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Effect of Compound Layer Thickness Composed of gamma '-Fe4N on Rotated- Bending Fatigue Strength in Gas-Nitrided JIS-SCM435 Steel

机译:γ'-Fe4N组成复合层厚度对气 - 氮化JIS-SCM435钢旋转弯曲疲劳强度的影响

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摘要

The rotating bending fatigue strength of gas nitrided JIS-SCM435 steel was evaluated to find the thickness that gives the highest bending fatigue strength. Four specimens were used that had different compound layer thicknesses composed of gamma'(-Fe4N) phase: 0, 2, 10, and 20 mu m. The composition of. phase was more than 70% of the volume of the compound layer in the specimens. The increment of the fatigue strength at 105-107 cycles was remarkably high when the compound layer thickness was from 0 to 10 mu m and gradually increased from 10 to 20 mu m. The increment of the fatigue strength was caused by the increment of the. phase thickness and the compressive residual stress depth as the compound layer thickness increased. The gradually increasing fatigue strength of more than 10 mu m thickness was responsible for the porous layer thickness increasing and the compressive residual stress reducing on the surface as the compound layer thickness increased. These findings show that the fatigue strength of gas-nitrided JIS-SCM435 steel composed of. phase depends on not only the compound layer thickness but also the porous layer thickness and the compressive residual stress of the compound layer.
机译:评价气体氮化JIS-SCM435钢的旋转弯曲疲劳强度,以找到弯曲疲劳强度的厚度。使用具有不同的化合物层厚度的四个标本,由γ'( - Fe 4N)相:0,2,10和20μm组成。的组成。相超过试样中复合层的70%的70%。当化合物层厚度为0至10μm时,105-107循环在105-107个循环中的疲劳强度的增量显着高,并且从10至20μm逐渐增加。疲劳强度的增量是由递增的。随着化合物层厚度的增加,相厚度和压缩残余应力深度。逐渐增加的疲劳强度大于10μmm厚度是对多孔层厚度的负责,随着化合物层厚度的增加而减小表面上的压缩残余应力。这些调查结果表明,气体氮化JIS-SCM435钢的疲劳强度组成。相位不仅取决于化合物层厚度,还取决于复合层的多孔层厚度和压缩残余应力。

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