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Fatigue life prediction of additively manufactured material: Effects of surface roughness, defect size, and shape

机译:增材制造材料的疲劳寿命预测:表面粗糙度,缺陷尺寸和形状的影响

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In this paper, the effects of process-induced voids and surface roughness on the fatigue life of an additively manufactured material are investigated using a crack closure-based fatigue crack growth model. Among different sources of damage under cyclic loadings, fatigue because of cracks originated from voids and surface discontinuities is the most life-limiting failure mechanism in the parts fabricated via powder-based metal additive manufacturing (AM). Hence, having the ability to predict the fatigue behaviour of AM materials based on the void features and surface texture would be the first step towards improving the reliability of AM parts. Test results from the literature on Inconel 718 fabricated via a laser powder bed fusion (L-PBF) method are analysed herein to model the fatigue behaviour based on the crack growth from semicircular/ellip-tical surface flaws. The fatigue life variations in the specimens with machined and as-built surface finishes are captured using the characteristics of voids and surface profile, respectively. The results indicate that knowing the statistical range of defect size and shape along with a proper fatigue analysis approach provides the opportunity of predicting the scatter in the fatigue life of AM materials. In addition, maximum valley depth of the surface profile can be used as an appropriate parameter for the fatigue life prediction of AM materials in their as-built surface condition.
机译:在本文中,使用基于裂纹闭合的疲劳裂纹扩展模型研究了工艺引起的空隙和表面粗糙度对增材制造材料疲劳寿命的影响。在循环载荷下的不同损坏来源中,由粉末和表面不连续性引起的裂纹引起的疲劳是通过粉末基金属增材制造(AM)制造的零件中寿命最长的失效机理。因此,具有基于空隙特征和表面纹理来预测AM材料的疲劳行为的能力将是提高AM零件可靠性的第一步。本文分析了通过激光粉末床熔合(L-PBF)方法制造的Inconel 718文献的测试结果,以基于基于半圆形/椭圆形表面缺陷的裂纹扩展对疲劳行为进行建模。分别使用空隙和表面轮廓的特征来捕获具有机械加工表面和竣工表面光洁度的样品的疲劳寿命变化。结果表明,了解缺陷尺寸和形状的统计范围以及适当的疲劳分析方法可提供预测AM材料疲劳寿命中的分散的机会。此外,表面轮廓的最大谷底深度可以用作预测AM材料在其建成状态下的疲劳寿命的适当参数。

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