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SIMPLIFIED FATIGUE DAMAGE AND CRACK GROWTH CALCULATIONS FOR WIND TURBINES

机译:风力涡轮机简化的疲劳损伤和裂纹增长计算

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Estimating fatigue life of wind turbine components, where the loading and structural response are random, can be a difficult task. The life estimate is sensitive to rare large loads and can be influenced by the sequence of load applications. Sequence effects in fatigue crack initiation and crack growth are outlined. A simplified model for sequence effects in crack growth is presented along with model predictions of an American Society for Testing and Materials (ASTM) crack growth test series. The relative importance of including these effects in fatigue calculations is discussed. Analytical solutions for the time to crack initiation and crack growth provide quick estimates of fatigue life by approximating the loading as a narrow-band Gaussian process and by neglecting sequence effects. This approximation is both conservative and within the usual scatter in fatigue life estimates due to material variability. It is therefore a useful tool in estimating fatigue life, especially when turbine response data is limited.
机译:估计风力涡轮机组件的疲劳寿命,其中装载和结构响应是随机的,可以是一项艰巨的任务。生命估计对罕见的大负载敏感,并且可以受到负载应用序列的影响。概述了疲劳裂纹引发和裂纹生长的序列效果。提出了一种简化的裂缝增长中的序列效应模型以及美国测试和材料(ASTM)裂纹生长试验系列的模型预测。讨论了在疲劳计算中包括这些影响的相对重要性。裂纹启动和裂纹增长的分析解决方案通过近似装载作为窄带高斯工艺来提供疲劳寿命的快速估计,并通过忽略序列效应来提供疲劳寿命的快速估计。这种近似是保守的,并且在疲劳寿命估计的通常散射内,由于材料变异性。因此,它是估计疲劳寿命的有用工具,尤其是当涡轮响应数据有限时。

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