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PRACTICAL CRITERION FOR ESTIMATION OF NOTCH FATIGUE STRENGTH

机译:缺口疲劳强度估算的实用准则

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In the present study, a practical criterion for the estimation of the fatigue strength of notched specimens is discussed from a practical standpoint of design and maintenance of machines and structures. First of all, a hypothesis of "Fatigue Plastic Adaptation" is proposed as one idea that is available to combine microscopic and macroscopic approaches to fatigue plasticity. The hypothesis expresses that, at a surface layer and at a notch root, elastic deformation arising at the cyclic maximum stress is transformed into local and inhomogeneous plastic deformation. Based on the hypothesis, mechanical models are constructed in order to simulate cyclic stress behavior at the surface layer and at the notch root. As a result, "Equivalent Stress Ratio" is formulated as a parameter for correspondence of cyclic stress conditions between notched and unnotched specimens. Moreover, on the basis of the hypothesis of the plastic adaptation, the equation of the equivalent stress ratio is also derived for the case of biaxial stress cycling in torsion, and it is finally expanded for the general case of proportional multiaxial stress cycling. The published fatigue data concerning tension-compression, bending, torsion and their combined loading are rearranged on the diagram where an abscissa indicates the equivalent stress ratio and an ordinate indicates the stress range at the notch root. As the result, it is recognized that the relation between the equivalent stress ratio and the notch-root-concentrated stress range is shown by a certain curve proper to material in spite of difference of stress concentration factors, loading types and mean stresses. Consequently, a criterion for notch fatigue strength is described on the basis of the equivalent stress ratio, i.e., the notch-root-concentrated stress range at the fatigue strength of the notched specimen for any nominal stress ratio is identical with the fatigue strength of the unnotched specimen for the equivalent stress ratio.
机译:在本研究中,从机械和结构的设计和维护的实际观点出发,讨论了用于评估缺口试样的疲劳强度的实用标准。首先,提出了“疲劳塑性适应”的假设,作为可以将微观和宏观方法相结合来实现疲劳可塑性的一种想法。该假设表示,在表面层和凹口根部,在循环最大应力下产生的弹性变形被转化为局部塑性变形和非均匀塑性变形。基于该假设,构造机械模型以模拟表面层和缺口根部的循环应力行为。结果,将“当量应力比”公式化为带缺口和无缺口试样之间的循环应力条件的对应参数。此外,在塑性适应性假设的基础上,还得出了扭转时双轴应力循环情况下的等效应力比方程,最后针对比例多轴应力循环的一般情况进行了扩展。在图表上重新排列了已发布的有关拉伸,压缩,弯曲,扭转及其组合载荷的疲劳数据,其中横坐标表示等效应力比,纵坐标表示切口根部的应力范围。结果,认识到,尽管应力集中系数,载荷类型和平均应力不同,但是由适合于材料的某条曲线示出了当量应力比与缺口根集中应力范围之间的关系。因此,基于等效应力比描述了缺口疲劳强度的标准,即,对于任何标称应力比,缺口试样疲劳强度下的缺口根集中应力范围与试样的疲劳强度相同。无缺口试样的等效应力比。

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