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Study of alternatives and experimental validation for predictions of hole- edge fatigue crack growth in 42CrMo4 steel

机译:预测42CrMo4钢孔边缘疲劳裂纹扩展的替代方法和实验验证的研究

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The objective of this work is to establish pertinent criteria allowing an optimal alternative to be chosen for calculating the inputs needed to make Run/Repair/Replace decisions and to program inspection plans for cracked wind turbine bearing rings. With this aim, the growth of a hole-edge through-crack was predicted analytically, simulated and measured in a 42CrMo4 steel plate subjected to mode-I cyclic loading. Different alternative procedures according to BS 7910:2013 fitness-for-service code were implemented. Unexpectedly, the numerical calculation of the local stresses in the uncracked body did not improve the estimations of the critical crack length and the number of cycles to failure performed following purely analytical alternatives. That alternative underestimated the critical crack length by 50%. Among the alternatives studied, the one based on numerically calibrated stress intensity factors and crack growth coefficients characterized at the corresponding stress ratios proved to be the most suitable one. Following that alternative, the fatigue life was found to be overestimated by 3.96% in the best scenario whereas the critical crack length was underestimated with an error less than 3%, determined using the Failure Assessment Diagram (FAD) as a failure criterion.
机译:这项工作的目的是建立相关的标准,以便为计算运行/修理/更换决策以及为破裂的风力涡轮机轴承套圈制定检查计划所需的输入,选择最佳的替代方案。出于这个目的,在承受I型循环载荷的42CrMo4钢板中,分析,模拟和测量了孔边缘贯穿裂纹的生长。实施了根据BS 7910:2013适用性服务规范的不同替代程序。出乎意料的是,在未破裂的物体中进行局部应力的数值计算并不能改善对临界裂缝长度的估计以及根据纯粹的分析方法执行的破坏循环次数。该替代方案将临界裂纹长度低估了50%。在研究的替代方案中,一种基于数字校准应力强度因子和以相应应力比为特征的裂纹扩展系数的方案被证明是最合适的方案。采用该替代方法后,在最佳情况下,疲劳寿命被高估了3.96%,而临界裂纹长度被低估了,误差小于3%(使用故障评估图(FAD)作为故障准则确定)。

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