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用Gleeble-1500型热模拟机研究TC4-DT钛合金在850~1100℃、应变速率0.001~10 s-1、变形量70%条件下的高温压缩热变形行为,分析了该合金的流变应力行为以及显微组织演变规律,建立了该合金的本构关系模型以及热加工图。研究结果表明, TC4-DT 钛合金在两相区和β相区的热变形激活能分别为544.03 kJ· mol-1和264.32 kJ· mol-1 ,分别大于纯α相和纯β相的自扩散激活能,表明TC4-DT钛合金热变形由高温扩散以外的过程控制。在两相区热变形时,原始组织发生了不同程度的球化,且变形温度越低球化效果越好。在β相区热变形时,低应变速率下(0.001~0.1 s-1)主要发生动态再结晶,而高应变速率(1~10 s-1)下主要发生动态回复,动态再结晶行为受到抑制。 TC4-DT钛合金的失稳区主要分布在低温高应变速率区域,变形温度主要在850~940℃,应变速率主要在0.1~10 s-1,功率耗散率η值小于28%。

Hot compressive deformation of TC4-DT titanium alloy was carried out with the hot-simulation machine of Gleeble-1500 at the deformation degree of 0.7, over the range of deformation temperature from 850 ℃ to 1 100 ℃, strain rate from 0.001 s-1 to 10 s-1 .The deformation behavior and microstructure evolution were analyzed, meanwhile the constitutive model and hot processing map were set up.The results reveal that the deformation activation energy of TC4-DT titanium alloy are 544.03 kJ · mol-1 in two-phase region and 264.32 kJ · mol-1 in βphase region respectively, larger than self diffusion activation energy of pureαandβphase, which shows the thermal deformation of TC4-DT titanium alloy is controlled by high temperature diffusion process.When the alloy is deformed in two-phase region, the globularization intensity increases obviously with temperature decreasing.In the βphase region, the dynamic recrystallization occurs at low strain rate ( 0.001 s -1 to 0.1 s-1 ) and the dynamic recovery occurs at high strain rate (1 s-1 to 10 s-1 ) .Furthermore, the instability zone of TC4-DT titanium alloy is mainly distributed in the low temperature and high strain rate region where the deformation temperature range from 850℃to 940℃, the strain rate range from 0.1 s-1 to 10 s-1 , and the power dissipation rate (η) is lesser than 28%.

参考文献

[1] 王金友;葛志明;周彦邦.航空用钛合金[M].上海:上海科学技术出版社,1985:78-79.
[2] 曹春晓.选材判据的变化与高损伤容限钛合金的发展[J].金属学报,2002(z1):4-11.
[3] 袁鸿,余槐,王金雪,王新南,朱知寿,李晓红.TC4-DT钛合金电子束焊接接头的损伤容限性能[J].材料工程,2007(08):17-19.
[4] 李辉,赵永庆,曲恒磊,曾卫东.损伤容限型TC4-DT合金疲劳裂纹扩展行为研究[J].稀有金属材料与工程,2007(06):963-967.
[5] 刘青,薛祥义,付宝全,王一川.TC4-DT钛合金的热变形行为研究[J].热加工工艺,2009(12):43-47.
[6] 朱知寿,马少俊,王新南,童路,吴学仁,赵永庆,曲恒磊.TC4-DT损伤容限型钛合金疲劳裂纹扩展特性的研究[J].钛工业进展,2005(06):10-13.
[7] 于兰兰,毛小南,李辉.温度对TC4-DT损伤容限型钛合金疲劳裂纹扩展行为的影响[J].稀有金属快报,2007(12):20-23.
[8] 李辉,曲恒磊,赵永庆,曾卫东,冯亮,陈军.显微组织对Ti-6Al-4V ELI合金疲劳裂纹扩展速率的影响[J].稀有金属快报,2006(03):26-29.
[9] 王小芳,陈明和,陈伟,朱知寿.TC4-DT钛合金高温热变形行为研究[J].航空材料学报,2012(01):30-34.
[10] 刘杰,李落星,李光耀,钟志华.AZ61镁合金高温变形应力修正及本构方程的建立[J].热加工工艺,2007(17):1-4.
[11] Sastry S M L;Pao P S;Sankaran K K.High temperature deformation of Ti-6Al-4V[A].Warrendale:The Metallurgical Society of AIME,1980:873-886.
[12] Philippart I.;Rack HJ. .High temperature dynamic yielding in metastable Ti-6.8Mo-4.5Fe-1.5Al[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1998(1/2):196-200.
[13] Prasad Y;Gegel H L;Doraivelu S M et al.Modeling of dynamic material behavior in hot deformation:forging of Ti-6242[J].Metallurgical Transactions A,1984,15(10):1883-1892.
[14] Ziegler H.Some extremum principles in irreversible thermo-dynamics with application to continuum mechanics[A].Amsterdam:North-Holland Publishing Company,1963:93.
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