期刊文献+

Hot compressive deformation behaviors and micro-mechanisms of TA15 alloy 被引量:3

Hot compressive deformation behaviors and micro-mechanisms of TA15 alloy
下载PDF
导出
摘要 The hot deformation behaviors of TA15 alloy,as well as the microstructure obtained after compressive deformation,were investigated.The results show that TA15 alloy exhibits a peak stress when deformed at temperature lower than 900 ℃,implying recrystallization characteristics.However,steady flow stress-stain behavior is observed without peak stress when deformation is employed at temperature higher than 900 ℃,showing recovery characteristics.Micro-deformation band appears at deformation temperature of 750 ℃,and equiaxed grains are found at 800 ℃,implying the occurrence of recrystallization.When deformed at 925 ℃,the specimen shows the recovery characteristics with dislocation networks and sub-grain boundaries. The hot deformation behaviors of TA15 alloy,as well as the microstructure obtained after compressive deformation,were investigated.The results show that TA15 alloy exhibits a peak stress when deformed at temperature lower than 900 ℃,implying recrystallization characteristics.However,steady flow stress-stain behavior is observed without peak stress when deformation is employed at temperature higher than 900 ℃,showing recovery characteristics.Micro-deformation band appears at deformation temperature of 750 ℃,and equiaxed grains are found at 800 ℃,implying the occurrence of recrystallization.When deformed at 925 ℃,the specimen shows the recovery characteristics with dislocation networks and sub-grain boundaries.
出处 《Rare Metals》 SCIE EI CAS CSCD 2007年第S1期162-167,共6页 稀有金属(英文版)
关键词 TA15 alloy hot compressive deformation micro-mechanisms TA15 alloy hot compressive deformation micro-mechanisms
  • 相关文献

参考文献8

  • 1徐文臣,单德彬,吕炎,李春峰.Effects of hot deformation parameters on flow stress and establishment of constitutive relationship system of BT20 titanium alloy[J].中国有色金属学会会刊:英文版,2005,15(S2):167-172. 被引量:6
  • 2Li Xingwu,Sha Aixue,Zhang Wangfeng.TA15 al- loy and its applications in plane constructions. Progress in TitaniumIndustry . 2003
  • 3Brun M,and Shachanova G.Titanium alloy structure and parameters definingits diversity. Ti- taniumScientific Technical Journal . 1993
  • 4Zhou Y.G,Zeng W.D,and Yu H.Q.Anin- vestigation of a newnear-betaforging processforti-taniumalloys andits applicationin aviation compo- nents. Materials Science and EngineeringA . 2005
  • 5Li Miaoquan,Pan Hongsi,Lin Yingying,LuoJiao.Hightemperature deformationbehavior of near alpha Ti-5 6Al-4 .8Sn-2 .0Zr alloy. Journal of Materials Science Letters . 2007
  • 6Barboza M.J.R,Perez E.A.C,Medeiros M. M,Reis D.A.P,Nono M.C.A,Piorino Neto F,and Silva C.R.M.Creep behavior of Ti-6Al- 4Vand a comparison withtitanium matrix compos- ites. Journal of Materials Science . 2006
  • 7Vo P,Jahazi M,Yuea S,and Bocher P.Flowstress prediction during hot working of near-α titaniumalloys. Journal of Materials Science . 2007
  • 8Warchomicka F,Stockinger M,and Degischer H.P.Quantitative analysis ofthe microstructure of near-titaniumalloy during compressiontests. Jour- nal ofMaterials ProcessingTechnology . 2006

共引文献5

同被引文献3

引证文献3

二级引证文献19

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