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Crack Growth Simulation and Residual Life Assessment of Freight Wheel

机译:货运轮船的裂缝增长模拟与剩余寿命评估

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Typical fatigue cracks at wheel web holes propagate under a combination of mechanical forces and braking thermal loads. The stress intensity factors (SIF) for different crack sizes are calculated using the approach of 1/4 node displacement and sub-model techniques. The commercial finite element code ANSYS is used for modeling and 3-D prismatic quarter point 20-node isoparametric degenerate singular elements are adopted for the region near the crack tip. Models on fatigue crack growth and residual life prediction are presented with help of Forman equation. Values of crack growth rate and residual life for a wheel worn by 20mm are finally given.The study indicates that the combination of mechanical forces and grade-braking thermal loads lead to the crack growth of the web hole and the propagation period of the crack less than 15mm can be ensured 3 years at least with the routine inspections. This provides fundamental data for setting up inspection plans and assessing the replacement period of the wheel.
机译:车轮孔的典型疲劳裂缝在机械力和制动热负荷的组合下传播。使用1/4节点位移和子模型技术的方法计算不同裂缝尺寸的应力强度因子(SIF)。商业有限元代码ANSYS用于建模,并且在裂纹尖端附近的区域采用了3-D棱镜四分之一点20节点等峰值等偏离的奇异元件。疲劳裂纹生长和剩余寿命预测的模型借助于Forman方程提出。最终给出20mm磨损的车轮的裂纹生长速率和剩余寿命的值。研究表明,机械力和等级制动热负荷的组合导致腹板的裂纹生长和裂缝的传播周期较少至少可以通过常规检查确保15毫米。这提供了用于设置检查计划并评估车轮的更换时段的基本数据。

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