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Multiaxial Fatigue Analysis - Approach Toward Real-World Life Prediction

机译:多轴疲劳分析 - 实现现实世界生活预测的方法

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Conventional fatigue analysis procedures followed in daily practices are at least 10 or more years old. Typically, equivalent stress (on a plane) approach is used for fatigue analysis. However, variation of stresses/strains in a particular plane may not yield accurate results for fatigue life calculation. With new developments in analysis practices and better solver capabilities, it is imperative to evaluate these techniques for fatigue analysis followed today. One such need is to evaluate the fatigue life when loads are highly complex and nonproportional. Study is done here to perform multiaxial fatigue analysis of the structure. It is compared against the existing methods for applicability in terms of cost and solution time. n-code fatigue analysis module is used for the study based on multiaxiality. Multiaxial fatigue analysis requires use of yield criteria to fatigue under combined loading. With nonproportional loading, there is increased strain hardening which needs to be considered appropriately. Hence, based on nonproportionality and biaxiality, a decision matrix is prepared to decide the appropriate notch correction and equivalent stress or strain approach. Notch correction methods studied are Neuber, Hoffmann-Seeger, Glinka and Jiang Sehitoglu. Available n-code multiaxiality options are explored and comparative study among these approaches is summarized here. The n-code multiaxial fatigue analysis proposes two approaches to predict the fatigue life. Two-step analysis and multistep analysis give closer solution to fatigue life, but time required for solution increases drastically. Two-step analysis can be selected as a trade-off for life prediction with multiaxiality in terms of time taken for solution. Multiaxial fatigue analysis is performed on one of our vehicle structure to correlate the results with actual life of the components predicted from the rig test.
机译:在日常实践中遵循的传统疲劳分析程序至少为10岁或以上。通常,等效应力(在平面上)方法用于疲劳分析。然而,特定平面中的应力/菌株的变化可能不会产生疲劳寿命计算的准确结果。随着分析实践和更好的求解能力的新发展,必须评估今天随访的疲劳分析技术。一种这样的需要是在负载高度复杂和非备产时评估疲劳寿命。研究完成了对结构进行多轴疲劳分析。在成本和解决方案时间方面与现有方法进行比较。 N代码疲劳分析模块用于基于多轴性的研究。多轴疲劳分析需要在组合负载下使用屈服标准来疲劳。通过非储载,存在增加的应变硬化,需要适当地考虑。因此,基于非比例和双轴性,准备决策矩阵来确定适当的凹口校正和等效应力或应变方法。学习的陷波校正方法是Neuber,Hoffmann-Seeger,Glinka和Jiang Sehitoglu。可用的N代码多信息选项是探讨的,并在此概述了这些方法之间的比较研究。 N代码多轴疲劳分析提出了两种方法来预测疲劳寿命。两步分析和多步骤分析给出了疲劳寿命更接近的解决方案,但解决方案所需的时间急剧增加。在解决方案所采取的时间方面,可以选择两步分析作为多轴性预测的折衷。多轴疲劳分析在我们的一个车辆结构上进行,以将结果与钻机测试预测的部件的实际寿命相关联。

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