欢迎登录材料期刊网

材料期刊网

高级检索

在变形温度为750~950℃、应变速率为0.1~0.001 s-1下进行Ti2AlNb 合金高温拉伸试验,研究了温度和应变速率对其抗拉强度和伸长率的影响,建立了高温变形条件下的应力-应变本构模型.结果表明:Ti2AlNb 合金是温度和应变速率敏感性材料,随着温度的升高或应变速率的降低,合金的抗拉强度下降,伸长率升高;通过修正 Hooke 定律和 Grosman 方程所建立的Ti2AlNb 合金热成形本构方程,其计算得到的流变曲线和试验曲线较吻合,可用于表征 Ti2AlNb合金的高温变形行为.

High temperature tensile test of Ti2AlNb alloy was carried out at different temperatures between 750 and 950 ℃ and at different strain rates between 0.1 and 0.001 s-1 .The influences of temperature and strain rate on the tensile strength and percentage elongation of the alloy were also studied, and then the stress-strain constitutive model of the alloy under the condition of high temperature deformation was established.The results show that the Ti2AlNb alloy was a kind of temperature sensitive and strain rate sensitive material.With the increase of the deformation temperature or decrease of the stain rate,the tensile strength of the alloy decreased and percentage elongation increased.The heat forming constitutive model of Ti2AlNb alloy was established based on the modified Hooke′s law and Grosman correction equation.The calculated flow curve of the model matched the experimental curve well,indicating that the constitutive model can be used to characterize the deformation behavior of the alloy.

参考文献

[1] 张宏建;温卫东;崔海涛.TiAl金属间化合物材料本构模型的研究进展[J].机械工程材料,2013(7):1-5,63.
[2] 李梁;孙健科;孟祥军.钛合金的应用现状及发展前景[J].钛工业进展,2004(5):19-24.
[3] 司玉锋;陈子勇;孟丽华;王肇文;陈玉勇.Ti3Al基金属间化合物的研究进展[J].特种铸造及有色合金,2003(4):33-35.
[4] 司玉锋;孟丽华;陈玉勇.Ti2AlNb基合金的研究进展[J].宇航材料工艺,2006(3):10-13,25.
[5] 冯艾寒;李渤渤;沈军.Ti2AlNb基合金的研究进展[J].材料与冶金学报,2011(1):30-38.
[6] 沈军;冯艾寒.Ti2AlNb基合金微观组织调制及热成形研究进展[J].金属学报,2013(11):1286-1294.
[7] Rae CMF;Hook MS;Reed RC.The effect of TCP morphology on the development of aluminide coated superalloys[J].Materials Science & Engineering, A. Structural Materials: Properties, Misrostructure and Processing,20051/2(1/2):231-239.
[8] 李少雨 .Ti2AlNb基合金相变及超塑性变形机理研究[D].哈尔滨工业大学,2013.
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%