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Low cycle fatigue life prediction in shot-peened components of different geometries - part Ⅱ: life prediction

机译:不同几何形状喷丸元件的低周疲劳寿命预测-第二部分:寿命预测

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This study investigates the effects of shot peening on the low-cycle fatigue performance of a low-pressure steam turbine blade material. The finite element model incorporating shot-peening effects, which has been introduced in part Ⅰ, has been used to predict the stabilised stress/strain state in shot-peened samples during fatigue loading. The application of this model has been extended to different notched geometries in this study. Based on the modelling results, both the Smith-Watson-Topper and Fatemi-Socie critical plane fatigue criteria have been used to predict the fatigue life of shot-peened samples (treated with two different peening intensities) with varying notched geometries. A good agreement between experiments and predictions was obtained. The application of a critical distance method considering the stress and strain hardening gradients near the shot-peened surface has been found to improve the life prediction results. The effects of surface defects on the accuracy of life predictions using the proposed method were also discussed.
机译:这项研究调查了喷丸处理对低压蒸汽轮机叶片材料的低周疲劳性能的影响。 Ⅰ部分引入了包含喷丸效应的有限元模型,用于预测疲劳载荷下喷丸样品的稳定应力/应变状态。在本研究中,该模型的应用已扩展到不同的槽口几何形状。根据建模结果,Smith-Watson-Topper和Fatemi-Socie临界平面疲劳标准已用于预测具有不同槽口几何形状的喷丸处理样品(用两种不同的喷丸强度处理)的疲劳寿命。实验和预测之间取得了良好的一致性。已经发现,考虑抛丸表面附近的应力和应变硬化梯度的临界距离方法的应用可以改善寿命预测结果。还讨论了表面缺陷对使用该方法的寿命预测精度的影响。

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