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利用热模拟试验机研究了GH710合金在变形温度为1110~1150℃,应变速率为0.01~1s^-1条件下的高温变形特性及变形后的组织特征。结果表明:在1150℃以下热变形时合金发生了亚固溶态的再结晶,且γ相在1130℃时已部分回溶;通过Arrhenius双曲正弦函数模型构建了合金的本构关系,得到了合金热变形激活能为693.46kJ·mol^-1;合金动态再结晶临界应变随着应变速率的增大及变形温度的降低而增加,且临界应变和峰值应变之间满足εc=0.61s;合金热加工过程中的软化机制为动态再结晶,根据热变形后的组织特征确定合金合理的热变形温度范围为1110~1130℃,应变速率为0.01S。

The hot deformation and microstructure characteristics of GH710 alloy were investigated by thermal simulated test at the strain rates of 0. 01--1 s 1 and temperatures of 1 ll0--1 150 ℃. The results show that metastable solid solution stare recrystallization occurred below 1 150 ℃, and phase partly dissolved into the matrix at 1 130 ℃. A hyperbolic sine function of Arrhenius was used to describe the constitutive relation for GH710 alloy with good fit accuracy, giving the hot deformation activation energy of 693.46 kJ ~ mo1-1, The critical strain of dynamic recrystalliztion, which met a linear relationship with peak strain as ec =0. 61~p, increased with increasing the strain rate and decreasing the deformation temperature. The soften mechanism of GHT10 alloy was dynamic recrystallization during hot working process. According to the microstructure after hot deformation, it was proposed for GH710 alloy that proper deformation temperature range was 1 110-1 130 ℃ and proper strain rate was 0. 01 s-1.

参考文献

[1] 田世藩,张国庆,李周,颜鸣皋.先进航空发动机涡轮盘合金及涡轮盘制造[J].航空材料学报,2003(z1):233-238.
[2] 王淑云,李惠曲,杨洪涛.等温锻造GH710合金组织与性能[J].锻压技术,2007(04):29-32.
[3] G. Gottstein;E. Brunger;M. Frommert;M. Goerdeler;M. Zeng .Prediction of the critical conditions for dynamic recrystallization in metals[J].Zeitschrift fur Metallkunde,2003(5):628-635.
[4] E. I. POLIAK;J. J. JONAS .Critical Strain for Dynamic Recrystallization in Variable Strain Rate Hot Deformation[J].ISIJ International,2003(5):692-700.
[5] Abbas NAJAFIZADEH;John J. JONAS .Predicting the Critical Stress for Initiation of Dynamic Recrystallization[J].ISIJ International,2006(11):1679-1684.
[6] 李文斌,潘清林,梁文杰,何运斌,刘俊生,李运春.含Sc超高强Al-Zn-Cu-Mg-Sc-Zr合金的热压缩变形流变应力[J].中国有色金属学报,2008(05):777-782.
[7] Shi H;McLaren AJ;Sellars CM;Shahani R;Bolingbroke R .Constitutive equations for high temperature flow stress of aluminium alloys[J].Materials Science and Technology: MST: A publication of the Institute of Metals,1997(3):210-216.
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