Lamellar Microstructure's Evolution Mechanism for Ti-8Al-1Mo-1V Titanium Alloy During Hot Rolling and Subsequent Annealing Based on Dislocation Density Analysis
SHI Xiaohui, CAO Zuhan, ZHANG Min, GUO Ruipeng, QIAO Junwei
College of Materials Science and Engineering, Taiyuan University of Technology, Taiyuan 030024, China
Abstract: The lamellar microstructure's evolution pattern and mechanism for Ti-8Al-1Mo-1V titanium alloy during hot rolling and subsequent annealing were studied by means of OM, EBSD, TEM etc. The results show that: hot rolling and subsequent annealing can not easily realize the glo-bularization of lamellar α phase. These processes can only realize the continuous distribution of α phase as well as the globularization of β phase. Insufficient accumulation of dislocation density during hot rolling is the main reason causing the lack of driving force for recrystallization for lamellar α. By comparing with the thick lamellar α phase, the thin and tiny β phase can be more easily broken into segments under the same rolling force. In the following annealing process, the segmented β phase can realize globularization through diffusion. Based on analyses, this work proposes the lamellar microstructure's evolution mechanism for Ti-8Al-1Mo-1V titanium alloy. In addition, it is found that the (0221)[3122] planar texture can be formed during the hot rolling of Ti-8Al-1Mo-1V titanium alloy with lamellar microstructure.
石晓辉, 曹祖涵, 张敏, 郭瑞鹏, 乔珺威. 基于位错密度分析的Ti-8Al-1Mo-1V钛合金片层组织在热轧及退火过程中的演变机制[J]. 材料导报, 2020, 34(12): 12101-12104.
SHI Xiaohui, CAO Zuhan, ZHANG Min, GUO Ruipeng, QIAO Junwei. Lamellar Microstructure's Evolution Mechanism for Ti-8Al-1Mo-1V Titanium Alloy During Hot Rolling and Subsequent Annealing Based on Dislocation Density Analysis. Materials Reports, 2020, 34(12): 12101-12104.
1 Zhao Y Q, Zhu K Y, Li Z C, et al. Rare Metal Materials and Enginee-ring,1997,26(3),35(in Chinese). 赵永庆,康英,李佐臣,等.稀有金属材料与工程,1997,26(3),35. 2 Dastidar I G, Khademi V, Bieler T R, et al. Materials Science and Engineering: A,2015,636,289. 3 Tao C H, Liu Q Q, Cao C X, et al. Failure and prevention of aeronautical titanium alloy, National Defence Industry Press, China,2002(in Chinese). 陶春虎,刘庆泉,曹春晓,等.航空用钛合金的失效及其预防,国防工业出版社,2002. 4 Dang M, Qi G X, Shi L K. Hot Working Technology,2010,39(4),44(in Chinese). 党淼,齐广霞,史丽坤.热加工工艺,2010,39(4),44. 5 Yang K, Zhong B, Huang Q, et al. International Journal of Fatigue,2018,116,80. 6 Zhang X H, Liu D X. International Journal of Fatigue,2009,31(5),889. 7 Jiao Z H, Yu H C, Zhong B, et al. Journal of Aeronautical Materials,2017,37(3),84(in Chinese). 焦泽辉,于慧臣,钟斌,等.航空材料学报,2017,37(3),84. 8 Leyens C, Peters M. Titanium and titanium alloys: fundamentals and applications,Wiley-VCH,2003. 9 Qi G X, Yu G Y, Chen X F. Forging and Stamping Technology,2011,36(2),111(in Chinese). 齐广霞,于广义,陈晓峰.锻压技术,2011,36(2),111. 10 Balachandran S, Kumar S, Banerjee D. Acta Materialia,2017,131,423. 11 Wang Y, Zeng W D, Ma X, et al. The Chinese Journal of Nonferrous Metals,2013,23(7),1861(in Chinese). 王扬,曾卫东,马雄,等.中国有色金属学报,2013,23(7),1861. 12 Wang K X, Zeng W D, Zhao Y Q, et al. Materials Science & Enginee-ring: A,2010,527(10-11),2559. 13 Kubin L P, Mortensen A. Scripta Materialia,2003,48,119. 14 Calcagnotto M, Ponge D, Demir E, et al. Materials Science & Enginee-ring: A,010,527(10-11),2738. 15 Wang H, Xu D S, Yang R. The Chinese Journal of Nonferrous Metals,2010,20(s1),457. 王皞,徐东生,杨锐.中国有色金属学报,2010,20(s1),457. 16 Elyas R, Mansour F, Ali G M, et al. ISRN Corrosion,2013,2013,1. 17 Stefansson N, Semiatin S L. Metallurgical and Materials Transactions A,2003,34(3),691. 18 Chen Z Y, Cai H N, Wang F C, et al. Rare Metal Materials and Engineering,2010,39(12),2101(in Chinese). 陈志永,才鸿年,王富耻,等.稀有金属材料与工程,2010,39(12),2101. 19 You L, Song X P. Acta Metallurgica Sinica,2008,44(11),1310(in Chinese). 尤力,宋西平.金属学报,2008,44(11),1310. 20 Kou H C, Chen Y, Tang B, et al. Journal of Alloys and Compounds,2014,603,23. 21 Sander B, Raabe D. Materials Science and Engineering: A,2008,479(1-2),236. 22 Wang Y N, Huang J C. Materials Chemistry and Physics,2003,81,11.