thermo-elasto-gasdynamic problem, the 3D energy equation and the generalized Reynolds equation are reduced by an averaging approach. The governing equations are solved by a finite element method.
机译:空气箔轴颈轴承是高速,无油涡轮机-ERY应用的重要组成部分。为了优化空气箔轴颈轴承支撑的转子系统的性能,需要详细的数值模型。本文介绍了一种完全耦合的热弹性气体动力轴承模型。使用该模型,在数值上研究了机械预载的三垫空气箔轴颈轴承的热弹性气体动力学行动。此外,完成实验以验证用数值模型获得的结果。 3D热弹性轴承模型包括凸块和顶部箔偏转的描述以及空气薄膜中的压力和温度分布的计算以及周围结构中的温度分布,即在转子中,在轴承中袖子和顶部和凸块箔。根据Reissner的非线性梁壳理论描述了凸块和顶箔偏转。该模型考虑了凸块和顶部箔之间的接触以及凸块箔和轴承套管之间。通过根据Dowson求解广义雷诺等式来计算压力分布。空气膜和周围结构中的温度分布从3D能量方程和适当的热方程获得。为了减少热弹性气体动力学问题的计算工作,通过平均方法减少了3D能量方程和广义雷诺等式。通过有限元方法解决了控制方程。

著录项

  • 来源
    《Mechanical systems and signal processing》 |2021年第2期|107221.1-107221.32|共32页
  • 作者单位

    Technical University of Darmstadt Department of Mechanical Engineering Institute of Applied Dynamics Otto-Berndt-Strasse 2 64287 Darmstadt Germany;

    Technical University of Darmstadt Department of Mechanical Engineering Institute of Applied Dynamics Otto-Berndt-Strasse 2 64287 Darmstadt Germany;

    Technical University of Darmstadt Department of Mechanical Engineering Institute of Applied Dynamics Otto-Berndt-Strasse 2 64287 Darmstadt Germany;

  • 收录信息
  • 原文格式 PDF
  • 正文语种 eng
  • 中图分类
  • 关键词

    Air Foil Bearings; Thermo-Elasto-Gasdynamics; Reduction Approaches; Temperature Measurements;

    机译:空气铝箔轴承;Thermo-Elasto-Gasdynamics;减少方法;温度测量;
  • 入库时间 2022-08-18 21:16:17

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