期刊文献+

20CrMnTi钢位错密度的测定及其位错形态研究 被引量:3

A study on dislocation densities and dislocation configuration in 20CrMnTi steel
在线阅读 下载PDF
导出
摘要 为了探讨20CrMnTi钢的冷变形强化过程位错密度的分布与位错形态,采用X射线衍射法及多晶单线付氏分析理论。在实验基础上测量了不同应变量冷变形时20CrMnTi钢的位错密度,分析了应变量与位错密度及加工硬化的关系,利用透射电子显微镜对冷镦粗件的位错形态进行了观察.结果表明,位错密度随变形量的增加而提高,同时,随变形量增加加工硬化效果增强,晶体位错形态为"曲折"形位错线,应变量较大时位错呈胞状结构. This paper analyses the density distribution and configuration of dislocation during the cold forming strengthen process of 20CrMnTi. This study can apply to practical production. By the way of X-ray diffraction method and Fourier's polycrystal single-line theory, the dislocation densities of 20CrMnTi are determined under different strains. Moreover, the dislocation mode of cold forging reduction pieces was observed with TEM. The results show that the dislocation density increases with the increase of the amount of deformation, and the larger the deformation, the more distinct the work hardening. In addition, crystal dislocation configuration is shown as 'tortous line'. When strain is large enough, dislocations are shown as crystiform sub-structure.
出处 《材料科学与工艺》 EI CAS CSCD 2004年第5期486-488,共3页 Materials Science and Technology
基金 国家"九五"科技攻关资助项目(96-A22-03-02)
关键词 20CRMNTI钢 位错密度 冷变形 加工硬化 冷镦 应变量 镦粗 体位 观察 增加 dislocation densities dislocation configuration cold defonnation
  • 相关文献

参考文献7

二级参考文献22

  • 1沈以赴,周本濂,何冠虎,姚戈,鄢红春.材料疲劳恢复新途径的探索Ⅰ──低碳钢疲劳寿命的延长[J].材料研究学报,1996,10(2):165-166. 被引量:33
  • 2杜百平.间隙回火对疲劳损伤件寿命恢复的作用[J].北京科技大学学报,2001,23:42-44.
  • 3L.F蒙多尔福 王祝堂 等译.铝合金的组织与性能[M].北京:冶金工业出版社,1984.9.
  • 4[1]Hansen J O, Sound H , Novotnak D, et al. Heat treatment to reduce embrittlement of titanium alloys[P]. US Patent: 5397404, 1995-03-14.
  • 5[2]Giary K. High-strength titanium resistant ignition[J]. Advanced Materials and Processes, 1993, 9: 7-10.
  • 6[3]Seagle S R. The state of the USA titanium industry in 1995[J]. Materials Science and Engineering A, 1996, 213: 1-7.
  • 7[4]Boyer R R. An overview on the use of titanium in the aerospace industry[J]. Materials Science and Engineering A, 1996, 213: 103-114.
  • 8[5]Li Y G, Zhang X D, Blenkinsop P A, et al. The development and evaluation of β titanium alloys for aerospace applications[A]. Blenkinsop P A, Evens W J. Proceedings of the 8th World Conference on Titanium[C]. London: The Institute of Materials, 1996. 2317-2324.
  • 9[6]Li Y G, Blenkinsop P A, Loretto M H, et al. Effect of aluminium on ordering of highly stabilized β-Ti-V-Cr alloys[J]. Materials Science and Technology, 1998, 14(8): 732-737.
  • 10[7]Li Y G, Blenkinsop P A, Loretto M H, et al. Effect of aluminium on deformation structure of highly stabilized β-Ti-V-Cr alloys[J]. Materials Science and Technology, 1999, 15(2): 151-155.

共引文献55

同被引文献23

引证文献3

二级引证文献7

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