首页> 外文会议>PID-vol.9; ASME International Mechanical Engineering Congress and Exposition; 20041113-19; Anaheim,CA(US) >STATISTICAL ANALYSIS OF DAMPER SEAL CLEARANCE DIVERGENCE AND IMPACT UPON ROTORDYNAMIC STABILITY
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STATISTICAL ANALYSIS OF DAMPER SEAL CLEARANCE DIVERGENCE AND IMPACT UPON ROTORDYNAMIC STABILITY

机译:阻尼器密封间隙散度和对转子动态稳定性的影响的统计分析

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摘要

Rotordynamic stability in a high-speed, high-pressure centrifugal compressor is achieved through introducing stabilizing forces and managing destabilizing forces. It becomes the original equipment manufacturer's (OEM) responsibility to provide sufficient stabilizing influence to ensure acceptable operational behavior. A variety of mechanisms exist to provide stability: damper bearings, de-swirl elements on seals, shunt holes and damper seals are commonly provided by the compressor manufacturer to combat instability. The application of damper seals provides a significant increase in rotordynamic stability if designed properly. A previous case study (Camatti, et. al. [1]) presented the detrimental effect of damper seal clearance divergence and seal gas pre-swirl upon predicted stability. Accurate prediction of rotordynamic stability requires knowledge of the destabilizing influences, and evaluation of the variation possible in the stability promoting elements. In particular, the damper seal can be strongly influenced by the presence of divergence in the seal-to-rotor clearance and can result in unexpected at-load behavior. One approach to ensure stable operation is to perform a "worst case" evaluation. However, this often results in excessive compromise (large seal clearance and impact on aerodynamic performance) to "eliminate" the possibility of unstable operation. A different and new approach is to define an acceptable envelope of probability. This study presents a statistical evaluation of the impact of damper seal clearance divergence, along with other compressor design parameters, and provides a method for ensuring stable operation regardless of manufacturing or operational variation. The logarithmic decrement is evaluated as a function of compressor design values and a statistical response surface is created. From the response surface and defined variation in design values, a measure of probability for instability can be obtained. Allowable parameter variation can be restricted to ensure stable operation. Three case studies will be presented where the potential for instability exists and the risk quantified using this statistical technique. Additionally, in one of these cases, test results are presented to support the analytical work.
机译:高速,高压离心压缩机的转子动力学稳定性是通过引入稳定力和控制不稳定力来实现的。提供足够的稳定影响以确保可接受的操作行为成为原始设备制造商(OEM)的责任。存在多种提供稳定性的机制:阻尼器轴承,密封件上的防旋流元件,分流孔和阻尼器密封件通常由压缩机制造商提供以应对不稳定。如果设计得当,减震器密封件的应用将大大提高转子的动力稳定性。先前的案例研究(Camatti等人[1])提出了阻尼器密封间隙发散和密封气体预旋流对预测稳定性的不利影响。转子动态稳定性的准确预测需要了解不稳定因素的影响,并需要评估稳定性促进元件中可能出现的变化。尤其是,阻尼器密封件会受到密封件与转子间隙中存在差异的强烈影响,并可能导致意外的空载行为。确保稳定运行的一种方法是执行“最坏情况”评估。但是,这通常会导致过度的折衷(较大的密封间隙和对空气动力性能的影响),以“消除”不稳定运行的可能性。另一种不同的新方法是定义可接受的概率包络。这项研究提出了对阻尼器密封间隙偏差影响的统计评估,以及其他压缩机设计参数,并提供了一种确保稳定运行的方法,无论制造或运行变化如何。根据压缩机设计值评估对数减量,并创建统计响应面。从响应面和定义的设计值变化中,可以获得不稳定性概率的度量。可以限制允许的参数变化以确保稳定运行。将提供三个案例研究,其中存在潜在的不稳定因素,并使用此统计技术量化风险。此外,在其中一种情况下,会提供测试结果以支持分析工作。

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