期刊文献+

Effect of microstructure on impact toughness of TC21 alloy

Effect of microstructure on impact toughness of TC21 alloy
下载PDF
导出
摘要 The impact toughness of TC21 alloy after different types of forging and heat treatments was studied. The results show that heat treatment at 915 ℃ for 1 h followed by air-cooling can achieve the highest impact toughness. The crack propagation path of bimodal microstructure is different from that of lamellar microstructure. Boundaries of primary α grain are observed to be preferential sites for microcrack nucleation. With the increase of heat treatment temperature,the volume fraction of primary α phase decreases and the nucleation sites of microcrack at the primary α phase boundaries also decrease,the impact toughness value is effectively improved. The microcracks of lamellar microstructure are located on α/β interface,or the boundary of colony,and/or grain boundary α phase. The crack propagates cross the colony,or along the colony boundary,and/or along β grain boundary. The crack propagation path of lamellar microstructure is dependent on the size,direction of colony. The crack path deflects at grain boundaries,colony boundaries,or arrests and deviates at α/β interface because of crisscross α lamellar. Therefore the impact toughness value of basket microstructure is higher than that of Widmanstatten microstructure. The impact toughness of TC21 alloy after different types of forging and heat treatments was studied. The results show that heat treatment at 915℃ for 1 h followed by air-cooling can achieve the highest impact toughness. The crack propagation path of bimodal microstructure is different from that of lamellar microstructure. Boundaries of primary a grain are observed to be preferential sites for microcrack nucleation. With the increase of heat treatment temperature, the volume fraction of primary a phase decreases and the nucleation sites of microcrack at the primary α phase boundaries also decrease, the impact toughness value is effectively improved. The microcracks of lamellar microstructure are located on α/β interface, or the boundary of colony, and/or grain boundary a phase. The crack propagates cross the colony, or along the colony boundary, and/or along β grain boundary. The crack propagation path of lamellar microstructure is dependent on the size, direction of colony. The crack path deflects at grain boundaries, colony boundaries, or arrests and deviates at α/β interface because of crisscross a lamellar. Therefore the impact toughness value of basket microstructure is higher than that of Widmanstatten microstructure.
出处 《中国有色金属学会会刊:英文版》 CSCD 2007年第A01期93-98,共6页 Transactions of Nonferrous Metals Society of China
基金 Project (2007CB613805) supported by the National Basic Research Program of China
关键词 钛合金 微观结构 压力 抗压强度 TC21 titanium alloy bi-modal microstructure lamellar microstructure impact toughness
  • 相关文献

参考文献1

二级参考文献8

  • 1ChenYali(陈亚莉).Materials Selection Analysis of F-22Fighter USA(美国F-22先进战斗机选材分析)[R].Beijing:Aeronautical Information Center of China,1995.1-5.
  • 2Wanhill R J H. Ambient Temperature Crack Growth in Titanium Alloys and Its Significance for Aircraft Structures[J]. Aeronautical Journal, 1977, 81: 68~82
  • 3Lutjering G. Influence of Processing on Microstructure and Mechanical Properties ofα+β Titanium Alloys[J]. Mat Sci Eng A, 1998, A243:32~45
  • 4Wang Jinyou(王金友),Ge Zhiming(葛志明)et al.Aeronautical Titanium Alloys(航空用钛合金)[M].Shanghai:Shanghai Science and Technology Press, 1985:208~231
  • 5Jafee R I, Burte H M. Titanium Science and Technology[M]. New York-London: Plenum Press, 1973: 1 257~1 270, 1 731~1 744
  • 6Yao Zekun(姚泽坤),Guo Hongzhen(郭鸿镇),Su Zuwu(苏祖武)et al.Efiect of Microstructure and Recrystallization and Mechanical Properties of Two-Phase(a+β)Ti Alloy[J].RareMetal Materials and Engineering(稀有金属材料与工程),2000,29(5):340~343
  • 7Zhang Wangfeng(张旺峰).Strengthen-Toughening Technology andthe Relationships between Structure and Mechanical Properties for TA15 Titanium alloy(TA15钛合金强韧化技术及组织与性能的关系)[R].Beijing:BeijingInstitute of Aeronautical Materials,2002
  • 8姚泽坤,郭鸿镇,杨陈,虢迎光,苏梅英.形变、相变交互作用对Ti-17合金等温锻件显微组织和力学性能影响规律研究[J].稀有金属材料与工程,2003,32(7):538-541. 被引量:3

共引文献34

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