首页> 外文期刊>Proceedings of the Institution of Mechanical Engineers. Part L, Journal of Materials: Design and Application >Multiaxial fatigue life estimation of defective aluminum alloy considering the microstructural heterogeneities effect
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Multiaxial fatigue life estimation of defective aluminum alloy considering the microstructural heterogeneities effect

机译:考虑微观结构异质性影响的缺陷铝合金多轴疲劳寿命估算

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摘要

The Al-Si-Mg high-cycle fatigue behavior is mainly affected by the microstructural heterogeneities and the presence of casting defects. This attempt aims to develop an analytical approach based on the evaluation of the highly stressed volume caused by local porosities and defined as the affected area methodology. The proposed approach is able to predict the aluminum alloy fatigue response by considering the effect of microstructure described by the secondary dendrite arm spacing and its correlation with the defect size effect. A representative elementary volume model is implemented to evaluate the stress distribution in the vicinity of the defect and to determine its impact on the high-cycle fatigue resistance. Work hardening due to cyclic loading is considered by applying the Lemaitre-Chaboche model. The Kitagawa-Takahashi diagrams corresponding to different microstructures and for two loading ratios: R-sigma = 0 and R-sigma = -1 were simulated based on the AA method. Simulations were compared to the experimental results carried out on cast aluminium alloy A356 with T6 post heat-treatment. The results show clearly that the proposed approach provides a good estimation of the A356-T6 fatigue limit and exhibits good ability in simulating the Kitagawa-Takahashi diagrams for fine and coarse microstructures.
机译:Al-Si-Mg高周疲劳行为主要受微观结构异质性和铸件缺陷的影响。此尝试旨在基于对局部孔隙引起的高应力体积的评估,并定义为受影响区域方法,以开发一种分析方法。所提出的方法能够通过考虑由次要枝晶臂间距描述的微观结构及其与缺陷尺寸效应的相关性来预测铝合金的疲劳响应。使用代表性的基本体积模型来评估缺陷附近的应力分布,并确定其对高周疲劳强度的影响。通过应用Lemaitre-Chaboche模型,可以考虑由于循环载荷而导致的工作硬化。基于AA方法,模拟了对应于不同微观结构和两种载荷比:R-sigma = 0和R-sigma = -1的Kitagawa-Takahashi图。将模拟与在T6后热处理的铸造铝合金A356上进行的实验结果进行了比较。结果清楚地表明,所提出的方法可以很好地估计A356-T6的疲劳极限,并且在模拟精细和粗糙微观结构的Kitagawa-Takahashi图时表现出良好的能力。

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