首页> 外文会议>ASME turbo expo: turbomachinery technical conference and exposition >CONCEPTUAL FLUTTER ANALYSIS OF LABYRINTH SEALS USING ANALYTICAL MODELS. PART Ⅱ: PHYSICAL INTERPRETATION
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CONCEPTUAL FLUTTER ANALYSIS OF LABYRINTH SEALS USING ANALYTICAL MODELS. PART Ⅱ: PHYSICAL INTERPRETATION

机译:使用分析模型对拉贝林密封进行概念颤振分析。第二部分:物理解释

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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 and Abbot, 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 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.
机译:提出了一个简单的无量纲模型来描述迷宫式密封件的颤振起伏。使用了代表翅片间密封腔的控制体积的线性化方程,该方程保留了由密封振动产生的周向非稳态流动扰动。首先,假定下游鳍被阻塞,而在第二步中,该模型针对非阻塞出口条件进行了概括。推导了无量纲的每周期工作的解析表达式。结论是,两片式密封件的稳定性取决于三个无量纲的参数,这些参数可以全面解释密封件的颤动行为。这些参数以紧凑且相互关联的形式考虑了压力比,腔体几何形状,翅片间隙,节点直径,流体旋流速度,振动频率和扭转中心位置的影响。通过彻底检查每个周期的工作表达(已被其他作者称为稳定性参数)得出了许多结论。已经发现,问题的物理性很大程度上取决于无量纲的声频。当密封腔的放电时间远大于声传播时间时,系统的阻尼非常小,并且在共振条件下的响应幅度也很高。该模型不仅为Ehrich和Abbot推导的稳定性标准提供了统一的框架,而且为两翅片旋转密封件的每周期工作量提供了明确的表达方式。尽管模型简单,但所有现有的和完善的工程趋势都包含在模型中。最后,包括流体中的涡旋效应。已经发现,翅片间腔中的流体的涡旋引起共振频率的校正并且使稳定区域移动。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对物理效应进行分组。本文的第一部分详细介绍了理论模型的推导,并得出了一些初步结论。第二部分深入分析了模型的含义,并概述了多腔密封的扩展。

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