|
|
Effect of solution aging treatment on microstructure and properties of TC4 titanium alloy |
XU Jian1, WANG Wen-yan1,2, ZHANG Hao-yin1, XIE Jing-pei1,2, LI Luo-li1 |
1. School of Material Science and Engineering, He’nan University of Science and Technology, Luoyang 471003, China 2. He’nan Key Laboratory of Non-Ferrous Materials Science and Processing Technology, Luoyang 471023, China |
|
|
Abstract TC4 titanium alloy powder was prepared with the method of cold isostatic pressing and vacuum sintering. By adopting different solution temperature and aging temperature, the effect of heat treatment process on microstructure and properties of TC4 powder metallurgy titanium alloy was studied. The results show that tensile strength and elongation of TC4 powder metallurgy titanium alloy can reach 852 MPa and 16%, respectively. With the improvement of solid solution temperature, the tensile strength increases and the elongation decreases. With the improvement of aging temperature, the tensile strength decreases and the elongation increases. When solid solution treated at 960 ℃ for 30 min and aged at 470 ℃ for 4 h, tensile strength of the alloy reaches 1 078 MPa, and the elongation reaches 11%.
|
Received: 31 December 2013
Published: 16 October 2014
|
|
|
|
[1] |
侯红亮, 李志强, 王亚军, 等.钛合金热氢处理技术及其应用前景[J].中国有色金属学报, 2003, 13(3):533-549
|
[2] |
曹春晓.一代材料技术, 一代大型飞机[J].航空学报, 2008, 29(3)701-706.
|
[3] |
王亮.高性能钛合金粉末冶金技术研究[J], 宇航材料工艺, 2003, (3):42~44.
|
[4] |
汤慧萍, 刘咏, 韦伟峰, 陈丽芳.添加稀土元素对粉末冶金合金显微组织和力学性能的影响[J].中国有色金属学报, 2004, 14(2):244-
|
[5] |
赵嘉琪, 南海, 黄东.氢合金化钛合金粉末成形制件技术的发展[J].特种铸造及有色合金, 2007, 27(8):593-596
|
[6] |
刘咏, 汤慧萍.粉末冶金钛基结构材料[M].长沙:中南大学出版社, 2012:26.
|
[7] |
马玲.热等静压温度对铍铝合金显微组织及力学性能的影响[J].飞航导弹, 2006, 8:57~59.
|
[8] |
李承爱.空间环境条件下材料的失效[J]. 宇航学报, 1992, (1):1—7.
|
[9] |
张民.热处理对TC21钛合金组织和性能的影响[D].西安:西北工业大学, 2004.
|
|
|
|