期刊文献+

热处理工艺对Ti53311S钛合金组织与性能的影响

Effect of Heat Treatment on Microstructure and Mechanical Properties of Ti53311S Titanium Alloy
下载PDF
导出
摘要 研究了低温退火和高温淬火+时效两种热处理方式对Ti53311S钛合金棒材显微组织与力学性能的影响。实验结果表明:经两种不同热处理制度处理后,均能获得满足Q/XB 1517—1998标准要求的Ti53311S钛合金棒材。经650℃低温退火处理后可获得等轴α+β组织,经高温淬火+时效处理后可获得等轴初生α+含针状α的转变β双态组织。在生产中,可根据实际情况选取更为适宜的热处理方式,其中,较为经济的热处理方式为650℃×60min/AC;可获得较好力学性能的热处理方式为980℃×(30~90)min/WQ+650℃×6h/AC。 Low temperature annealing and high temperature quenching combines with aging were two common heat treatment processes, and the effects of these processes on microstructure and mechanical properties of Ti53311S titani- um alloy were investigated. The results show that properties of Ti53311S titanium bars processed by them both can meet the standard of Q/XB 1517--1998. Equiaxial primary a +β structure is obtained at the 650 ℃ annealing. When quenched at high temperature and aged at 650℃, the microstructure is double phase. The proper heat treatment process can be selected by the situation, the more economical heat treatment processing is 650 ℃ × 60 min/AC, and better mechanical properties can be obtained by using 980℃ ×(30 - 90) min/WQ + 650℃ × 6 h/AC.
出处 《钛工业进展》 CAS 2013年第1期23-26,共4页 Titanium Industry Progress
关键词 Ti53311S钛合金 热处理 显微组织 力学性能 Ti53311S titanium alloy heat treatment microstructure mechanical properties
  • 相关文献

参考文献4

二级参考文献29

  • 1马济民 曹春晓.航空用钛合金的新进展[J].稀有金属,1997,21:1-9.
  • 2胡清熊 刘振球 魏寿庸.宝鸡钛的35年[J].金属学报,1999,35:15-21.
  • 3毛小南 周廉 等.TIC颗粒增强钛基复合材料的界面反应动力学[J].金属学报,1999,35(1):339-343.
  • 4Boyer R R.Mater Sci Eng,1996,A213:103-107
  • 5Giary K.Advanced Mater Proc,1993,(9):7
  • 6Boyer R R. Proc. of 9th World Conference on Ti, 1999, Russia(in press)
  • 7Zhou Y G, Zeng W. D, Yu H Q.Mater Sci. Eng, 1996,A211:58-62
  • 8吴之乐.第七届全国钛及钛合金学术交流会论文集,1990:516-518
  • 9Han Chuanxi. Proc. of 7th World Conference on Ti, 1992
  • 10Zhao Y Q, Zhu KY, Qu H L, et.al. Mater, Sci. Eng, 2000,A282:153-157

共引文献101

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