Influence Rule of Process Parameters on Residual Stress Cave Induced by Laser Shock
摘 要
通过建立残余应力洞数学模型,引入残余应力洞的相对洞深、相对洞宽及应力损失比等概念,采用经过试验验证的有限元模型来定量分析激光冲击能量(1.0~3.0 J)、光斑直径(1.0~3.0 mm)、冲击次数(1~5次)、光斑搭接率(30%~70%)等工艺参数对残余应力洞的影响。结果表明:在研究的工艺参数范围内,由残余应力洞所造成的应力损失比都很小,都小于3%,相对洞宽均小于20%,而相对洞深的变化范围较大,为0~70%,相对洞深是影响表面残余应力分布均匀性的主要因素;为改善表面残余应力分布的均匀性,当单个残余应力洞的相对洞深超过10%时,应采用光斑搭接方式进行冲击强化,且相邻光斑中心的距离应等于残余应力洞的洞口半径。
Abstract
The concepts of relative cave depth, relative cave width and stress loss ratio of residual stress cave were introduced by establishment of the residual stress cave math model. The effect of shock energy (1.0-3.0 J), spot diameter (1.0-3.0 mm), shock number (1-5 times) and spot overlap ratio (30%-70%) on residual stress cave was quantitatively analyzed by finite element model verified by experiment. The results show that stress loss ratios caused by residual stress cave were all very small, which were all less than 3%; relative cave widths were all less than 20%; the variation range of relative cave depths was large, which was 0-70%, and relative cave depth was the main factor to affect the uniformity of surface residual stress. In order to improve the uniformity of surface residual stress, when the relative cave depth of single residual stress cave was more than 10%, the spot overlap method should be used to shock peening, and the distance between two neighbouring spot center should be equal to the opening radius of the residual stress cave.
中图分类号 TG178 DOI 10.11973/jxgccl201911012
所属栏目 物理模拟与数值模拟
基金项目 国家自然科学基金资助项目(51575117)
收稿日期 2019/6/22
修改稿日期 2019/10/18
网络出版日期
作者单位点击查看
联系人作者夏琴香教授
备注程秀全(1964-),男,安徽滁州人,教授,硕士
引用该论文: CHENG Xiuquan,YAN Chang,CHENG Sizhu,XIA Qinxiang. Influence Rule of Process Parameters on Residual Stress Cave Induced by Laser Shock[J]. Materials for mechancial engineering, 2019, 43(11): 53~56
程秀全,晏畅,程思竹,夏琴香. 工艺参数对激光冲击诱导表面残余应力洞的影响规律[J]. 机械工程材料, 2019, 43(11): 53~56
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参考文献
【1】PEYRE P, FABBRO R, MERRIEN P, et al. Laser shock processing of aluminium alloys. Application to high cycle fatigue behavior[J]. Material Science and Engineering A:1996, 210:102-113.
【2】ACHINTHA M, NOWELL D, FUFARI D, et al. Fatigue behaviour of geometric features subjected to laser shock peening:Experiments and modelling[J]. International Journal of Fatigue, 2014, 62:171-179.
【3】马壮,李应红,任旭东,等. 航空铝合金激光激波强化工艺[J]. 机械工程材料, 2007,31(8):32-34.
【4】TRDAN U, SKARBA M, GRUMA J. Laser shock peening effect on the dislocation transitions and grain refinement of Al-Mg-Si alloy[J]. Materials Characterization, 2014,97:57-68.
【5】BHAMARE S, RAMAKRISHNAN G, MANNAVA S R, et al. Simulation-based optimization of laser shock peening process for improved bending fatigue life of Ti-6Al-2Sn-4Zr-2Mo alloy[J]. Surface & Coatings Technology, 2013, 232:464-474.
【6】贾凯翔, 张传伟, 聂祥樊. 激光冲击"残余应力洞"的参数影响[J]. 火力与指挥控制, 2014, 39(8):1384-1388.
【7】王学德,周鑫,王路成,等. GH742合金激光冲击强化后的表面残余应力[J]. 机械工程材料, 2012, 36(3):79-80.
【8】姜银方, 来彦玲,张磊,等. 激光冲击材料表面"残余应力洞"形成规律与分析[J]. 中国激光,2010,37(8):2073-2079.
【9】王波, 陈东林, 周留成, 等. 激光冲击波加载金属材料中心压应力缺失效应[J].红外与激光工程,2014,43(11):3521-3526.
【10】王学德,聂祥樊,臧顺来,等. 激光冲击强化"残余应力洞"的形成机制[J]. 强激光与粒子束,2014,26(11):119003.
【11】FABBRO R, PEYRE P, BERTHE L, et al. Physics and application of laser shock processing[J]. Laser Application, 1998, 10(6):265-279.
【12】FAIRAND B P,CLAUER A H.Laser generated of high-amplitude stress waves in materials[J]. Journal of Applied Physics, 1978,50(3):265-279.
【13】程龙. 不同激光冲击工艺参数对40Cr钢表面应力应变影响的模拟试验研究[D].镇江:江苏大学, 2017.
【14】樊玉杰. 激光微喷丸强化的压力模型及冲击效应研究[D]. 镇江:江苏大学, 2011.
【15】花国然,蒋苏州,曹宇鹏,等.激光冲击7050铝合金表面"残余应力洞"的模拟[J].金属热处理, 2017, 42(7):154-157.
【16】陈浩天,曹宇鹏,花国然,等.激光冲击690高强钢表面残余应力工艺优化模拟[J]. 金属热处理,2018, 43(10):206-209.
【17】张兴权,张永康,顾永玉,等.激光喷丸诱导的残余应力的有限元分析[J].塑性工程学报, 2008(4):188-193.
【18】帅高鹏.基于在线修复的飞机受损件激光喷丸残余应力研究[D].广州:华南理工大学, 2017.
【19】彭薇薇, 凌祥. 激光冲击残余应力场的有限元分析[J]. 航空材料学报,2006(6): 30-37.
【20】刘贵杰,杨胜瑞.激光冲击诱导的残余应力洞数值建模仿真分析[J].材料热处理学报, 2015,36(10):241-247.
【21】李兴成,张永康,周金宇,等.激光冲击强化AZ31镁合金表面残余应力分析[J].激光技术, 2016, 40(1):5-10.
【22】余天宇,戴峰泽,张永康,等.平顶光束激光冲击2024铝合金诱导残余应力场的模拟与实验[J].中国激光,2012,39(10):1993991.
【23】段志勇.激光冲击波及激光冲击处理技术的研究[D].合肥:中国科学技术大学,2000.
【2】ACHINTHA M, NOWELL D, FUFARI D, et al. Fatigue behaviour of geometric features subjected to laser shock peening:Experiments and modelling[J]. International Journal of Fatigue, 2014, 62:171-179.
【3】马壮,李应红,任旭东,等. 航空铝合金激光激波强化工艺[J]. 机械工程材料, 2007,31(8):32-34.
【4】TRDAN U, SKARBA M, GRUMA J. Laser shock peening effect on the dislocation transitions and grain refinement of Al-Mg-Si alloy[J]. Materials Characterization, 2014,97:57-68.
【5】BHAMARE S, RAMAKRISHNAN G, MANNAVA S R, et al. Simulation-based optimization of laser shock peening process for improved bending fatigue life of Ti-6Al-2Sn-4Zr-2Mo alloy[J]. Surface & Coatings Technology, 2013, 232:464-474.
【6】贾凯翔, 张传伟, 聂祥樊. 激光冲击"残余应力洞"的参数影响[J]. 火力与指挥控制, 2014, 39(8):1384-1388.
【7】王学德,周鑫,王路成,等. GH742合金激光冲击强化后的表面残余应力[J]. 机械工程材料, 2012, 36(3):79-80.
【8】姜银方, 来彦玲,张磊,等. 激光冲击材料表面"残余应力洞"形成规律与分析[J]. 中国激光,2010,37(8):2073-2079.
【9】王波, 陈东林, 周留成, 等. 激光冲击波加载金属材料中心压应力缺失效应[J].红外与激光工程,2014,43(11):3521-3526.
【10】王学德,聂祥樊,臧顺来,等. 激光冲击强化"残余应力洞"的形成机制[J]. 强激光与粒子束,2014,26(11):119003.
【11】FABBRO R, PEYRE P, BERTHE L, et al. Physics and application of laser shock processing[J]. Laser Application, 1998, 10(6):265-279.
【12】FAIRAND B P,CLAUER A H.Laser generated of high-amplitude stress waves in materials[J]. Journal of Applied Physics, 1978,50(3):265-279.
【13】程龙. 不同激光冲击工艺参数对40Cr钢表面应力应变影响的模拟试验研究[D].镇江:江苏大学, 2017.
【14】樊玉杰. 激光微喷丸强化的压力模型及冲击效应研究[D]. 镇江:江苏大学, 2011.
【15】花国然,蒋苏州,曹宇鹏,等.激光冲击7050铝合金表面"残余应力洞"的模拟[J].金属热处理, 2017, 42(7):154-157.
【16】陈浩天,曹宇鹏,花国然,等.激光冲击690高强钢表面残余应力工艺优化模拟[J]. 金属热处理,2018, 43(10):206-209.
【17】张兴权,张永康,顾永玉,等.激光喷丸诱导的残余应力的有限元分析[J].塑性工程学报, 2008(4):188-193.
【18】帅高鹏.基于在线修复的飞机受损件激光喷丸残余应力研究[D].广州:华南理工大学, 2017.
【19】彭薇薇, 凌祥. 激光冲击残余应力场的有限元分析[J]. 航空材料学报,2006(6): 30-37.
【20】刘贵杰,杨胜瑞.激光冲击诱导的残余应力洞数值建模仿真分析[J].材料热处理学报, 2015,36(10):241-247.
【21】李兴成,张永康,周金宇,等.激光冲击强化AZ31镁合金表面残余应力分析[J].激光技术, 2016, 40(1):5-10.
【22】余天宇,戴峰泽,张永康,等.平顶光束激光冲击2024铝合金诱导残余应力场的模拟与实验[J].中国激光,2012,39(10):1993991.
【23】段志勇.激光冲击波及激光冲击处理技术的研究[D].合肥:中国科学技术大学,2000.
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