Conceptual Flutter Analysis of Labyrinth Seals Using Analytical Models: Part II — Physical Interpretation

A. Vega, R. Corral
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引用次数: 5

Abstract

A simple non-dimensional model to describe the flutter onset of labyrinth seals is presented. The linearized equations for a control volume which represents the inter-fin seal cavity, retaining the circumferential unsteady flow perturbations created by the seal vibration, are used. Firstly, the downstream fin is assumed to be choked, whereas in a second step the model is generalized for unchocked exit conditions. An analytical expression for the non-dimensional work-per-cycle is derived. It is concluded that the stability of a two-fin seal, depends on three non-dimensional parameters, which allow explaining seal flutter behaviour in a comprehensive fashion. These parameters account for the effect of the pressure ratio, the cavity geometry, the fin clearance, the nodal diameter, the fluid swirl velocity, the vibration frequency and the torsion center location in a compact and interrelated form. A number of conclusions have been drawn by means of a thorough examination of the work-per-cycle expression, also known as the stability parameter by other authors. It was found that the physics of the problem strongly depends on the non-dimensional acoustic frequency. When the discharge time of the seal cavity is much greater than the acoustic propagation time, the damping of the system is very small and the amplitude of the response at the resonance conditions is very high. The model not only provides a unified framework for the stability criteria derived by Ehrich [1] and Abbot [2], but delivers an explicit expression for the work-per-cycle of a two-fin rotating seal. All the existing and well established engineering trends are contained in the model, despite its simplicity. Finally, the effect of swirl in the fluid is included. It is found that the swirl of the fluid in the inter-fin cavity gives rise to a correction of the resonance frequency and shifts the stability region. The non-dimensionalization of the governing equations is an essential part of the method and it groups physical effects in a very compact form. Part I of the paper[3] detailed the derivation of the theoretical model and drew some preliminary conclusions. Part II analyzes in depth the implications of the model and outlines the extension to multiple cavity seals.
使用分析模型的迷宫密封的概念颤振分析:第二部分-物理解释
提出了一个简单的无量纲模型来描述迷宫式密封的颤振发作。控制体积的线性化方程代表了翅片间密封腔,保留了密封振动引起的周向非定常流动扰动。首先,假设下游翅片被阻塞,然后在第二步将模型推广到无阻塞出口条件。导出了无量纲每周期工作量的解析表达式。结论是,双翅片密封的稳定性取决于三个非三维参数,这可以全面地解释密封的颤振行为。这些参数将压力比、腔体几何形状、翅片间隙、节直径、流体旋流速度、振动频率和扭转中心位置的影响以紧凑而相互关联的形式反映出来。其他作者通过对工作周期表达式(也称为稳定性参数)的彻底检查,得出了许多结论。结果表明,该问题的物理性质强烈依赖于无量纲声频率。当密封腔的放电时间远大于声传播时间时,系统的阻尼很小,共振条件下的响应幅值很高。该模型不仅为Ehrich[1]和Abbot[2]导出的稳定性准则提供了统一的框架,而且为双翅片旋转密封的每周期工作提供了明确的表达式。尽管模型很简单,但所有现有的和建立良好的工程趋势都包含在模型中。最后,考虑了流体中旋流的影响。研究发现,流体在翅间腔内的旋流会引起共振频率的修正,并使稳定区域发生位移。控制方程的无量纲化是该方法的重要组成部分,它以非常紧凑的形式将物理效应分组。论文[3]第一部分详细推导了理论模型,并得出了一些初步结论。第二部分深入分析了该模型的含义,并概述了扩展到多腔密封。
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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