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Fatigue Crack Growth in a Solid Circular Shaft Under Fully Reversed Rotating Bending

机译:完全反向旋转弯曲下实心圆轴的疲劳裂纹扩展

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摘要

The axle of a load train failed after 5.37 × 10~6 cycles from its service. Macro-fractography showed clearly the fatigue fracture. The stress distribution in the shaft revealed that the maximum alternating stress was considerably less than the material modified fatigue limit obtained at 10~7 cycles from the S-N diagram. Micro-fractography reported from the metallurgical laboratory proved the existence of a surface flaw. Ultimately, fatigue crack growth simulation was performed based on the simple Paris-Erdogan model for estimating the fatigue life of the defective axle. The results showed that the actual life of the axle could be satisfactorily predicted by means of the Paris-Erdogan model.
机译:负载列车的轴在其运行后的5.37×10〜6个循环后失效。宏观形貌清晰地显示出疲劳断裂。轴中的应力分布表明,最大交变应力明显小于从S-N图获得的在10〜7个循环中进行的材料修正疲劳极限。冶金实验室报道的微形貌证明了表面缺陷的存在。最终,基于简单的Paris-Erdogan模型进行了疲劳裂纹扩展模拟,以估计有缺陷的车轴的疲劳寿命。结果表明,通过Paris-Erdogan模型可以令人满意地预测轴的实际寿命。

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