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Calculation of leakage and dynamic coefficients of stepped labyrinth gas seals

机译:阶梯式迷宫式气封泄漏量和动态系数的计算

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摘要

Rotor-fluid interactions can cause self-excited vibrations in high-density turbomachines. One of the most important sources for excitation is the flow through labyrinth seals. The gas flow through the seals creates net pressure and shear forces acting on the rotor. It is necessary to predict these forces exactly for reliably operating turbomachines. The labyrinth seal forces are characterized by rotordynamic coefficients. This paper presents a theoretical work on the calculation of leakage and dynamic coefficients for stepped labyrinth gas seals. The continuity and circumferential momentum equations are given for compressible flow in a stepped labyrinth seal. Periodic and analytic solutions of these equations are obtained for the case of time dependent flow generated by a non-axisymmetric rotation of the rotor using an axisymmetric solution based on different assumption about the flow coefficient. The rotordynamic coefficients are then calculated and the results of this analysis are compared with relatively recent experimental data. (C) 2003 Elsevier Inc. All rights reserved.
机译:转子-流体相互作用会导致高密度涡轮机中的自激振动。激励最重要的来源之一是通过迷宫式密封件的流动。通过密封件的气流会产生作用在转子上的净压力和剪切力。为了可靠地操作涡轮机,必须准确预测这些力。迷宫式密封力由转子动力学系数表征。本文介绍了关于阶梯式迷宫式气密封件泄漏和动态系数计算的理论工作。给出了迷宫式密封中可压缩流的连续性和周向动量方程。对于基于时间的流,该流是基于转子流量的非轴对称旋转而生成的,这些时间依赖于流量,该轴依赖于关于流量系数的不同假设,使用轴对称解。然后计算转子动力系数,并将分析结果与相对较新的实验数据进行比较。 (C)2003 Elsevier Inc.保留所有权利。

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