欢迎登录材料期刊网

材料期刊网

高级检索

对粗片层状TA15钛合金在Thermecmaster-Z型热模拟试验机上进行等温恒应变速率压缩试验,采用基于Murty判据的加工图技术研究了该合金在温度1 000~1 100℃、应变速率0.001~10 s-1参数范围内的微观变形机制,并优化出该合金的锻造工艺参数.结果表明:在β单相区变形时,TA15钛合金较佳的变形参数范围为1 030~1 075℃、0.001~0.03 s-1,以1 050℃、0.001 s-1附近为最佳,其变形机制为β晶粒充分均匀的动态再结晶;失稳区变形参数范围为1 000~1 100℃、1.78~10 s-1,在该区出现了β晶粒的不均匀变形.

Hot compression tests of TA15 titanium alloy with coarse lamellar microstructure were conducted using Thermecmastor-Z hot working simulator. Microstructural deformation mechanisms were investigated by means of processing map technology based on Murty criterion in the temperature range of 1 000-1 100 ℃ and strain rate range of 0. 001-10 s-1, and the forging thermal parameters were optimized. The results show that in β phase field the desired deformation regions were in the range of 1 030- 1 075 ℃ and 0.001- 0.03 s-1 with the deformation mechanism of full and uniform dynamic recrystallization, and the optimum deformation parameters were at 1 050 ℃ and 0.001 s-1. The regions of flow instability occurred in the temperature range of 1 000- 1 100 ℃ and strain rate range of 1.78-10 s-1, and non-uniform deformation of β grains appeared in this range.

参考文献

[1] 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.
[2] 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.
[3] 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.
[4] 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.
[5] 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.
[6] Murty S.V. S. N.;Rao B.N. .Instability criteria for hot deformation of materials[J].International Materials Reviews,2000(1):15-26.
[7] 鲍如强,黄旭,曹春晓,柯俊.加工图在钛合金中的应用[J].材料导报,2004(07):26-29.
[8] Murty SVSN.;Rao BN. .On the development of instability criteria during hotworking with reference to IN 718[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1998(1/2):76-82.
[9] S. V. S. Narayana Murty;B. Nageswara Rao;B. P. Kashyap .On the hot working characteristics of 6061 Al-SiC and 6061-Al_2O_3 particulate reinforced metal matrix composites[J].Composites science and technology,2003(1):119-135.
[10] Long M.;Rack HJ. .THERMO-MECHANICAL STABILITY OF FORGED TI-26AL-10NB-3V-1MO(AT.PERCENT)[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,1995(1):99-111.
[11] T. Seshacharyulu;S. C. Medeiros;W. G. Frazier;Y. V. R. K. Prasad .Hot working of commercial Ti-6Al-4V with an equiaxed α-β microstructure: materials modeling considerations[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,2000(1/2):184-194.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%