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分别以1020℃保温30 min后空冷和炉冷得到的TA15合金为原材料,对其进行等温恒应变速率压缩试验,研究了温度800~950℃、应变速率0.001~1 s-1、真应变0.51~1.20时,不同原始α片层厚度对TA15合金动态球化行为的影响.结果表明:真应力-真应变曲线均呈现出明显的流动软化,峰值应力和流动软化率对α片层厚度的依赖程度较小.当热变形参数相同时,细片状比粗片状组织更容易发生动态球化,这与其在试验范围内测得的变形激活能分别为597 kJ/mol和650 kJ/mol是一致的.TA15合金中片状α除了形成低和高角度界面及强烈的局部剪切带导致动态球化外,还有动态再结晶等其它方式.

Soaked at 1020 ℃ for 30 min and then followed by air and furnace cooling to room temperature,two kinds of microstructure with alpha lamella of different thickness in TA15 alloy were obtained,respectively.The influence of thickness of alpha lamella on dynamic globularization behavior of the alloy was studied at 800-950℃ and strain rate range of 0.001-1 s-1 through isothermal constant strain rate compression tests with true strain varied from 0.51 to 1.20.The results show that all the true stress-true stain curves exhibit sharp flow softening,and no significant effect of the thickness of alpha lamella on the peak stress and flow softening rate is observed.Under the same hot deformation condition,the dynamic globularization of thin lamellar alpha occurs more easily than that of thick lamellar alpha,which is in accordance with the corresponding deformation activation energy 597 kJ/mol for thin lamellar alpha and 650 kJ/mol for thick lamellar alpha in the temperature and strain rate range involved.Besides the interface separation of low and high angle alpha/alpha boundaries and shear bands across alpha plates,the dynamic recrystallization lead to dynamic globularization.

参考文献

[1] 周军,曾卫东,舒滢,周义刚.应用热加工图研究TC17合金片状组织球化规律[J].稀有金属材料与工程,2006(02):265-269.
[2] S. L. SEMIATIN;T. R. BIELER .THE EFFECT OF ALPHA PLATELET THICKNESS ON PLASTIC FLOW DURING HOT WORKING OF Ti-6Al-4V WITH A TRANSFORMED MICROSTRUCTURE[J].Acta materialia,2001(17):3565-3573.
[3] 李兴无,沙爱学,张旺峰,储俊鹏,马济民.TA15合金及其在飞机结构中的应用前景[J].钛工业进展,2003(04):90-94.
[4] 刘黎明,杜鑫,张兆栋,王敏,李锋.TA15钛合金接头活性剂补焊的组织特征[J].中国有色金属学报,2005(12):1910-1916.
[5] 王向明,刘文珽,贺小帆.TA15板与电子束焊接疲劳特性研究[J].北京航空航天大学学报,2003(09):807-811.
[6] 曹京霞,黄旭,李臻熙.TA15钛合金的高周疲劳性能和断裂特征[J].材料工程,2004(03):28-30,34.
[7] 范荣辉,朱明,惠松骁,叶文君,于洋,李士凯.TA15(ELI)钛合金厚板损伤容限性能研究[J].金属热处理,2007(02):27-30.
[8] 李士凯,熊柏青,惠松骁.热处理制度对TA15合金组织与性能的影响[J].材料热处理学报,2008(06):82-85.
[9] 王洋,尤逢海,朱景川,来忠红,刘勇.TA15合金热变形行为研究[J].机械工程材料,2006(11):63-65,98.
[10] 李淼泉,李晓丽,龙丽,许广兴,于浩,迟彩楼,温国华.TA15合金的热变形行为及加工图[J].稀有金属材料与工程,2006(09):1354-1358.
[11] 徐文臣,单德彬,李春峰,吕炎.TA15钛合金的动态热压缩行为及其机理研究[J].航空材料学报,2005(04):10-15,19.
[12] Verlinden B;Wouters P;McQueen H J et al.Effect of different homogenization treatments on the hot workability of aluminium alloy AA2024[J].Materials Science and Engineering A,1990,123:229-237.
[13] Shell E B;Semiatin S L .Effect of initial microstructure on plastic flow and dynamic globularization during hot working of Ti-6Al-4V[J].Metallurgical and Materials Transactions A:Physical Metallurgy and Materials Science,1999,30:3219-3229.
[14] 洪权,张振祺,赵永庆,曲恒磊,魏寿庸.Ti-6Al-2ZR-1Mo-1V合金的热压变形特性及塑性b动方程[J].广东有色金属学报,2001(02):129-133.
[15] 梁业,郭鸿镇,刘鸣,张伏层,姚泽坤.TA15合金高温本构方程的研究[J].塑性工程学报,2008(04):150-154.
[16] Margolin H;Cohen P.Evolution of the equiaxed morphology of phases in Ti-6Al-4V[A].TMS:Warrendale:PA,1980:1554-1561.
[17] 孙新军 .钛合金片层组织的等轴化规律及超细晶钛合金超塑性的研究[D].清华大学,1999.
[18] Weiss I;Froes F H;Eylon D et al.Modification of alpha morphology in Ti-6Al-4V by thermomechanical processing[J].Metallurgical and Materials Transactions A:Physical Metallurgy and Materials Science,1986,17:1935-1947.
[19] Semiatin SL;Weiss I;Seetharaman V .Flow behavior and globularization kinetics during hot working of Ti-6Al-4V with a colony alpha microstructure[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1999(2):257-271.
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