Influence of Forging Temperature on Microstructure and Tensile StrengthAeolotropy of TA15 Titanium Alloy
摘 要
在(α+β)相区对TA15钛合金棒进行锻造,研究了tβ-15℃、tβ-30℃和tβ-50℃(tβ为β相变温度)3种锻造温度对合金显微组织和抗拉强度各向异性的影响。结果表明:随着锻造温度降低,TA15钛合金中初生αp相含量增加,片层状α相含量减少,厚度和长宽比减小,抗拉强度提高;TA15钛合金在tβ-50℃温度锻造后沿流线方向的抗拉强度可达973 MPa,3个方向抗拉强度的极差随锻造温度的降低而减小;TA15钛合金锻造后的拉伸断口均为韧性断口,锻造温度越低,初生αp相含量越高,断口韧窝越深,而含有较多较细长片层状α相时,断口韧窝较浅。
Abstract
TA15 titanium alloy bars were fored in (α+β) phase region, and the effect of three forging temperatures, namely tβ-15℃, tβ-30℃ and tβ-50℃ (tβ was β phase transition temperature), on the microstructure and tensile strength aeolotropy of the alloy was investigated. The results show that with the decrease of forging temperature, the content of primary αp phase in the TA15 titanium alloy increased while that of lamellar α phase decreased, and the thickness and aspect ratio of lamellar α phase decreased; therefore the tensile strength increased. After forging at Tβ-50℃, the tensile strength along the streamline direction of the TA15 titanium alloy reached 973 MPa. The tensile strength difference in three directions decreased with decreasing forging temperature. The tensile fracture of the forged TA15 titanium alloy was ductile fracture. The lower the forging temperature, the higher the content of primary αp phase, the deeper the dimples on fractures; when more slender lamellar α phases existed, the fracture dimples were shallower.
中图分类号 TG146.23 DOI 10.11973/jxgccl202207002
所属栏目 试验研究
基金项目 两机重大专项基础研究项目(J2019-Ⅶ-002)
收稿日期 2021/5/19
修改稿日期 2022/6/22
网络出版日期
作者单位点击查看
备注王哲(1987-),男,陕西咸阳人,高级工程师,博士通信作者:冉兴研究员
引用该论文: WANG Zhe,RAN Xing,LIU Chengcheng,WANG Xin. Influence of Forging Temperature on Microstructure and Tensile StrengthAeolotropy of TA15 Titanium Alloy[J]. Materials for mechancial engineering, 2022, 46(7): 6~10
王哲,冉兴,刘程程,王欣. 锻造温度对TA15钛合金显微组织及抗拉强度各向异性的影响[J]. 机械工程材料, 2022, 46(7): 6~10
共有人对该论文发表了看法,其中:
人认为该论文很差
人认为该论文较差
人认为该论文一般
人认为该论文较好
人认为该论文很好
参考文献
【1】BOYER R R, WELSCH G, COLLINGS E W. Materials properties hangbook:Titanium alloys[M].[S.l.]:AMS International, 1993.
【2】曹春晓.航空用钛合金的发展概况[J].航空科学技术,2005,16(4):3-6. CAO C X.General development situation of titanium alloys for aviation[J].Aeronautical Science and Technology,2005,16(4):3-6.
【3】朱知寿,王新南,商国强,等.新型高性能钛合金研究与应用[J].航空材料学报,2016,36(3):7-12. ZHU Z S,WANG X N,SHANG G Q,et al.Research and application of new type of high performance titanium alloy[J].Journal of Aeronautical Materials,2016,36(3):7-12.
【4】王哲,王新南,商国强,等.新型超高强韧钛合金热变形行为研究[J].稀有金属材料与工程,2018,47(3):810-815. WANG Z,WANG X N,SHANG G Q,et al.Hot deformation behavior of new high strength and toughness titanium alloy[J].Rare Metal Materials and Engineering,2018,47(3):810-815.
【5】FAN J K,KOU H C,LAI M J,et al.Characterization of hot deformation behavior of a new near beta titanium alloy:Ti-7333[J].Materials & Design,2013,49:945-952.
【6】WANG Z,WANG X N,ZHU Z S.Characterization of high-temperature deformation behavior and processing map of TB17 titanium alloy[J].Journal of Alloys and Compounds,2017,692:149-154.
【7】张旺峰,李兴无,马济民,等.组织类型对钛合金损伤容限性能的影响及电镜原位观察[J].航空材料学报,2006,26(3):313-314. ZHANG W F,LI X W,MA J M,et al.Effect of microstructure on damage tolerance properties and SEM in situ observation for titanium alloy[J].Journal of Aeronautical Materials,2006,26(3):313-314.
【8】JI Z,YANG H,LI H W.Evolution of two types of α plates in tri-modal microstructure of TA15 alloy under varying processing conditions[J].Rare Metal Materials and Engineering,2015,44(3):527-531.
【9】WU C B,YANG H,FAN X G,et al.Dynamic globularization kinetics during hot working of TA15 titanium alloy with colony microstructure[J].Transactions of Nonferrous Metals Society of China,2011,21(9):1963-1969.
【10】张旺峰,曹春晓,李兴无,等.钛合金断裂韧性与屈强差的关系初探[J].稀有金属材料与工程,2005,34(4):549-551. ZHANG W F,CAO C X,LI X W,et al.Relationship between fracture toughness and proof-ultimate strength difference of Ti alloy[J].Rare Metal Materials and Engineering,2005,34(4):549-551.
【11】王哲,王新南,祝力伟,等.TB17钛合金β相区晶粒长大行为[J].钛工业进展,2016,33(6):11-15. WANG Z,WANG X N,ZHU L W,et al.Grain growth behavior in β single phase of TB17 titanium alloy[J].Titanium Industry Progress,2016,33(6):11-15.
【12】吴欢,赵永庆,葛鹏,等.β稳定元素对钛合金α相强化行为的影响[J].稀有金属材料与工程,2012,41(5):805-810. WU H,ZHAO Y Q,GE P,et al.Effect of β stabilizing elements on the strengthening behavior of titanium α phase[J].Rare Metal Materials and Engineering,2012,41(5):805-810.
【13】AHMED T,RACK H J.Phase transformations during cooling in α+β titanium alloys[J].Materials Science and Engineering:A,1998,243(1/2):206-211.
【14】沙爱学,李兴无,王庆如,等.热变形温度对TC18钛合金显微组织和力学性能的影响[J].中国有色金属学报,2005,15(8):1167-1172. SHA A X,LI X W,WANG Q R,et al.Influence of hot deformation temperature on microstructure and mechanical properties of TC18 alloy[J].The Chinese Journal of Nonferrous Metals,2005,15(8):1167-1172.
【15】郭萍,赵永庆,曾卫东,等.两相区热处理对TC4-DT钛合金断裂韧性的影响[J].稀有金属材料与工程,2018,47(4):1221-1225. GUO P,ZHAO Y Q,ZENG W D,et al.Effect of heat treatment in α+β zone on fracture toughness of TC4-DT titanium alloy[J].Rare Metal Materials and Engineering,2018,47(4):1221-1225.
【16】蔡建明,许超, 郝孟一,等. SP700和Ti-6Al-4V钛合金细晶组织的疲劳裂纹扩展特征[J].航空材料学报,2006,26(3):71-74. CAI J M, XU C, HAO M Y, et al. Fatigue crack growth characteristics of SP700 and Ti-6Al-4V titanium alloys[J].Journal of Aeronautical Materials,2006,26(3):71-74.
【17】孟笑影,庞克昌,殷俊林.热处理工艺对TC18钛合金组织和性能的影响[J].热处理,2006,21(1):36-39. MENG X Y,PANG K C,YIN J L.Effect of heat treatment process on structure and property of TC18 titanium alloy[J].Heat Treatment,2006,21(1):36-39.
【2】曹春晓.航空用钛合金的发展概况[J].航空科学技术,2005,16(4):3-6. CAO C X.General development situation of titanium alloys for aviation[J].Aeronautical Science and Technology,2005,16(4):3-6.
【3】朱知寿,王新南,商国强,等.新型高性能钛合金研究与应用[J].航空材料学报,2016,36(3):7-12. ZHU Z S,WANG X N,SHANG G Q,et al.Research and application of new type of high performance titanium alloy[J].Journal of Aeronautical Materials,2016,36(3):7-12.
【4】王哲,王新南,商国强,等.新型超高强韧钛合金热变形行为研究[J].稀有金属材料与工程,2018,47(3):810-815. WANG Z,WANG X N,SHANG G Q,et al.Hot deformation behavior of new high strength and toughness titanium alloy[J].Rare Metal Materials and Engineering,2018,47(3):810-815.
【5】FAN J K,KOU H C,LAI M J,et al.Characterization of hot deformation behavior of a new near beta titanium alloy:Ti-7333[J].Materials & Design,2013,49:945-952.
【6】WANG Z,WANG X N,ZHU Z S.Characterization of high-temperature deformation behavior and processing map of TB17 titanium alloy[J].Journal of Alloys and Compounds,2017,692:149-154.
【7】张旺峰,李兴无,马济民,等.组织类型对钛合金损伤容限性能的影响及电镜原位观察[J].航空材料学报,2006,26(3):313-314. ZHANG W F,LI X W,MA J M,et al.Effect of microstructure on damage tolerance properties and SEM in situ observation for titanium alloy[J].Journal of Aeronautical Materials,2006,26(3):313-314.
【8】JI Z,YANG H,LI H W.Evolution of two types of α plates in tri-modal microstructure of TA15 alloy under varying processing conditions[J].Rare Metal Materials and Engineering,2015,44(3):527-531.
【9】WU C B,YANG H,FAN X G,et al.Dynamic globularization kinetics during hot working of TA15 titanium alloy with colony microstructure[J].Transactions of Nonferrous Metals Society of China,2011,21(9):1963-1969.
【10】张旺峰,曹春晓,李兴无,等.钛合金断裂韧性与屈强差的关系初探[J].稀有金属材料与工程,2005,34(4):549-551. ZHANG W F,CAO C X,LI X W,et al.Relationship between fracture toughness and proof-ultimate strength difference of Ti alloy[J].Rare Metal Materials and Engineering,2005,34(4):549-551.
【11】王哲,王新南,祝力伟,等.TB17钛合金β相区晶粒长大行为[J].钛工业进展,2016,33(6):11-15. WANG Z,WANG X N,ZHU L W,et al.Grain growth behavior in β single phase of TB17 titanium alloy[J].Titanium Industry Progress,2016,33(6):11-15.
【12】吴欢,赵永庆,葛鹏,等.β稳定元素对钛合金α相强化行为的影响[J].稀有金属材料与工程,2012,41(5):805-810. WU H,ZHAO Y Q,GE P,et al.Effect of β stabilizing elements on the strengthening behavior of titanium α phase[J].Rare Metal Materials and Engineering,2012,41(5):805-810.
【13】AHMED T,RACK H J.Phase transformations during cooling in α+β titanium alloys[J].Materials Science and Engineering:A,1998,243(1/2):206-211.
【14】沙爱学,李兴无,王庆如,等.热变形温度对TC18钛合金显微组织和力学性能的影响[J].中国有色金属学报,2005,15(8):1167-1172. SHA A X,LI X W,WANG Q R,et al.Influence of hot deformation temperature on microstructure and mechanical properties of TC18 alloy[J].The Chinese Journal of Nonferrous Metals,2005,15(8):1167-1172.
【15】郭萍,赵永庆,曾卫东,等.两相区热处理对TC4-DT钛合金断裂韧性的影响[J].稀有金属材料与工程,2018,47(4):1221-1225. GUO P,ZHAO Y Q,ZENG W D,et al.Effect of heat treatment in α+β zone on fracture toughness of TC4-DT titanium alloy[J].Rare Metal Materials and Engineering,2018,47(4):1221-1225.
【16】蔡建明,许超, 郝孟一,等. SP700和Ti-6Al-4V钛合金细晶组织的疲劳裂纹扩展特征[J].航空材料学报,2006,26(3):71-74. CAI J M, XU C, HAO M Y, et al. Fatigue crack growth characteristics of SP700 and Ti-6Al-4V titanium alloys[J].Journal of Aeronautical Materials,2006,26(3):71-74.
【17】孟笑影,庞克昌,殷俊林.热处理工艺对TC18钛合金组织和性能的影响[J].热处理,2006,21(1):36-39. MENG X Y,PANG K C,YIN J L.Effect of heat treatment process on structure and property of TC18 titanium alloy[J].Heat Treatment,2006,21(1):36-39.
相关信息