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Residual Stress Creep Relaxation Around Cold Expanded Holes in an Aluminum Alloy

机译:铝合金冷扩孔周围的残余应力蠕变松弛

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Residual stress distributions were measured in aluminum-alloy 2650 disks after cold expansion and after exposure to creep at 150℃ for various times. Strains measured as a result of boring out the hole after cold expansion were found to exhibit significant angular variations around the hole. However, after exposure to 150℃ residual strains and stresses showed less angular variation. To take account of the angular variation, the Garcia—Sachs technique for measuring residual stresses was employed. Surface residual stresses on the entrance and exit faces of the disks were measured using the x-ray method. The most significant relaxation of the residual stresses occurred within the first 100 h. Two simple models were used to predict residual stress relaxation, one using a uniaxial creep relaxation model and a second using tensile and isochronous stress-strain curves. A good comparison between predictions and experiments was observed.
机译:在铝合金2650盘上冷膨胀后和暴露于150℃蠕变不同时间后,测量残余应力分布。发现由于在冷膨胀后钻出孔而测得的应变在孔周围显示出明显的角度变化。然而,暴露于150℃后,残余应变和应力的角度变化较小。考虑到角度变化,采用了Garcia-Sachs技术来测量残余应力。使用X射线方法测量磁盘入口和出口表面的表面残余应力。残余应力最明显的松弛发生在前100小时内。使用两个简单模型来预测残余应力松弛,一个模型使用单轴蠕变松弛模型,第二个模型使用张应力和等时应力-应变曲线。观察到的预测和实验之间进行了很好的比较。

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