• 文献检索
  • 文档翻译
  • 深度研究
  • 学术资讯
  • Suppr Zotero 插件Zotero 插件
  • 邀请有礼
  • 套餐&价格
  • 历史记录
应用&插件
Suppr Zotero 插件Zotero 插件浏览器插件Mac 客户端Windows 客户端微信小程序
定价
高级版会员购买积分包购买API积分包
服务
文献检索文档翻译深度研究API 文档MCP 服务
关于我们
关于 Suppr公司介绍联系我们用户协议隐私条款
关注我们

Suppr 超能文献

核心技术专利:CN118964589B侵权必究
粤ICP备2023148730 号-1Suppr @ 2026

文献检索

告别复杂PubMed语法,用中文像聊天一样搜索,搜遍4000万医学文献。AI智能推荐,让科研检索更轻松。

立即免费搜索

文件翻译

保留排版,准确专业,支持PDF/Word/PPT等文件格式,支持 12+语言互译。

免费翻译文档

深度研究

AI帮你快速写综述,25分钟生成高质量综述,智能提取关键信息,辅助科研写作。

立即免费体验

揭示激光冲击强化诱导6061-T6铝合金残余应力分布特征

Unraveling Residual Stress Distribution Characteristics of 6061-T6 Aluminum Alloy Induced by Laser Shock Peening.

作者信息

Wang Qian, Ge Yaqiong, Chen Jingjia, Suzuki Tosei, Sagisaka Yoshihiro, Ma Ninshu

机构信息

Joining and Welding Research Institute, Osaka University, Osaka 567-0047, Japan.

College of Materials Science and Engineering, Taiyuan University of Science and Technology, 66 Waliu Road, Taiyuan 030024, China.

出版信息

Materials (Basel). 2024 Jul 14;17(14):3484. doi: 10.3390/ma17143484.

DOI:10.3390/ma17143484
PMID:39063776
原文链接:https://pmc.ncbi.nlm.nih.gov/articles/PMC11277776/
Abstract

Laser shock peening (LSP) is a powerful technique for improving the fatigue performance of metallic components by customizing compressive residual stresses in the desired near-surface regions. In this study, the residual stress distribution characteristics of 6061-T6 aluminum alloy induced by LSP were identified by the X-ray diffraction method, and their dependent factors (i.e., LSP coverage, LSP energy, and scanning path) were evaluated quantitatively by numerical simulations, exploring the formation mechanism of LSP residual stresses and the key role factor of the distribution characteristics. The results show that LSP is capable of creating anisotropic compressive residual stresses on the specimen surface without visible deformation. Compressive residual stresses are positively correlated with LSP coverage. The greater the coverage, the higher the residual stress, but the longer the scanning time required. Raising LSP energy contributes to compressive residual stresses, but excessive energy may lead to a reduction in the surface compressive residual stress. More importantly, the anisotropy of residual stresses was thoroughly explored, identifying the scanning path as the key to causing the anisotropy. The present work provides scientific guidance for efficiently tailoring LSP-induced compressive residual stresses to improve component fatigue life.

摘要

激光冲击喷丸(LSP)是一种通过在所需近表面区域定制压缩残余应力来提高金属部件疲劳性能的强大技术。在本研究中,采用X射线衍射法确定了LSP诱导的6061-T6铝合金残余应力分布特征,并通过数值模拟定量评估了其相关因素(即LSP覆盖率、LSP能量和扫描路径),探索了LSP残余应力的形成机制及分布特征的关键作用因素。结果表明,LSP能够在试样表面产生各向异性的压缩残余应力,且无可见变形。压缩残余应力与LSP覆盖率呈正相关。覆盖率越大,残余应力越高,但所需扫描时间越长。提高LSP能量有助于产生压缩残余应力,但能量过高可能导致表面压缩残余应力降低。更重要的是,深入研究了残余应力的各向异性,确定扫描路径是导致各向异性的关键因素。本研究为有效定制LSP诱导的压缩残余应力以提高部件疲劳寿命提供了科学指导。

https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/6be95427049b/materials-17-03484-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/d71e9173da51/materials-17-03484-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/77b2edd2e728/materials-17-03484-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/1cfb826c7ad5/materials-17-03484-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/10ee4bbd43b1/materials-17-03484-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/565a15fe6dd3/materials-17-03484-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/43c7280ec2b3/materials-17-03484-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/479e23aaebba/materials-17-03484-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/7a3afc8058f9/materials-17-03484-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/67ea14153022/materials-17-03484-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/13064f9fa43a/materials-17-03484-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/6be95427049b/materials-17-03484-g011.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/d71e9173da51/materials-17-03484-g001.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/77b2edd2e728/materials-17-03484-g002.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/1cfb826c7ad5/materials-17-03484-g003.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/10ee4bbd43b1/materials-17-03484-g004.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/565a15fe6dd3/materials-17-03484-g005.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/43c7280ec2b3/materials-17-03484-g006.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/479e23aaebba/materials-17-03484-g007.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/7a3afc8058f9/materials-17-03484-g008.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/67ea14153022/materials-17-03484-g009.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/13064f9fa43a/materials-17-03484-g010.jpg
https://cdn.ncbi.nlm.nih.gov/pmc/blobs/d3be/11277776/6be95427049b/materials-17-03484-g011.jpg

相似文献

1
Unraveling Residual Stress Distribution Characteristics of 6061-T6 Aluminum Alloy Induced by Laser Shock Peening.揭示激光冲击强化诱导6061-T6铝合金残余应力分布特征
Materials (Basel). 2024 Jul 14;17(14):3484. doi: 10.3390/ma17143484.
2
Surface Conditions after LASER Shock Peening of Steel and Aluminum Alloys Using Ultrafast Laser Pulses.使用超快激光脉冲对钢和铝合金进行激光冲击喷丸后的表面状况。
Materials (Basel). 2023 Oct 19;16(20):6769. doi: 10.3390/ma16206769.
3
Effect of Residual Stress on S-N Curves and Fracture Morphology of Ti6Al4V Titanium Alloy after Laser Shock Peening without Protective Coating.无防护涂层激光冲击强化后残余应力对Ti6Al4V钛合金S-N曲线及断口形貌的影响
Materials (Basel). 2019 Nov 19;12(22):3799. doi: 10.3390/ma12223799.
4
Numerical Prediction of the Effect of Laser Shock Peening on Residual Stress and Fatigue Life of Ti-6Al-4V Titanium Alloy.激光冲击强化对Ti-6Al-4V钛合金残余应力和疲劳寿命影响的数值预测
Materials (Basel). 2022 Aug 10;15(16):5503. doi: 10.3390/ma15165503.
5
Numerical Study on Laser Shock Peening of Pure Al Correlating with Laser Shock Wave.纯铝激光冲击强化与激光冲击波相关性的数值研究
Materials (Basel). 2022 Oct 11;15(20):7051. doi: 10.3390/ma15207051.
6
Confinement and absorption layer free nanosecond laser shock peening of tungsten and its alloy.钨及其合金的无约束和吸收层纳秒激光冲击强化
Opt Lett. 2022 Sep 15;47(18):4736-4739. doi: 10.1364/OL.472800.
7
Improvement in Fatigue Performance of Aluminium Alloy Welded Joints by Laser Shock Peening in a Dynamic Strain Aging Temperature Regime.在动态应变时效温度范围内通过激光冲击强化提高铝合金焊接接头的疲劳性能
Materials (Basel). 2016 Sep 26;9(10):799. doi: 10.3390/ma9100799.
8
Laser Peening Process and Its Impact on Materials Properties in Comparison with Shot Peening and Ultrasonic Impact Peening.激光喷丸工艺及其与喷丸和超声冲击喷丸相比对材料性能的影响。
Materials (Basel). 2014 Dec 10;7(12):7925-7974. doi: 10.3390/ma7127925.
9
Laser Shock Peening of SiCp/2009Al Composites: Microstructural Evolution, Residual Stress and Fatigue Behavior.SiCp/2009Al复合材料的激光冲击强化:微观结构演变、残余应力与疲劳行为
Materials (Basel). 2021 Feb 26;14(5):1082. doi: 10.3390/ma14051082.
10
A parametric neutron Bragg edge imaging study of additively manufactured samples treated by laser shock peening.激光冲击强化处理的增材制造样品的参数化中子布拉格边缘成像研究。
Sci Rep. 2021 Jul 21;11(1):14919. doi: 10.1038/s41598-021-94455-3.

本文引用的文献

1
Peen treatment on a titanium implant: effect of roughness, osteoblast cell functions, and bonding with bone cement.钛植入物上的喷丸处理:粗糙度、成骨细胞功能及与骨水泥结合的影响
Int J Nanomedicine. 2016 Feb 4;11:585-94. doi: 10.2147/IJN.S89376. eCollection 2016.