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不同应变速率下TA15钛合金β形变过程中动态再结晶行为 被引量:16

Dynamic Recrystallization of Titanium Alloy TA15 during β Hot Process at Different Strain Rates
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摘要 研究TA15钛合金在1050℃时,不同应变速率下变形过程中动态再结晶组织演变,讨论动态再结晶动力学、形核率和晶粒尺寸的演变规律。结果表明,随高低应变速率不同,存在两种类型的动态再结晶现象:连续动态再结晶和不连续动态再结晶。动力学分析应变速率为0.01,0.1,1s-1时,对应的动态再结晶稳态应变分别为1.26,1.57,2.93,说明增大应变速率则相应地提高稳态应变,在高应变速率条件下,往往难于达到稳态阶段。高应变速率下的形核率明显高于低应变速率下的形核率,且低应变速率下,较小幅度的增大应变速率就能使晶粒尺寸较大幅度下降;而在较高应变速率下,晶粒尺寸变化随应变速率改变较小。采用高应变速率及大应变下发生的连续动态再结晶可实现组织明显细化。 Dynamic recrystallization microstructure evolution of titanium alloy TA15 was investigated during deformation at 1050 oC and different strain rates.The dynamic recrystallization kinetics,nucleation rate and grain size evolution were discussed.Results show that with different strain rates there are two types of dynamic recrystallization,i.e.the continuous and the discontinuous.According to the dynamic analysis,at the strain rates of 0.01,0.1 and 1 s-1,the corresponded dynamic recrystallization steady strains are 1.26,1.57 and 2.93,indicating higher strain rates lead to higher steady strain.It is hard to reach steady stage at higher strain rates while the nucleation is obviously higher than that at lower strain rates.At lower strain rate,a slight increment of strain rates can greatly decrease the grain size;however,at higher strain rates,the grain size is little dependent on the strain rates.Therefore,refinement of structure can be obtained by the continuous dynamic recrystallization at high strain rate and large strain.
出处 《稀有金属材料与工程》 SCIE EI CAS CSCD 北大核心 2011年第2期325-330,共6页 Rare Metal Materials and Engineering
基金 江西省自然科学基金(2008GZC0041) 江西省教育厅科技项目(GJJ08203) 南昌航空大学航空高校基金(EC200801145)
关键词 β形变 动态再结晶 TA15钛合金 β hot process dynamic recrystallization TA15 titanium alloy
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  • 1王永强,陶海林,冯永琦,张永强,魏寿庸.加热温度及冷却速度对BT20钛合金组织与性能的影响[J].金属学报,2002,38(z1):87-88. 被引量:4
  • 2蔡建明,郝孟一,杜娟,李臻熙,李四清,马济民,曹春晓.SP700钛合金的晶粒细化[J].金属学报,2002,38(z1):147-149. 被引量:6
  • 3李兴无,刘瑞民,沙爱学,储俊鹏,张旺峰,马济民.显微组织对TA15合金疲劳性能的影响[J].金属学报,2002,38(z1):280-281. 被引量:10
  • 4杨王玥,金属学报,2000年,36卷,1期,1192页
  • 5Wang R Z,Son Metall Mater,1994年,31卷,9期,1192页
  • 6ChenYali(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.
  • 7Wanhill R J H. Ambient Temperature Crack Growth in Titanium Alloys and Its Significance for Aircraft Structures[J]. Aeronautical Journal, 1977, 81: 68~82
  • 8Lutjering G. Influence of Processing on Microstructure and Mechanical Properties ofα+β Titanium Alloys[J]. Mat Sci Eng A, 1998, A243:32~45
  • 9Wang 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
  • 10Jafee R I, Burte H M. Titanium Science and Technology[M]. New York-London: Plenum Press, 1973: 1 257~1 270, 1 731~1 744

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