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Fatigue crack initiation from small defects under low stress ratios inSAE52100 bearing steel

机译:低应力比在低应力率下缺陷的疲劳裂纹引发INSAE52100轴承钢

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Axial-loading fatigue tests were carried out under low stress ratios, R = -∞ ~ —5.33, by use of a cylindrical specimen of SAE52100 bearing steel having drill holes of 50~ 200 μm in diameter. The maximum stresses, σ_(max)= 0 ~300 MPa were combined with the minimum stresses, σ_(min) of —1600 or —1800 MPa. Even at σ_(max) = 0, fatigue cracks were initiated at hole edges by cyclic compressive stress of σ_(min) = —1800 MPa, and the cracks finally became non-propagating. When σ_(max) was positive, fatigue cracks were initiated even at σ_(min) = —1600 MPa and they also became non-propagating. The length of non-propagating cracks increased with an increase in σ_(max)· Those phenomena were considered to be related to the tensile residual stress that was induced by the plastic deformation in the vicinity of hole edges. The relationship between the length of non-propagating crack and the residual stress field was investigated in terms of elastic-plastic finite element analysis.
机译:通过使用SAE52100轴承钢的圆柱形样品,在低应力比率下进行轴向加载疲劳试验,r =-∞〜5.33,通过钻孔直径为50〜200μm的钻孔。最大应力σ_(max)= 0〜300MPa与最小应力,σ_(min)为-1600或-1800MPa。甚至在Σ_(max)= 0时,通过σ_(min)= -1800mPa的循环压缩应力在孔边缘处引发疲劳裂缝,并且裂缝最终变得不繁殖。当σ_(max)是阳性时,即使在σ_(min)= -1600MPa下也会启动疲劳裂缝,并且它们也变得不繁殖。非传播裂缝的长度随着Σ_(最大)的增加而增加,认为这些现象与孔边缘附近的塑性变形引起的拉伸残余应力相关。在弹性塑料有限元分析方面研究了非传播裂缝长度与残余应力场之间的关系。

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