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Dynamics of turbine rotor's rub-impact with model accounting for Alford forces

机译:考虑Alford力模型的涡轮转子碰摩动力学

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Dynamics of rotor-to-stator rub-impact has been widely discussed with simplified models, namely pure structural model of a Jeffcott rotor under imbalance. However, study on this problem with comprehensive models that represent better the actual operation conditions than the simplified models has hardly been seen in literatures. This paper initiates an investigation on this subject. Three component models, including an Alford force model, a rub-impact force model and an imbalance force model, are presented. A global rotordynamic model, which incorporates the Alford forces into the restoring force and considers the imbalance forces and rub-impact forces as excitations, is developed with a multi-turbine-rotor system as physical prototype. The global model is solved with the fourth-order Runge-Kutta method. The dynamic properties represented by the solved response are demonstrated by means of bifurcation diagrams, waveforms, frequency spectrums, orbits, and Poincare maps. Conclusions are summarized in the end. It is believed that the conclusions should make sense to the dynamical design and fault diagnosis of turbomachinery.
机译:已经用简化模型广泛讨论了转子到定子的摩擦冲击动力学,即不平衡状态下的Jeffcott转子的纯结构模型。然而,在文献中几乎没有发现用比简化模型更好的代表实际操作条件的综合模型来研究这个问题。本文就这一主题展开了调查。提出了三部分模型,包括Alford力模型,摩擦力模型和不平衡力模型。使用多涡轮机-转子系统作为物理原型,开发了一个全局转子动力学模型,该模型将Alford力纳入恢复力,并将不平衡力和摩擦力视为激励。使用四阶Runge-Kutta方法求解全局模型。通过分叉图,波形,频谱,轨道和庞加莱图证明了所求解响应所表示的动态特性。最后总结了结论。相信这些结论对涡轮机械的动力学设计和故障诊断是有意义的。

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