期刊文献+

激光冲击强化优化TA15电子束焊接接头的组织性能(英文)

Microstructure and Properties of TA15 EBW Joints Optimized by Laser Shock Processing
原文传递
导出
摘要 采用激光冲击强化技术(LSP)对TA15钛合金电子束焊接(EBW)接头进行处理。对经过LSP处理的TA15钛合金接头,分别检测了接头的表面硬度、耐腐蚀性能、25℃室温与300℃拉伸力学性能及断口形貌。与未经LSP处理的EBW接头相比,经过LSP处理后的TA15 EBW接头表面的HV硬度得到了提高,耐腐蚀性能并没有明显降低,在25℃室温和高温300℃拉伸时,接头的拉伸性能均得到了显著提高。研究结果表明:LSP技术能够有效改善TA15钛合金EBW接头的组织性能。 Laser shock processing(LSP) was introduced to treat electron beam welding(EBW) joints of TA15 titanium alloy.After LSP treatment,surface hardness,corrosion resistance,tensile mechanical properties at 300 oC,and the fractures of joints were detected.The results show the properties of TA15 titanium alloy EBW joints treated by LSP have been improved.After LSP treatment,the bead surface HV hardness is increased.Compared with original weld beads,the corrosion resistance of these joints treated by LSP is not reduced.After LSP treatment,tensile properties of TA15 titanium alloy joints at 25 and 300 oC are improved observably.
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2013年第S2期151-154,共4页 Rare Metal Materials and Engineering
关键词 激光冲级强化 TA15钛合金 HV硬度 耐腐蚀性能 拉拉伸力学性能 laser shock processing TA15 titanium alloy HV hardness corrosion resistance tensile properties
  • 相关文献

参考文献4

二级参考文献18

  • 1乔梁.一种机动辐射源的单站无源定位跟踪滤波算法[J].上海航天,2008,25(1):33-35. 被引量:1
  • 2严超.目标跟踪下的Kalman算法与IMM算法性能比较[J].科技情报开发与经济,2007,17(15):229-231. 被引量:4
  • 3邵荣宽,隆小庆编.民用飞机的腐蚀与控制[M].海潮出版社,2000.2.
  • 4Boeing. Structure Repair for Airline Engineers.
  • 5Welch G, Bishop G. Department of computer scince university of north carolina at chapel hill chapel hill[R]. NC 27599-3175.
  • 6Hartikainen J, Sarkka S. Optimal filtering with kalman filters and smo-others a manual for matlab toolbox[J]. EKF UKF February, 2008, 3 (5) : 219-292.
  • 7Arrieta A.J.,Multidisciplinary Design Optimization of a Fighter Aircraft with Damage Tolerance Constraints and a Probabilistic Model of the Fatigue Environment[Dissertation],University of Oklahoma Graduate College,USA,2001:10.
  • 8Briges R.D.,Effect of cooling rate from mill annealing temperature on stress corrosion threshold of titanium 6Al-4V ELI beta annealed,[in] Advances in the Science and Technology of Titanium Alloy Processing,Warrendale,1996:413.
  • 9Shankar P.S.and Ravichandran K.S.,Fatigue response and micro mechanisms of crack initiation in Ti-10V-2Fe-3Al titanium alloy,[in] Fatigue Behavior of Titanium Alloys,TMS Fall Meeting'98,Chicago,1998:135.
  • 10Yoder G.R.,Cooley L.A.,and Boyer R.R.,Microstructure/crack tolerance aspects of notched fatigue life in Ti-10V-2Fe-3Al alloy,[in] Microstructure Fracture Toughness and Fatigue Crack Growth Rate in Titanium Alloys,ATMS-AIME Marriott,1987:209.

共引文献31

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