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Branch crack behaviour in bearing steel under rolling contact fatigue

机译:滚动接触疲劳下轴承钢的分支裂纹行为

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摘要

In rolling contact fatigue, cracks grow by tensile (Mode I) or shear modes (Mode II and III) under the material surface due to the complicated tri-axial stress state. Flaking type failure, such as bearings and rails, is essentially due to the crack growth behaviour of these cracks. In order to evaluate the fatigue strength under rolling contact loading, it is important to understand the characteristics of such cracks under complicated stress state.The aim of this thesis was to study mixed mode behaviour of fatigue cracks, under cyclic shear stress and static compressive stress. Both experimental and numerical methods are applied. Experimental work consisted of the fatigue testing of bearing steel (SAE52100) under compressive mean stress. The test results show that resistance to mode I crack propagation increases with increasing compressive mean stress. In addition, non-propagating cracks, which are hardly observed at stress ratio R of -1 in high strength steel, were observed at R = -5 and -10. In the numerical investigations, stress intensity factor of complicated branch cracks in a plate (2D) under combined cyclic shear stress and static compressive stress was determined by finite element method. This study reveal the interaction behavior between the mode I and II cracks. The experimental and simulation results showed that there is a competitive behaviour between the Mode I and Mode II crack growth. The role of the compressive mean stress is to suppress the Mode I crack propagation. The magnitude of the compressive mean stress required to suppress Mode I crack growth depends on the Mode II crack length and applied cyclic shear stress. It was also observed that mode I crack lengths, if long enough, may reduce the KII of the Mode II crack even by 63%. The observation of non-propagating cracks for high compressive mean stress is one of novel finding of this study. However, the physical reason for this is not yet know. This is left future work. Furthermore, the numerical investigations can be extended to study more detail the influence of crack surface friction on crack growth mechanics.
机译:在滚动接触疲劳中,由于复杂的三轴应力状态,在材料表面下,裂纹会通过拉伸(模式I)或剪切模式(模式II和III)增长。诸如轴承和导轨之类的剥落型故障基本上是由于这些裂纹的裂纹扩展行为所致。为了评估滚动接触载荷下的疲劳强度,重要的是要了解这种应力在复杂应力状态下的特性。本论文的目的是研究在周期性剪切应力和静态压应力下疲劳裂纹的混合模式行为。 。实验方法和数值方法均适用。实验工作包括在压缩平均应力下对轴承钢(SAE52100)进行疲劳测试。测试结果表明,随着压缩平均应力的增加,对I型裂纹扩展的抵抗力也随之增加。此外,在R = -5和-10时,在高强度钢的应力比R -1下几乎没有观察到非传播裂纹。在数值研究中,通过有限元方法确定了循环剪切应力和静压缩应力共同作用下板(2D)中复杂分支裂纹的应力强度因子。这项研究揭示了I型和II型裂纹之间的相互作用行为。实验和仿真结果表明,I型和II型裂纹扩展之间存在竞争行为。平均压缩应力的作用是抑制I型裂纹的扩展。抑制I型裂纹扩展所需的平均压缩应力的大小取决于II型裂纹的长度和所施加的循环剪切应力。还观察到,如果长度足够长,I型裂纹的长度可能会使II型裂纹的KII降低63%。对非传播裂纹进行高压缩平均应力的观察是这项研究的新发现之一。但是,尚不清楚其物理原因。这是未来的工作。此外,数值研究可以扩展到更详细地研究裂纹表面摩擦对裂纹扩展力学的影响。

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  • 作者

    Abass Adeyinka;

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  • 年度 2017
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