Effect of Solid Solution and Aging Process Parameters on Microstructure and Tensile Property of TA19 Titanium Alloy
摘 要
对TA19钛合金进行不同温度(930,960,990℃)固溶2 h+不同温度(550,590,630℃)时效8,16 h热处理,研究了工艺参数对显微组织与拉伸性能的影响。结果表明:不同温度固溶+590℃时效8 h处理后,随着固溶温度的升高,试验合金中的等轴α相含量降低,抗拉强度增大。经960℃固溶2 h处理后,试验合金的组织由等轴α相和α'马氏体组成,在后续550℃时效8 h过程中,α'马氏体分解不充分,颗粒状α相含量较少,合金抗拉强度增加有限;当时效温度升高到590℃,时效时间分别为8,16 h时,组织中析出细小弥散的颗粒状α相,抗拉强度提高;继续升高时效温度至630℃时,α相粗化,抗拉强度又有所下降。
Abstract
TA19 titanium alloy was treated by solid solution at different temperatures (930, 960, 990℃) for 2 h and then aging at different temperatures (550, 590, 630℃) for 8, 16 h. Effects of process parameters on microstructure and tensile property were studied. The results show that after solid solution at different temperatures and then aging at 590℃ for 8 h, the equiaxed α phase content in the test alloy decreased and the tensile strength was improved with the rise of solid solution temperature. After solid solution at 960℃ for 2 h, the microstructure of the test alloy was composed of equiaxed α phase and α' martensite. During the subsequent aging at 550℃ for 8 h, α' martensite decomposed unsufficiently, so the content of granular α phase was relatively small and therefore the tensile strength of the alloy increased limitedly. When the aging temperature rose to 590℃ and the aging time was 8 h and 16 h, fine and diffuse granular α phase precipitated in the microstructure, resulting in the increase of tensile strength. When the aging temperature continuously increased to 630℃, the α phase was coarsened and the tensile strength decreased.
中图分类号 TG166.5 DOI 10.11973/jxgccl201908002
所属栏目 试验研究
基金项目 国家自然科学基金资助项目(51461007,51761003)
收稿日期 2018/9/19
修改稿日期 2019/6/15
网络出版日期
作者单位点击查看
备注周烨(1977-),男,贵州贵阳人,高级工程师,学士
引用该论文: ZHOU Ye,DU Jianping,HAN Moliu,LIANG Yu. Effect of Solid Solution and Aging Process Parameters on Microstructure and Tensile Property of TA19 Titanium Alloy[J]. Materials for mechancial engineering, 2019, 43(8): 7~11
周烨,杜剑平,韩墨流,梁宇. 固溶时效工艺参数对TA19钛合金显微组织与拉伸性能的影响[J]. 机械工程材料, 2019, 43(8): 7~11
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【4】李明怡. 航空用钛合金结构材料[J]. 世界有色金属, 2000(6):17-20.
【5】LI D R, WANG K, YAN Z B, et al. Evolution of microstructure and tensile properties during the three-stage heat treatment of TA19 titanium alloy[J]. Materials Science and Engineering:A, 2018, 716:157-164.
【6】LI C, CHEN J, LI W, et al. Effect of heat treatment variations on the microstructure evolution and mechanical properties in a β metastable Ti alloy[J]. Journal of Alloys and Compounds, 2016, 684:466-473.
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【8】罗文忠,孙峰,赵小花,等.固溶处理对Ti60合金组织及拉伸性能的影响[J].稀有金属材料与工程,2017,46(12):3967-3971.
【9】徐建伟, 边丽虹, 薛强, 等. 固溶温度对TA19钛合金显微组织和力学性能的影响[J]. 钛工业进展, 2015, 32(6):27-30.
【10】SUN F, LI J, KOU H, et al. Effect of α' martensite on microstructure refinement after α+β isothermal treatment in a near-α titanium alloy Ti60[J]. Journal of Materials Engineering and Performance, 2015, 24(5):1945-1952.
【11】KUMAR V A, GUPTA R K, RAO G S. Solution treatment and aging (STA) study of Ti alloy Ti5Al3Mo1.5V[J]. Journal of Materials Engineering and Performance, 2015, 24(1):24-31.
【12】MCBAGONLURI F, AKPAN E, MERCER C, et al. An investigation of the effects of microstructure on fatigue crack growth in Ti-6242[J]. Journal of Engineering Materials and Technology, 2005, 127(1):46-57.
【13】SHI Z, GUO H, QIN C, et al. A method to determine main microstructural features influencing mechanical properties of two-phase titanium alloys[J]. Materials Science and Engineering:A, 2014, 611:136-141.
【14】JAWORSKI A, ANKEM S. Influence of the second phase on the room-temperature tensile and creep deformation mechanisms of α-β titanium alloys:Part I. Tensile deformation[J]. Metallurgical and Materials Transactions A, 2006, 37(9):2739-2754.
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