Prediction of fatigue life of mistuned steam turbine blades subjected to variations in blade geometry

Makgwantsha Mashiachidi, Dawood Desai
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Abstract

There is a large number of power stations suffering from fatigue failures of the steam turbine blades. The steam turbine blades are also subjected to steam flow bending, centrifugal loading, vibration response, and structural mistuning. These mentioned factors significantly contribute to the fatigue failure of the steam turbine blades. Low-Pressure (LP) steam turbines experience premature blade and disk failures due to the stress concentrations at the blade root area of its bladed disk. Driven by the problems encountered by the steam power plant electricity generating utilities with regards to steam turbine blades fatigue failure, this study of the mistuned steam turbine blades subjected to variation in blade geometry will be of great significance to the electricity generation industry. A simplified, scaled-down mistuned steam turbine bladed disk model was developed using ABAQUS finite element analysis (FEA) software. Acquisition of the vibration characteristics and steady-state stress response of the disk models was performed through FEA. Thereafter, numerical stress distributions were acquired, and the model was subsequently exported to Fe-Safe software for fatigue life calculations based on centrifugal and harmonic sinusoidal pressure loading. The vibration characteristics and the response of the variation steam turbine geometric blade was conducted. The FEA natural frequencies compared well with published literature of the real steam turbines indicating reliability of the developed FEA model. The study found that the fatigue life is most sensitive to changes in blade length, followed by the width, and then the thickness, in this order. The analytical life cycles and Fe-Safe software shows the percentage difference of less than 4.86%. This concludes that the developed numerical methodology can be used for real-life mistuned steam turbine blades subjected to variations in blade geometry.
叶片几何形状变化下失谐汽轮机叶片疲劳寿命的预测
有大量的电站存在汽轮机叶片疲劳失效的问题。汽轮机叶片还受到蒸汽流弯曲、离心载荷、振动响应和结构失谐的影响。这些因素是汽轮机叶片疲劳失效的重要原因。低压(LP)汽轮机由于叶片根部区域的应力集中导致叶片和圆盘过早失效。由于蒸汽发电厂发电设施所遇到的汽轮机叶片疲劳失效问题,因此对叶片几何形状变化的失谐汽轮机叶片的研究将对发电行业具有重要意义。利用ABAQUS有限元分析软件建立了一个简化的、按比例缩小的失谐汽轮机叶片盘模型。通过有限元分析获取了圆盘模型的振动特性和稳态应力响应。然后,获得数值应力分布,并将模型导出到Fe-Safe软件中,进行离心和谐波正弦压力载荷下的疲劳寿命计算。研究了变型汽轮机几何叶片的振动特性和响应。实际汽轮机的有限元分析固有频率与已发表的文献比较良好,表明所建立的有限元模型是可靠的。研究发现,叶片的疲劳寿命对叶片长度的变化最为敏感,其次是叶片宽度,最后是叶片厚度。分析生命周期和Fe-Safe软件的百分比差异小于4.86%。由此得出结论,所开发的数值方法可用于实际生活中受叶片几何形状变化影响的失谐汽轮机叶片。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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