Trombley Megan, Birnbaum Andrew, Allison John
Department of Materials Science and Engineering, University of Michigan, Ann Arbor, MI, 48109, USA.
Materials Science and Technology Division, United States Naval Research Laboratory, Washington, DC, 20375, USA.
Sci Rep. 2025 Apr 18;15(1):13385. doi: 10.1038/s41598-025-97031-1.
In this investigation, the influence of section diameter on high cycle fatigue (HCF) behavior of additively manufactured 316 L stainless steel was characterized. Three gauge-section diameters (5.0 mm, 2.5 mm, and 1.5 mm) were examined for their influence on the ultrasonic fatigue response of samples built via laser-powder bed fusion (L-PBF). HCF was conducted under full reversed loading (R=-1) conditions. A total of 130 specimens were characterized in the as-built state at maximum stresses ranging from 70 to 220 MPa. A Random Fatigue Limit (RFL) model using a Maximum Likelihood Estimation (MLE) was used to quantify statistical variability and estimate an S-N curve fit. The fatigue response shows that the largest gauge diameter (5.0 mm) resulted in the lowest fatigue strength at 89.5 ± 5.6 MPa, and the smallest diameter (1.5 mm) resulted in the highest fatigue strength at 122.0 ± 32.8 MPa. The 2.5 mm diameter specimens exhibited a fatigue strength of 98.7 ± 7.0 MPa. The primary failure mechanism in all as-built specimens was surface initiated cracking from crevices in the as-built surface finish. Additional specimens with a nominal diameter of 5.0 mm were fatigue tested with the as-built surface removed via low stress surface grinding. The fatigue strength of these samples increased to 170 MPa when 75 μm of the surface was removed and 179 MPa when the surface contour was entirely removed. Residual stresses were characterized by x-ray diffraction (XRD) and show a reduced axial residual stress with reduction in gauge diameter. Additional specimens were fatigue tested after undergoing a stress relief anneal, resulting in a 51% reduction in the residual stress and a 30% improvement in fatigue strength. An in-depth analysis of the microstructure, surface roughness, defects, and fracture surface indicate that both the surface condition and residual stress are the primary factors influencing the observed diameter effects on HCF.
在本研究中,表征了截面直径对增材制造316L不锈钢高周疲劳(HCF)行为的影响。研究了三种标距段直径(5.0毫米、2.5毫米和1.5毫米)对通过激光粉末床熔融(L-PBF)制造的样品超声疲劳响应的影响。高周疲劳试验在完全反向加载(R = -1)条件下进行。总共130个试样在最大应力范围为70至220兆帕的状态下进行了表征。使用基于最大似然估计(MLE)的随机疲劳极限(RFL)模型来量化统计变异性并估计S-N曲线拟合。疲劳响应表明,最大标距直径(5.0毫米)导致最低疲劳强度,为89.5±5.6兆帕,最小直径(1.5毫米)导致最高疲劳强度,为122.0±32.8兆帕。直径为2.5毫米的试样表现出的疲劳强度为98.7±7.0兆帕。所有原始状态试样的主要失效机制是在原始表面光洁度的缝隙处引发表面裂纹。另外,对名义直径为5.0毫米的试样进行了疲劳试验,通过低应力表面磨削去除了原始表面。当去除75微米表面时,这些样品的疲劳强度增加到170兆帕,当完全去除表面轮廓时,疲劳强度增加到179兆帕。通过X射线衍射(XRD)表征了残余应力,结果表明轴向残余应力随着标距直径的减小而降低。另外的试样在进行应力消除退火后进行了疲劳试验,残余应力降低了51%,疲劳强度提高了30%。对微观结构、表面粗糙度、缺陷和断口表面的深入分析表明,表面状况和残余应力都是影响观察到的直径对高周疲劳影响的主要因素。