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Shrink fit effects on rotordynamic stability: experimental and theoretical study

机译:收缩拟合对转子动态稳定性的影响:实验和理论研究

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摘要

This dissertation presents an experimental and theoretical study of subsynchronousrotordynamic instability in rotors caused by interference and shrink fitinterfaces. The experimental studies show the presence of strong unstable subsynchronousvibrations in two different rotor setups with interference and shrink fitinterfaces that were operated above their first critical speeds. The unstable vibrationsoccur at the first natural frequency of the rotor-bearing system. The instability causedcomplete wreckage of the test rig in one of the setups showing that these vibrations arepotentially dangerous to the safe operation of rotating machines. The two different rotorsetups that are studied are a single-disk rotor mounted on a uniform diameter shaft and atwo-disk rotor with an aluminum sleeve shrink fitted to it at the outer surface of the twodisks. In the single-disk rotor, an adjustable interference arrangement between the diskand the shaft is obtained through a tapered sleeve arrangement, which acts as theinterference fit joint. The unstable sub-synchronous vibrations originate from slippagein the shrink fit and the interference fit interfaces that develop friction forces, which actas destabilizing cross-coupled moments when the rotor is operated above its first criticalspeed. The unique contribution offered through this work is the experimental validationof a physically correct model of internal friction which models the destabilizing mechanism as a system of cross-coupled internal moments at the shrink fit interface. Thedissertation describes stability simulations of various test rotor setups using the correctinternal moments model. A commercial finite-element based software called XLTRCTMis used to perform rotordynamic simulations for stability studies. The method of stabilitystudy is the computation of eigenvalues of the rotor-bearing system. A negative real partof the eigenvalue indicates instability. The simulations include the test rotors that wereexperimentally observed as stable and unstable with shrink and interference fit interfacesin their assemblies. The dissertation also describes the simulations of various imaginedrotor configurations with shrink fit interfaces, and seeks to explain how configurationsdiffer on rotordynamic stability depending upon several rotor-bearing parameters such asgeometry and elastic properties, as well as upon the amount of internal frictionparameters, which differ from configuration to configuration.
机译:本文提出了由干涉和热缩配合界面引起的转子亚同步转子动力不稳定性的实验和理论研究。实验研究表明,在两种不同的转子设置中,存在过强的不稳定亚同步振动,且过盈配合和收缩配合界面在其第一临界速度以上运行。不稳定的振动发生在转子轴承系统的第一固有频率处。在其中一种设置中,这种不稳定性导致测试设备完全残骸,表明这些振动可能对旋转机械的安全运行造成危险。研究的两种不同的转子设置是:单盘转子,其安装在直径均匀的轴上;双盘转子,其铝套收缩安装在两个盘的外表面上。在单盘式转子中,通过锥形套筒装置获得了在盘与轴之间的可调干涉装置,该锥形套筒装置用作干涉配合接头。不稳定的次同步振动是由收缩配合和过盈配合界面中的滑动引起的,这些界面产生了摩擦力,当转子以高于其第一临界速度的速度运转时,这会破坏交叉耦合力矩的稳定性。通过这项工作提供的独特贡献是对物理上正确的内部摩擦模型进行了实验验证,该模型将去稳定机制建模为在收缩配合界面处的交叉耦合内部力矩系统。本文描述了使用正确的内部力矩模型对各种测试转子装置进行稳定性仿真的方法。一种基于商业有限元软件,称为XLTRCTM,用于执行转子动力学仿真,以进行稳定性研究。稳定性研究的方法是计算转子轴承系统的特征值。特征值的负实部表示不稳定。仿真包括试验转子,实验转子在组件中具有收缩和过盈配合界面,被视为稳定和不稳定。论文还描述了具有收缩配合界面的各种想象中的转子结构的仿真,并试图解释该结构如何根据转子轴承的一些参数(例如几何形状和弹性特性以及内部摩擦参数的数量)而对转子动态稳定性有所不同。配置到配置。

著录项

  • 作者

    Jafri Syed Muhammad Mohsin;

  • 作者单位
  • 年度 2007
  • 总页数
  • 原文格式 PDF
  • 正文语种 en_US
  • 中图分类

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