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Effect of local cold working on the fatigue life of 7475-T7351 aluminium alloy hole specimens

机译:局部冷加工对7475-T7351铝合金孔试样疲劳寿命的影响

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摘要

Different degrees of cold working (ranging from 0 percent to 5.58 percent) were applied to the hole of plate specimens of 7475-T7351 aluminium alloy. These specimens were then subjected to cyclic loading. In each test, the crack initiation was detected and subsequently the crack length was monitored, using a video camera system. The experimental results were analysed in order to determine the cold working effect on the fatigue initiation period, on the propagation life and finally on the overall fatigue life. It was found, for example, that the propagation life improvement factor for a degree of cold working of 5.58 percent is about 43.0 and 4.9 for applied nominal stresses of 191 and 300 MPa, respectively. For the same conditions, the fatigue life improvement factor is about 3.2 and 1.5. A numerical analysis was also performed, using three-dimensional finite element method to establish the stress and strain distributions resulting from the superposition of the cold working process and the fatigue loading. Then, the results were used in connection with the non-cold worked hole data for calculating the cold worked plate initiation period according to the strain-life concept; for determining the propagation life, the weight function technique was applied. The predictions are very close to the experimental results.
机译:对7475-T7351铝合金板的孔进行了不同程度的冷加工(范围从0%到5.58%)。然后对这些样品进行循环加载。在每个测试中,检测到裂纹的产生,然后使用摄像机系统监视裂纹的长度。分析实验结果,以确定冷加工对疲劳萌生期,传播寿命以及最终对整体疲劳寿命的影响。例如,发现对于191和300 MPa的额定公称应力,冷加工度为5.58%时,传播寿命的改善系数分别约为43.0和4.9。在相同条件下,疲劳寿命提高系数约为3.2和1.5。还使用三维有限元方法进行了数值分析,以建立由冷加工过程和疲劳载荷叠加产生的应力和应变分布。然后,将结果与非冷加工孔数据结合使用,根据应变寿命概念计算冷加工板的起始时间。为了确定传播寿命,应用了权重函数技术。这些预测与实验结果非常接近。

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