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Experimental Investigation of Turbine Blade-Tip Excitation Forces

机译:涡轮叶片尖端励磁力的实验研究

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摘要

This paper presents results of a program to investigate the magnitude and parametric variations of rotordynamic forces which arise in high power turbines due to blade-tip leakage effects. Five different unshrouded turbine configurations and one configuration shrouded with a labyrinth seal were tested with static offsets of the turbine shaft. The forces along and perpendicular to the offset were measured directly with a rotating dynamometer. Exploration of casing pressure and flow velocity distributions was used to investigate the force-generating mechanisms. For unshrouded turbines, the cross-forces originate mainly from the classical Alford mechanism (nonuniform work extraction due to varying blade efficiency with tip gap) while the direct forces arise mainly from a slightly skewed pressure pattern. The Alford coefficient for cross-force was found to vary between 2.4 and 4.0, while the similar direct force coefficient varied from 1.5 to 3.5. The cross-forces are found to increase substantially when the gap is reduced from 3.0% to 1.9% of blade height, probably due to viscous blade-tip effects. The forces also increase when the hub gap between stator and rotor decreases. The force coefficient decreases with operating flow coefficient In the case of the shrouded turbine, most of the forces arise from nonuniform seal pressures. This includes about 80% of the transverse forces. The rest appears to come from uneven work extraction (Alford mechanism). Their level is about 50% higher than in the unshrouded cases.
机译:本文提出了一种程序的结果,以研究由于叶片漏效应导致的高动力涡轮机中出现的旋转动力力的幅度和参数变化。用涡轮轴的静电偏移测试五种不同的未经吸引的涡轮机配置和带有迷宫式密封罩的一种配置。用旋转测功机直接测量沿偏移和垂直于偏移的力。用于探索套管压力和流速分布来研究力产生机构。对于不受欢迎的涡轮机,横向主要来自经典阿尔福德机构(由于具有尖端间隙的不同叶片效率而导致的非均匀工作提取),而直接力主要来自略微偏斜的压力图案。发现跨力的阿尔福德系数在2.4和4.0之间变化,而类似的直接力系数在1.5到3.5之间变化。当间隙从叶片高度的3.0%降低到叶片高度的3.0%至1.9%时,发现横向增加。当定子和转子之间的轮毂间隙减小时,力也会增加。在罩涡轮机的情况下,力系数随运行流量系数而减小,大部分力来自非均匀密封压力。这包括约80%的横向力。其余的似乎来自不均匀的工作提取(阿尔福德机制)。他们的水平高于不受欢迎的案件。

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