期刊文献+

基于凝聚介质模型的矩形均匀激光诱导冲击强化研究

The Research on Rectangular Uniform Laser Induced Shock Strengthening Based on Condensed Medium Model
原文传递
导出
摘要 基于凝聚介质模型分析了均匀矩形激光脉冲诱导冲击压强峰值,以及其在金属材料中产生的残余压应力分布。利用稠密气体状态方程和冲击波基本关系式推导得到矩形均匀激光冲击产生的塑性影响深度L_(p)与激光峰值光强I_(p)的2/3次方存在正比关系。对LY2铝合金材料进行矩形均匀激光冲击强化并测试其残余应力深度及振动疲劳寿命,残余应力深度超过1.2 mm,与未处理试件相比较,振动疲劳寿命平均提升了4.5倍。利用矩形均匀激光冲击强化可有效预防金属材料的振动疲劳失效,提高金属材料的振动疲劳寿命,延长金属材料的服役时间。 The shock pressure induced by rectangular uniform laser pulse and the distribution of residual compressive stresses in metal materials were analyzed based on the condensed matter model.The plastic influence depth L_(p) produced by rectangular uniform laser shock was derived from the basic shock wave relations and the stiffened gas equation of state,which was related to the two-thirds power of laser peak intensity I_(p).The LY2 aluminum alloy was shocked by rectangular uniform laser pulse and the residual stress and vibration fatigue life were measured.The residual stress depth was more than 1.2 mm.Compared with the untreated specimens,the average vibration fatigue life was increased by 4.5 times.Therefore,using the rectangular uniform laser peening technique can effectively prevent the vibration fatigue failure of metal materials,improve the vibration fatigue life,and prolong the service time of metal materials.
作者 邵莉 艾军军 沈重阳 段嘉诚 邓晓旭 Shao Li;Ai Junjun;Shen Chongyang;Duan Jiacheng;Deng Xiaoxu(AECC Xi'an Aero-Engine Ltd.,Xi'an,Shaanci 710021,China;School of Physics and Astronomy,Shanghai Jiao Tong University,Shanghai 200240,China)
出处 《应用激光》 CSCD 北大核心 2022年第8期95-100,共6页 Applied Laser
基金 国家自然科学基金(61927822)。
关键词 矩形均匀激光 激光冲击强化 凝聚介质模型 振动疲劳寿命 rectangular uniform laser laser shock peening condensed matter model vibration fatigue life
  • 相关文献

参考文献5

二级参考文献44

  • 1Lu, K,Lu, J.Surface Nanocrystallization (SNC) of Metallic Materials-Presentation of the Concept behind a New Approach[J].Journal of Materials Science & Technology,1999,15(3):193-197. 被引量:298
  • 2胡奈赛,徐可为,方刚.喷丸件的残余应力松弛与位错亚结构变化[J].中国表面工程,1992,9(1):24-28. 被引量:4
  • 3YANG J M, HER Y .C,HAN N,et al. Laser Shock Peening on Fatigue Behavior of 2024-T3 AI Alloy with Fastener Holes and Stopholes [J]. Materials Science and Engineering A, A298, 2001 (1) : 296-299.
  • 4ZHANG HONG, YU CHENGYE. Laser shock processing of Holes[J]. Surface Engineering, 22 (2) : 153-156.
  • 5OMAR HATAMLEH, JED LYONS, ROYCE FORMAN. Laser and shot peening effects on fatigue crack growth in friction stirwelded 7075-T7351 aluminum alloy joints [J]. International Journal of Fatigue, 2007 (29) : 421-434.
  • 6Pereira J M, Lerch B A. Effects of heat treatment on the ballistic impact properties of Inconel718 for jet engine fan containment applications[J]. International Journal of Impact Engineering, 2001, 25: 715-733.
  • 7Loria E A. The status and prospects of alloy 718[J]. Journal of Metals, 1988, 40(7): 35-41.
  • 8Altenberger I, Stach E A, Liu G, et al. An in situ transmission electron microscope study of the thermal stability of near-surface microstructures induced by deep rolling and laser-shock peening[J]. Scripta Materialia, 2003, 48(12): 1593-1598.
  • 9Liao Y L, Ye C, Kim B J, et al. Nucleation of highly dense nanoscale precipitates based on warm laser shock peening[J]. Journal of Applied Physics, 2010, 108(6): 063518.
  • 10Ye C, Suslov S, Kim B J, et al. Fatigue performance improvement in AISI 4140 steel by dynamic strain aging and dynamic precipitation during warm laser shock peening[J]. Acta Materialia, 2011, 59(3): 1014-1025.

共引文献46

相关作者

内容加载中请稍等...

相关机构

内容加载中请稍等...

相关主题

内容加载中请稍等...

浏览历史

内容加载中请稍等...
;
使用帮助 返回顶部