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Test versus predictions for rotordynamic coefficients and leakage rates of hole-pattern gas seals at two clearances in choked and unchoked conditions

机译:在阻塞和未阻塞条件下两个间隙处的孔型气密封件的转子动力学系数和泄漏率的测试与预测

摘要

This thesis documents the results of high pressure testing of hole-pattern annular gas seals conducted at the Texas A&M University's Turbomachinery Laboratory. The testing conditions were aimed at determining the test seals sensitivity to pressure ratio, inlet fluid preswirl, rotor speed, and rotor to seal clearance. The rotordynamic coefficients showed only small changes resulting from the different pressure ratios tested. Only the damping terms at the lower frequencies showed some influence. One other notable result from the testing of different pressure ratios is that the seals were tested in a choked flow condition, and there was not a significant change in the seal behavior when the seals transitioned to the choked condition. The inlet fluid preswirl only had a notable effect on the cross-coupled stiffness in the larger clearance tests. These results lead to the conclusion that a swirl brake could have some rotordynamic value, but only if the seals have sufficiently large clearance. Conversely this also means that if hole-pattern seals are being implemented with a small clearance, then a swirl brake would not be an effective way to improve the rotordynamic stability of the system. The only significant effect that the rotor speeds had on the rotordynamic coefficients were that the cross-coupled coefficients increased as the rotor speed increased. This is the expected result because as the rotor speed increases there is a greater shear force on the gas as it passes through the seal resulting in more fluid circumferential velocity, which results in stronger cross-coupled coefficients. The changes in clearance resulted in drastic changes in the magnitude of the coefficients. The smaller clearance yielded much higher coefficients than the larger clearance. All of the rotordynamic coefficients were predicted well by ISOTSEAL. The code was found to do a good job predicting the seal leakage as well. This gives more credence to the coefficients and leakage that ISOTSEAL predicts.
机译:本文记录了在德州农工大学的涡轮机械实验室进行的孔型环形气密封件高压测试的结果。测试条件旨在确定测试密封件对压力比,入口流体预旋流,转子速度以及转子到密封件间隙的敏感性。转子动力学系数仅显示出由所测试的不同压力比引起的微小变化。仅低频处的阻尼项显示出一些影响。不同压力比测试的另一个显着结果是,密封件在节流条件下进行了测试,当密封件过渡到节流条件时,密封性能没有明显变化。在较大的间隙测试中,入口流体的预旋流仅对交叉联接的刚度产生显着影响。这些结果得出的结论是,涡旋制动器可能具有一定的转子动力学值,但前提是密封件具有足够大的间隙。相反,这也意味着,如果以较小的间隙实现孔型密封,那么涡流制动器将不是提高系统转子动力学稳定性的有效方法。转子速度对转子动力学系数的唯一重要影响是交叉耦合系数随转子速度的增加而增加。这是预期的结果,因为随着转子速度的增加,气体通过密封件时会对气体产生更大的剪切力,从而导致更大的流体圆周速度,从而导致更强的交叉耦合系数。间隙的变化导致系数幅度的急剧变化。较小的间隙产生的系数要比较大的间隙大得多。通过ISOTSEAL可以很好地预测所有转子动力系数。发现该代码还可以很好地预测密封泄漏。这使ISOTSEAL预测的系数和泄漏更加可信。

著录项

  • 作者

    Wade Jonathan Leigh;

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  • 年度 2004
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  • 原文格式 PDF
  • 正文语种 en_US
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