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首页> 外文期刊>Fatigue of Aircraft Structures >Deterministic Approach to Predicting the Fatigue Crack Growth in the 2024-T3 Aluminum Alloy Under Variable Amplitude Loading
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Deterministic Approach to Predicting the Fatigue Crack Growth in the 2024-T3 Aluminum Alloy Under Variable Amplitude Loading

机译:2024-T3铝合金在变幅载荷下疲劳裂纹扩展的确定性预测方法

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摘要

The paper presents the attempt to predict fatigue crack growth rate in a component subjected to variable amplitude loading containing overload-underload cycles. For this goal in a deterministic approach the modified Willenborg retardation model was applied. To provide experimental data the research into fatigue crack growth for 2024-T3 aluminum alloy sheet CCT specimens under LHL type block program loading with multiple overload-underload cycles was developed. The microfractographic analysis of fatigue fractures with the use of the transmission electron microscope (TEM) made it possible to trace the effect of block program loading on the crack growth rate. The knowledge of the affection of a particular overload-underload cycle or a block of these cycles on crack rate on the basis of microfractographic analysis was utilized for assessing the equivalent loading for the LHL block program. The diagrams that presented the crack growth rate both on the surface and inside the aluminum alloy sheet was performed. The crack growth rate inside the sheet was estimated on the basis of the striation spacing analysis.
机译:本文提出了一种尝试来预测部件在包含超载-欠载循环的可变振幅载荷下的疲劳裂纹扩展速率。为此,在确定性方法中应用了改进的Willenborg延迟模型。为提供实验数据,对2024-T3铝合金薄板CCT试样在LHL型块程序荷载下具有多个超载-欠载循环的疲劳裂纹扩展进行了研究。使用透射电子显微镜(TEM)对疲劳断裂进行显微分形分析,可以追踪程序块加载对裂纹扩展率的影响。利用特定的超载-欠载循环或这些循环中的一个对裂纹率的影响的知识(基于显微形貌分析),可用于评估LHL块程序的等效载荷。进行表示铝合金板的表面和内部的裂纹扩展率的图。基于条纹间距分析估计板内部的裂纹扩展速率。

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