Fatigue life prediction of mistuned steam turbine blades subjected to deviations in blade geometry

Makgwantsha Mashiachidi, Dawood Desai
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Abstract

The blades of the steam turbine are subjected to bending of the steam flow, centrifugal loading, vibration response, and structural mistuning. These factors mentioned contribute significantly to the fatigue failure of steam turbine blades. Low pressure (LP) steam turbines experience premature blade and disk failures due to the stress concentrations in the root location of the blade of its bladed disk. This study of mistuned steam turbine blades subjected to variation in blade geometry will be of great significance to the electricity generation industry. A simplified, mistuned, scaled-down steam turbine bladed disk model was developed using ABAQUS finite element analysis (FEA) software. The acquisition of the vibration characteristics and steady-state stress response of the disk models was carried out through FEA. Such studies are very limited. Subsequently, 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. Vibration characteristics and response of the variation of the geometric blade of the steam turbine were investigated. Natural FEA frequencies compared well with the published literature of real steam turbines, indicating the reliability of the developed FEA model. The study found that fatigue life is most sensitive to changes in blade length, followed by width and then thickness, in this order. Analytical life cycles and Fe-Safe software show a percentage difference of less than 4.86%. This concludes that the numerical methodology developed can be used for real-life mistuned steam turbine blades subjected to variations in blade geometry.
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叶片几何偏差下失谐汽轮机叶片疲劳寿命预测
汽轮机叶片受到蒸汽流弯曲、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。低压汽轮机由于叶片盘叶片根部的应力集中,导致叶片盘过早失效。研究汽轮机失谐叶片几何形状变化对发电工业具有重要意义。利用ABAQUS有限元分析软件建立了简化、失谐、按比例缩小的汽轮机叶片盘模型。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。这样的研究非常有限。随后,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。研究了汽轮机叶片几何形状变化的振动特性及响应。实际汽轮机的自然有限元频率与已发表的文献比较,表明所建立的有限元模型是可靠的。研究发现,疲劳寿命对叶片长度的变化最为敏感,其次是宽度,然后是厚度。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。
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