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Probabilistic Finite Element Analysis of Cooled High-Pressure Turbine Blades-Part B: Probabilistic Analysis

机译:冷却高压涡轮叶片的概率有限元分析 - B部分:概率分析

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Modern high-pressure turbine (HPT) blade design stands out due to high complexity comprising three-dimensional blade features, multipassage cooling system (MPCS), and film cooling to allow for progressive thermodynamic process parameters. During the last decade, probabilistic design approaches have become increasingly important in turbomachinery to incorporate uncertainties such as geometric variations caused by manufacturing scatter. In Part B of this two-part article, real geometry effects are considered within a probabilistic finite element (FE) analysis that aims at sensitivity evaluation. The knowledge about the geometric variability is derived based on a blade population of more than 400 individuals by means of parametric models that are introduced in Part A. The HPT blade population is statistically assessed, which allows for reliable sensitivity analysis and robustness evaluation taking the variability of the airfoil, profiled endwalls (PEWs) at hub and shroud, wedge surfaces (WSFs), and the MPCS into account. The probabilistic method-Monte Carlo simulation (MCS) using an extended Latin hypercube sampling (eLHS) technique-is presented subsequently. Afterward, the FE model that involves thermal, linear-elastic stress, and creep analysis is described briefly. Based on this, the fully automated process chain involving computer-aided design (CAD) model creation, FE mesh morphing, FE analysis, and postprocessing is executed. Here, the mesh morphing process is presented involving a discussion of the mesh quality. The process robustness is assessed and quantified referring to the impact on input parameter correlation. Finally, the result quantities of the probabilistic FE simulation are evaluated in terms of sensitivities. For this purpose, regions of interest are determined, wherein the statistical analysis is conducted to achieve the sensitivity ranking. A significant influence of the considered geometric uncertainties onto mechanical output quantities is observed, which motivates to incorporate these in modern design strategies or robust optimization.
机译:现代高压涡轮机(HPT)刀片设计脱颖而出,由于包括三维刀片特性,多级叶片系统(MPC)和薄膜冷却,允许逐步热力学过程参数。在过去十年中,概率设计方法在涡轮机械中越来越重要,以纳入由制造散射引起的几何变化等不确定性。在该两部分文章的B部分中,实际几何效应被认为是旨在敏感性评估的概率有限元(FE)分析。关于几何变异性的知识基于借助于A部分介绍的参数模型基于400多个单独的叶片群。HPT刀片群在统计上评估,这允许采取可靠性的可靠性敏感性分析和鲁棒性评估翼型,轮毂和护罩,楔形表面(WSF)和MPCS的翼型。随后介绍了使用扩展拉丁超立体采样(ELHS)技术的概率方法蒙特卡罗模拟(MCS)。之后,简要描述涉及热,线性弹性应力和蠕变分析的FE模型。基于此,执行涉及计算机辅助设计(CAD)模型创建,FE网格变形,FE分析和后处理的全自动过程链。这里,呈现涉及对网格质量的讨论的网格变形过程。评估和量化过程鲁棒性,从而提及对输入参数相关的影响。最后,在敏感度方面评估了概率化Fe模拟的结果量。为此目的,确定感兴趣区域,其中进行统计分析以实现敏感性排名。观察到考虑的几何不确定性对机械输出量的显着影响,这激励了这些在现代设计策略或强大的优化中。

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