Stress Analysis of Turbocharger Turbine based on Fluid-Structure Coupling

R. Yan, Zhenlei Chen, Chang Liu, Fengyuan Yang, Yi Hu
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Abstract

In order to study the cracking problem of turbine components under high temperature conditions, a global fluid-structure interaction model was established by numerical simulation method. The temperature field distribution of the turbine casing and the stress distribution of typical components were simulated and analyzed. The comparison with the traditional fluid-structure interaction model was carried out. The results show that the temperature field obtained by the global fluid-solid coupling model is highly consistent with the test results, and is more accurate than the traditional model.The increase of Nozzle Ring assembly stress and Vane expansion stagnation are the main reasons for the cracking of parts under high temperature load, which is the cause of cracking. Research results can provide reference for engineering application analysis of turbine casing failure and part structure optimization.
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基于流固耦合的涡轮增压器应力分析
为了研究高温条件下涡轮部件的开裂问题,采用数值模拟方法建立了涡轮部件的流固耦合全局模型。对涡轮机匣的温度场分布和典型部件的应力分布进行了仿真分析。并与传统流固耦合模型进行了比较。结果表明,采用全局流固耦合模型得到的温度场与试验结果高度吻合,且比传统模型精度更高。喷嘴环总成应力增大和叶片膨胀滞胀是高温载荷作用下零件开裂的主要原因,是导致开裂的原因。研究结果可为涡轮机匣失效的工程应用分析和零件结构优化提供参考。
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