用户名: 密码: 验证码:
TB17钛合金高温压缩变形行为
详细信息    查看全文 | 推荐本文 |
  • 英文篇名:High temperature compression deformation behavior of TB17 titanium alloy
  • 作者:朱鸿昌 ; 罗军明 ; 朱知寿
  • 英文作者:ZHU Hongchang;LUO Junming;ZHU Zhishou;School of Materials Science and Engineering,Nanchang Hangkong University;Aviation Key Laboratory of Science and Technology on Advanced Titanium Alloys,AECC Beijing Institute of Aeronautical Materials;
  • 关键词:TB17钛合金 ; 热变形 ; 连续动态再结晶 ; 不连续动态再结晶 ; Arrhenious本构方程
  • 英文关键词:TB17 titanium alloy;;thermal deformation;;continuous dynamic recrystallization;;discontinuous dynamic recrystallization;;constitutive equations
  • 中文刊名:HKCB
  • 英文刊名:Journal of Aeronautical Materials
  • 机构:南昌航空大学材料科学与工程学院;中国航发北京航空材料研究院先进钛合金航空科技重点实验室;
  • 出版日期:2019-06-01
  • 出版单位:航空材料学报
  • 年:2019
  • 期:v.39
  • 基金:国家自然科学基金项目(5176401)
  • 语种:中文;
  • 页:HKCB201903006
  • 页数:9
  • CN:03
  • ISSN:11-3159/V
  • 分类号:48-56
摘要
通过Gleeble 3800热模拟试验机对TB17钛合金在变形温度860~980℃、应变速率为0.001~1 s~(-1)、最大变形量为70%下高温变形行为进行研究。通过材料参数与真应变之间的关系,利用Arrhenious本构方程关系式和Z参数建立流变应力和变形温度、应变速率和真应变三者之间的本构关系,并对组织进行分析。结果表明:TB17钛合金在应变速率为0.001~0.01 s~(-1)、变形温度为890~980℃下更容易发生连续动态再结晶,而在应变速率为0.1~1 s~(-1)下主要发生不连续动态再结晶;误差分析结果显示计算值与实测值平均相对误差为6%,说明建立的本构关系模型具有较高的准确度。
        The high temperature hot deformation behavior of TB17 titanium alloy was studied using Gleeble-3800 thermocompression simulation tester at the temperature of 860-980 ℃,strain rate of 0.001-1 s~(-1) and the deformation degree of 0.7.The deformation behavior and microstructure were studied.By building the relationship between material parameters and true strain,the relationship between flow stress and deformation temperature,strain rate and strain was established by using Arrhenious constitutive equation and Z parameter.The results show that TB17 titanium alloy is more likely to happen continuous dynamic recrystallization at strain rate of 0.001-0.01 s~(-1) and deformation temperature of 890-980 ℃,while discontinuous dynamic recrystallization occur mainly at high strain rate(≥ 0.1 s~(-1)).The error analysis shows that the average relative error between calculated and measured values is 6%.It indicates that the constitutive relation model has higher accuracy.
引文
[1]朱知寿.我国航空用钛合金技术研究现状及发展[J].航空材料学报,2014,34(4):44-50.(ZHU Z S.Recent research and development of titanium alloys for aviation application in china[J].Journal of Aeronautical Materials,2014,34(4):44-50.)
    [2]曹春晓.钛合金在大型运输机上的应用[J].稀有金属快报,2006,25(1):17-21.(CAO C X.Application of titanium alloys on lager transporter[J].Rare Metals Letters,2006,25(1):17-21.)
    [3]商国强,朱知寿,常辉,等.超高强度钛合金研究进展[J].稀有金属,2011(2):286-291.(SHANG G Q,ZHU Z S,CHANG H,et al.Development of ultra-high strength titanium alloy[J].Chinese Journal of Rare Metals,2011(2):286-291.)
    [4]金和喜,魏克湘,李建明,等.航空用钛合金研究进展[J].中国有色金属学报,2015,25(2):280-292.(JIN H X,WEI K X,LI J M,et al.Research development of titanium alloy in aerospace industry[J].The Chinese Journal of Nonferrous Metals,2015,25(2):280-292.)
    [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]HUA K,XUE X,KOU H,et al.Characterization of hot deformation microstructure of a near beta titanium alloy Ti-5553[J].Journal of Alloys&Compounds,2014,615:531-537.
    [7]ZHU Y,ZENG W,FENG F,et al.Characterization of hot deformation behavior of as-cast TC21 titanium alloy using processing map[J].Materials Science&Engineering:A,2011,528(3):1757-1763.
    [8]LIU S F,LI M Q,LUO J,et al.Deformation behavior in the isothermal compression of Ti-5Al-5Mo-5V-1Cr-1Fe alloy[J].Materials Science&Engineering:A,2014,589(1):15-22.
    [9]东赟鹏,于秋颖,方爽,等.TA7钛合金高温流变行为研究[J].航空材料学报,2015,35(1):13-19.(DONG Y P,YU Q Y,FANG S,et al.Plastic deformation behavior of TA7 titanium alloy[J].Journal of Aeronautical Materials,2015,35(1):13-19.)
    [10]袁武华,卢政,齐占福,等.TA15钛合金热变形本构方程及热加工图[J].热加工工艺,2017(17):33-37.(YUAN W H,LU Z,QI Z F,et al.Constitutive equation and hot processing map for hot deformation of TA15 titanium alloy[J].Hot Working Technology,2017(17):33-37.)
    [11]杨建辉,张鹏,赵升吨.TC4-DT钛合金热变形本构方程[J].塑性工程学报,2016,23(2):120-125.(YANG J H,ZHANG P,ZHAO S D.Hot deformation constitutive equation of TC4-DT titanium alloy[J].Journal of Plasticity Engineering,2016,23(2):120-125.)
    [12]陈海生,冯勇,马凡蛟,等.基于BP网络Ti-6Al-3Nb-2Zr-1Mo合金等温压缩流变应力预测[J].稀有金属材料与工程,2016,45(6):1549-1553.(CHEN H S,FENG Y,MA F J,et al.Isothermal compression flow stress prediction of Ti-6Al-3Nb-2Zr-1Mo alloy base on BP-ANN[J].Rare Metal Material and Engineering,2016,45(6):1549-1553.)
    [13]邱伟,鲁世强,欧阳德来,等.锻态TB6钛合金热变形行为及组织演变[J].塑性工程学报,2010,17(3):38-43.(QIU W,LU S Q,OUYANG D L,et al.Investigation on the hot temperature deformation behavior and microstructure evolution of forged titanium alloy TB6[J].Journal of Plasticity Engineering,2010,17(3):38-43.)
    [14]NIE X A,HU Z,LIU H Q,et al.High temperature deformation and creep behavior of Ti-5Al-5Mo-5V-1Fe-1Cr alloy[J].Materials Science&Engineering:A,2014,613:306-316.
    [15]PHILIPPART I,RACK H J.High temperature dynamic yielding in metastable Ti-6.8Mo-4.5F-1.5Al[J].Materials Science&Engineering:A,1998,243(1/2):196-200.
    [16]MATSUMOTO H,KITAMURA M,LI Y,et al.Hot forging characteristic of Ti-5Al-5V-5Mo-3Cr alloy with single metastableβmicrostructure[J].Materials Science&Engineering:A,2014,611:337-344.
    [17]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.Study on hot deformation behavior of new high strength and toughness titanium alloy[J].Rare Metal Materials and Engineering,2018,47(3):810-815.)
    [18]周盛武,董洪波,姜智勇,等.TB17钛合金热压缩流变应力分析及本构方程[J].塑性工程学报,2018,25(1):218-223.(ZHOU S W,DONG H B,JIANG Z Y,et al.Flow stress analysis and constitutive equation of TB17 titanium alloy during hot compression[J].Journal of Plasticity Engineering,2018,25(1):218-223.)
    [19]欧阳德来,鲁世强,崔霞,等.不同应变速率下TA15钛合金β形变过程中动态再结晶行为[J].稀有金属材料与工程,2011,40(2):325-330.(OUYANG D L,LU S Q,CUI X,et al.Dynamic recrystallization of titanium alloy TA15 duringβhot process at different strain rates[J].Rare Metal Materials and Engineering,2011,40(2):325-330.)
    [20]孙坤,王富耻,程兴旺,等.TC6钛合金不同组织绝热剪切带的形成机理[J].稀有金属材料与工程,2009,38(1):34-37.(SUN K,WANG F C,CHENG X W,et al.Formation mechanics of adiabatic shear band for the different microstructures of TC6 alloy[J].Rare Metal Materials and Engineering,2009,38(1):34-37.)
    [21]ZHAO J,DING H,ZHAO W,et al.Modelling of the hot deformation behaviour of a titanium alloy using constitutive equations and artificial neural network[J].Computational Materials Science,2014,92(5):47-56.
    [22]ZENER C,HOLLOMON J H.Effect of strain rate upon plastic flow of steel[J].Journal of Applied Physics,1944,15(1):22-32.

© 2004-2018 中国地质图书馆版权所有 京ICP备05064691号 京公网安备11010802017129号

地址:北京市海淀区学院路29号 邮编:100083

电话:办公室:(+86 10)66554848;文献借阅、咨询服务、科技查新:66554700