Effect of size and depth of small defect on the rolling contact fatigue strength of a bearing steel SUJ2

H. Komata, J. Yamabe, H. Matsunaga, Y. Fukushima, S. Matsuoka
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引用次数: 12

Abstract

Rolling contact fatigue tests of JIS-SUJ2 steel were performed using plate specimens having a small drill hole with various diameters and depths. In all the tests, fatigue crack initiated at the edge near the bottom of the hole just after starting the fatigue test, and then propagated by shear mode. Even in the unbroken specimens tested up to N = 2×10 cycles, a short fatigue crack was found at the edge. Fatigue life, Nf, plotted against the maximum contact pressure, qmax, was greatly varied according to the diameter and depth of the hole. The effect of the depth at crack initiation on the fatigue life Nf was uniquely characterized by using the nominal shear stress amplitude, τa, instead of qmax. Further, based on the consideration of the rolling contact fatigue strength as a small shear-mode crack problem, the fatigue life data were plotted using the novel parameter, τ a/( area ), where the area is a projected area of the hole. Consequently, all the fatigue life data were successfully fitted on a unified line irrespective of the diameter and depth of the hole, i.e. a defect size dependence in the rolling contact fatigue strength was manifested in a small crack regime. Moreover, the fatigue life data for smooth specimens fractured from an internal non-metallic inclusion were also in accordance with the data for the drill holes in the plot of Nf versus τ a/( area ). The result infers that a lower limit of the rolling contact fatigue strength of bearings with various dimensions can be evaluated by means of the following two dominant parameters: (i) maximum inclusion size predicted by the statistics of extremes in a given control volume and (ii) the maximum value of nominal shear stress amplitude produced under the rolling contact.
小缺陷尺寸和深度对轴承钢SUJ2滚动接触疲劳强度的影响
采用带不同直径和深度的小孔板试样对JIS-SUJ2钢进行了滚动接触疲劳试验。在所有试验中,疲劳裂纹都是在刚开始疲劳试验时,在靠近孔底的边缘处产生,然后以剪切方式扩展。即使在N = 2×10循环试验中,在边缘处也发现了短的疲劳裂纹。疲劳寿命Nf(由最大接触压力qmax绘制)随着孔的直径和深度的不同而变化很大。用名义剪应力幅值τa代替qmax来表征裂纹起裂深度对疲劳寿命Nf的影响。此外,基于将滚动接触疲劳强度考虑为小剪切型裂纹问题,使用新参数τ a/(面积)绘制疲劳寿命数据,其中面积为孔的投影面积。因此,所有的疲劳寿命数据都成功地拟合在一条统一的线上,而不考虑孔的直径和深度,即在小裂纹区表现出滚动接触疲劳强度的缺陷尺寸依赖性。此外,内部含有非金属夹杂的光滑试样的疲劳寿命数据也与Nf - τ a/(面积)图中钻孔的数据一致。结果表明,不同尺寸轴承的滚动接触疲劳强度下限可以通过以下两个主要参数来评估:(i)在给定控制体积中由极值统计预测的最大夹杂物尺寸和(ii)滚动接触下产生的名义剪切应力幅值的最大值。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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