中国激光, 2012, 39 (3): 0303010, 网络出版: 2012-02-20   

中高温条件下6061-T651铝合金激光冲击强化研究

Experimental Research of Laser Shock Processing 6061-T651 Aluminum Alloy during Elevated Temperature
作者单位
江苏大学机械工程学院, 江苏 镇江 212013
摘要
利用高功率、短脉冲NdYAG激光对6061-T651铝合金进行表面冲击强化处理,并分别在200 ℃、300 ℃、400 ℃和500 ℃的温度下对其进行性能测试,从残余应力、显微硬度和微观组织等方面分析了激光冲击处理(LSP)对其在高温条件下性能的影响。研究结果表明中高温条件下激光冲击6061-T651铝合金的强化效果明显。200 ℃和400 ℃时试件的最大残余压应力出现在次表层,且温度越高残余压应力释放得越快,激光冲击硬化层深度约为0.3 mm,500 ℃时的晶粒平均尺寸要比400 ℃时的大,晶粒尺寸和强化相是提高硬度的主要原因,不连续且粗大的晶界析出物提高了6061-T651铝合金的抗腐蚀性能。
Abstract
The 6061-T651 aluminum alloy samples are treated by laser shock processing (LSP) with high power and short pulse NdYAG laser, and then are kept warm at 200 ℃, 300 ℃, 400 ℃ and 500 ℃ respectively. The effects of 6061-T651 aluminum alloy on mechanical properties after LSP are analyzed from residual stress, micro-hardness and microstructure during elevated temperature. The results indicate that the strengthening effect of 6061-T651 aluminum alloy by LSP at elevated temperature is obvious. The maximum residual stress of specimens are tested in subsurface at 200 ℃ and 400 ℃. At the same time, the higher the temperature, the faster the residual stress releases. The hardening layer depth of 6061-T651 aluminum alloy is about 0.3 mm. The primary cause of improving micro-hardness is grain size and strengthening phase, and the pitting resistance of 6061-T651 aluminum alloy is improved obviously by the big and discontinuous precipitated phase.

任旭东, 阮亮, 皇甫喁卓, 占秋波, 杨慧敏, 张永康. 中高温条件下6061-T651铝合金激光冲击强化研究[J]. 中国激光, 2012, 39(3): 0303010. Ren Xudong, Ruan Liang, Huangfu Yongzhuo, Zhan Qiubo, Yang Huimin, Zhang Yongkang. Experimental Research of Laser Shock Processing 6061-T651 Aluminum Alloy during Elevated Temperature[J]. Chinese Journal of Lasers, 2012, 39(3): 0303010.

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