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作 者:张青来[1] 吴铁丹 钱阳[1] 王荣[1] 洪妍鑫 陈骏[1]
机构地区:[1]江苏大学材料科学与工程学院,江苏镇江212013
出 处:《中国激光》2014年第10期87-93,共7页Chinese Journal of Lasers
基 金:国家自然科学基金(51175231)
摘 要:为了研究激光冲击对AZ91D-T6铸造镁合金高周疲劳性能的影响,采用钕玻璃脉冲激光器(波长1064nm,脉冲宽度20ns),对中心缺口试样进行激光冲击强化(LSP)处理,并进行了拉-拉疲劳试验,分析了表面形貌、表面显微硬度、微观组织、疲劳断口特征和残余应力分布,结果表明:以1.5GW/cm2功率密度和光斑50%搭接的激光冲击强化后,中心缺口疲劳试样上下表面形成高残余压应力,显微硬度提高24%左右,晶粒明显细化,冲击试样循环周次比未冲击的提高33.7%,疲劳断口呈解理断裂特征,主要表现为大量解理台阶和河流花样,β-Mg17Al12相的存在改变了疲劳裂纹扩展路径。激光冲击延迟了裂纹萌生时间,提高了AZ91D-T6铸造镁合金的疲劳寿命。In order to study the effect of laser shock processing(LSP)on the high cycle fatigue properties of AZ91DT6 cast magnesium alloy,the test samples with center hole are shocked with Nd:glass laser with the wavelength of1064 nm and pulse width of 20 ns.Tensile-tensile fatigue test is also carried out on the samples.The surface morphology,surface micro-hardness,microstructures,fatigue fracture characteristics and residual stress are analyzed.The results show that after LSP with power density of 1.5 GW/cm^2 and spots of 50% overlap rate,high residual compressive stress is generated on the upper and lower surface of the fatigue samples.The micro-hardness of shocking area increases by about 24% and the grains are refined obviously.Fatigue life of the shocked samples is improved by 33.7%than that of the un-shocked samples.The Fatigue fractures show characteristics of the cleavage fracture,and the cleavage steps and river pattern are mainly observed.The crack propagation path is changed because of the existence of theβ-Mg17Al12 phase.The crack initiation time is delayed after LSP,which improves the fatigue life of AZ91D-T6 cast magnesium alloy.
关 键 词:材料 镁合金 激光冲击强化 疲劳性能 残余应力 微观组织
分 类 号:TN249[电子电信—物理电子学] TG146.22[一般工业技术—材料科学与工程]
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