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TC11合金β相区大应变热变形行为及组织研究
引用本文:李鑫,赵为纲,鲁世强,王克鲁. TC11合金β相区大应变热变形行为及组织研究[J]. 兵器材料科学与工程, 2007, 30(3): 28-33
作者姓名:李鑫  赵为纲  鲁世强  王克鲁
作者单位:1. 南京航空航天大学,材料科学与技术学院,江苏,南京,210016;南昌航空工业学院,材料科学与工程学院,江西,南昌,330034
2. 南昌航空工业学院,材料科学与工程学院,江西,南昌,330034
摘    要:利用热模拟试验机,在温度为1020~1080℃和应变速率为0.001~70 s~(-1)范围内对TC11合金进行真应变为1.2的大应变等温恒应变速率压缩试验,获悉高温塑性流动的应力-应变关系曲线特征,并对变形前后的微观组织进行观察。结果表明:流动应力随应变速率升高和温度降低而增加,但前者比后者对流动应力的影响更为显著;在所研究的温度范围内,当应变速率大于10.0 s~(-1)时,变形组织主要为拉长的β晶粒;当应变速率在1.0~0.01 s~(-1)之间时,变形试样分别发生部分动态再结晶和完全动态再结晶;当应变速率为0.001 s~(-1)时,变形试样以动态回复为主。为获得良好的变形组织,热加工区域以温度在1020~1050℃,应变速率在0.01~1.0 s~(-1)范围为宜。

关 键 词:TC11合金  热态压缩  流动应力  微观组织  变形机制
文章编号:1004-244X(2007)03-0028-05
修稿时间:2006-05-10

Investigation on hot deformation behavior and microstructure of TC11 alloy at large strain during β-phase
LI Xin,ZHAO Wei-gang,LU Shi-qiang,WANG Ke-lu. Investigation on hot deformation behavior and microstructure of TC11 alloy at large strain during β-phase[J]. Ordnance Material Science and Engineering, 2007, 30(3): 28-33
Authors:LI Xin  ZHAO Wei-gang  LU Shi-qiang  WANG Ke-lu
Affiliation:1. Institute of Materials Science and Technology, Nanjing University of Aeronautics and Astronautics, Nanjing 210016,China; 2. Institute of Materials Science and Engineering, Nanchang Institute of Aeronautical Technology, Nanchang 330034,China
Abstract:The isothermal constant strain rate compression tests of TC11 alloy were conducted up to a large strain of 1.2 in the temperature range 1 020~1080℃and strain rate range 0.001~70.0 s~(-1)by using the Thermecmastor-Z hot working simulator.The characteristic of high temperature plastic flow stress-strain curves was revealed,and the microstructures of the pressed samples with those before pressing were investigated.The results showed that the flow stress increased with the increase of strain rate and the decrease of temperature,but the former influenced the flow stress more markedly than the later.In the temperature range studied,elongatedβgrains were developed in the strain rate range 10.0~70.0 s~(-1),part or full dynamic recrystaUization ofβgrains occurred in the strain rate range 0.01~1.0 s~(-1),and dynamic recovery ofβgrains predominates at 0.001 s~(-1).To obtain the desirable deformed microstructures,the optimum hot working conditions for TC11 alloy were found out in the temperature range 1 020~1 050℃and strain rate range 0.01~1.0 s~(-1).
Keywords:TC11 alloy   hot compression   flow stress   microstructure   deformation mechanism
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