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Improvement in fatigue properties of 2024-T351 aluminum alloy subjected to cryogenic treatment and laser peening

机译:改善2024-T351铝合金经受低温处理和激光喷丸的疲劳性能

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摘要

The aim of this study was to investigate the effects of Cryogenic Treatment (CT) and Laser Peening (LP) on the fatigue properties of 2024-T351 aluminum alloy. The measurements of tensile properties and microhardness were carried out, and the residual stress tests were also conducted through x-ray diffraction (XRD) technology. Examination of microstructure was executed by Scanning Electron Microscopy (SEM) and Transmission Electron Microscopy (TEM) observations. Fatigue tests were conducted and the fatigue fracture morphologies were also analyzed by SEM. Experimental results found that both CT and LP could enhance the fatigue properties of 2024-T351 aluminum alloy. The process of CT prior to LP could provide a higher fatigue life compared with single CT or LP process. After CT prior to LP, the fatigue life of the treated specimen was 28,077 cycles under gradient loading, which obtained an increase of 4640 cycles compared to the untreated specimen. Meanwhile, compared with single CT and LP, CT prior to LP could produce finer grains, more precipitated second phases, higher density dislocation and compressive residual stresses. Beneficial microstructure evolution and compressive residual stress induced by CT prior to LP were considered to be the main factors that contribute to the improvement of the fatigue properties.
机译:本研究的目的是调查深冷处理(CT)和激光喷丸(LP)对2024-T351铝合金的疲劳特性的效果。拉伸性能和显微硬度的测量结果进行的,并且残余应力试验也通过X射线衍射(XRD)技术进行的。显微组织的检查,通过扫描电子显微镜(SEM)和透射电子显微镜(TEM)观察来执行。疲劳试验中进行,并且还通过SEM分析出的疲劳断裂形态。实验结果发现,CT和LP两个可增强2024-T351的铝合金的疲劳特性。 CT之前LP的方法可以用单一的CT或LP工艺相比提供了更高的疲劳寿命。 CT后之前LP,经处理的试样的疲劳寿命是根据梯度载荷,它得到比未处理样品的增加的4640个循环28077次循环。同时,随着单个CT和LP相比,CT之前LP能产生更细的晶粒,更析出第二相,较高密度的位错和压缩残余应力。有益组织演变和之前LP诱导CT压缩残余应力被认为是有助于疲劳特性的提高的主要因素。

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