Ti-Al-Mo-V-Cr-Nb系高强钛合金热变形行为及组织演变规律

    Hot Deformation Behavior and Microstructure Evolution of Ti-Al-Mo-V-Cr-Nb High Strength Titanium Alloy

    • 摘要: 采用Gleeble-3800型热模拟实验机对Ti-Al-Mo-V-Cr-Nb钛合金在不同温度、应变速率和一定变形量下进行高温热压缩实验,实验条件:变形温度为760~840℃、应变速率为0.001~1 s-1、最大变形量为60%。根据Ti-Al-Mo-V-Cr-Nb钛合金在不同温度和应变速率下的真应力-真应变曲线,分析流动应力和微观组织随变形温度、应变速率的演变规律。结果表明,流动应力随着应变速率的降低和变形温度的升高而下降;在真应变为0.9的实验条件下,钛合金的热变形激活能为218.15 kJ/mol;利用参数Z和Arrhenius双曲正弦方程建立了Ti-Al-Mo-V-Cr-Nb钛合金真应变为0.9时的热变形本构方程;对建立的本构方程进行验证,发现实验条件下构建出的Arrhenius型本构方程精度较高,可以作为钛合金的本构方程模型;Ti-Al-Mo-V-Cr-Nb钛合金的α相含量随变形温度的升高和应变速率的降低而下降。

       

      Abstract: Ti-Al-Mo-V-Cr-Nb titanium alloy was tested by a thermal-mechanical physical simulation system(Gleeble-3800) at different temperatures, strain rates and a certain amount of deformation. The isothermal compression was carried out in the deformation temperature range of 760 ℃-840 ℃, strain rate range of 0.001 s-1-1 s-1, and deformation degree of 60%. According to the true stress-true strain curves of Ti-Al-Mo-V-Cr-Nb titanium alloy at different temperatures and strain rates, the evolution of flow stress and microstructure with deformation temperatures, strain rates were analyzed. The results show that the flow stress decreases with the decrease of strain rate and the increases of deformation temperature. The deformation thermal activation energy of titanium alloy is 218.15 kJ/mol under the condition of true strain 0.9. Using parameter Z and Arrhenius type constitutive equation, the hot deformation constitutive equation of Ti-Al-Mo-V-Cr-Nb titanium alloy is established when the true strain is 0.9. The established constitutive equation is verified, and it is found that the Arrhenius type constitutive equation constructed under experimental conditions has high accuracy, and can be used as the constitutive equation model of titanium alloy. The α phase content of Ti-Al-Mo-V-Cr-Nb titanium alloy decreases with the increase of deformation temperatures and the decreases of strain rates.

       

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