Comparison of a Liquid Annular Seal for Pump Applications With and Without a Swirl Brake

N. E. Balke, D. Childs
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Abstract

An annular seal is an annular clearance between a rotor and a stator within a turbomachine that restricts leakage flow, arising due to the seal’s pressure differential. Annular seals are important for consideration in turbomachinery in that they affect the rotodynamics and stability of the turbomachine. Data were available for a smooth liquid annular seal that had been previously tested with no swirl brakes. The seal was modified by adding slots at the inlet to produce a swirl brake seal. Tests produced static and dynamic data for the swirl brake seal. The swirl brake and unmodified seal data are compared to demonstrate how swirl brakes impact the seal’s rotordynamic performance. Adding a swirl brake to a liquid annular seal increases direct stiffness, decreases cross-coupled stiffness, modestly increases direct damping, reduces cross-coupled damping, and decreases both the direct and cross-coupled virtual mass terms. The measured drop in cross-coupled stiffness via the addition of swirl brakes shows why swirl brakes are effective in remedying rotordynamic instabilities. Results show that varying inlet pre-swirl, or fluid rotation, on a swirl brake seal has little effect on the seal’s dynamic performance characteristics. A notable phenomenon was observed with the direct stiffness. At certain test points the direct stiffness would abruptly increase and decrease when increasing either pressure or running speed. The behavior could be largely explained by transitioning the laminar/transitional/turbulent boundaries.
带和不带涡流制动器的泵用液体环形密封的比较
环形密封是涡轮机械中转子和定子之间的环形间隙,由于密封的压差而产生的泄漏流受到限制。在涡轮机械中,环形密封是重要的考虑因素,因为它影响涡轮机械的旋转动力学和稳定性。在之前没有涡流制动器的情况下,测试了光滑的液体环空密封。通过在进口处增加槽来改进密封,以产生涡流制动密封。试验获得了旋流制动密封的静态和动态数据。将涡流制动器和未修改的密封数据进行比较,以证明涡流制动器如何影响密封的转子动力性能。在液体环空密封中加入涡流制动器可增加直接刚度,降低交叉耦合刚度,适度增加直接阻尼,降低交叉耦合阻尼,并降低直接和交叉耦合虚质量项。通过增加涡流制动器测量的交叉耦合刚度下降表明为什么涡流制动器在纠正转子动力不稳定性方面是有效的。结果表明,改变进口预旋流或流体旋转对旋流制动密封的动态性能影响不大。用直接刚度观察到一个显著的现象。在某些测试点,当压力或运行速度增加时,直接刚度会突然增大和减小。这种行为在很大程度上可以通过层流/过渡/湍流边界的过渡来解释。
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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