某低压汽轮机叶片断裂分析

Ernst Plesiutschnig, Patrick Fritzl, Norbert Enzinger, Christof Sommitsch
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引用次数: 23

摘要

对不同固有频率低压汽轮机叶片第三排根部的裂纹进行了分析。疲劳裂纹萌生的根本原因是铁素体/马氏体锻造X20Cr13材料的点蚀。通过金相分析、有限元分析和断裂力学分析,结合文献中的实验数据,对裂纹扩展应力进行了评估,讨论了运行条件。计算结果表明,涡轮叶片根部的腐蚀坑增加了超过屈服强度的局部应力。通过改变转子转速来激发固有频率不是裂纹扩展的原因。非定常蒸汽力引起的离心载荷和叠加弯曲载荷是裂纹扩展的主要原因。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Fracture analysis of a low pressure steam turbine blade

Cracks were analysed at the root of the third blade row of low-pressure steam turbine blades of different natural frequencies. The root cause of the fatigue crack initiation was pitting corrosion of the forged ferritic/martensitic X20Cr13 material. Metallographic investigations, finite element analysis and fracture mechanics analysis combined with experimental data from the literature are used to evaluate crack propagating stresses to discuss the operating conditions. The calculations show that corrosion pits at the root of the turbine blade increase the local stresses above yield strength. Excitation of natural frequencies by changing the rotor speed is not responsible for the crack propagation. The centrifugal load and superimposed bending load caused by unsteady steam forces are responsible for the crack propagation.

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