在变形温度700~860 ℃、应变速率0.001~1 s-1下,对TB6合金进行热压缩变形,以研究TB6合金的热压缩流变应力行为.研究温度、变形量、应变速率等因素对TB6热变形流变应力的影响,建立了TB6合金热变形流变应力的本构模型方程.结果表明:合金在热压缩过程中,流变应力随着应变的增大而增加,达到峰值应力后逐渐趋于平稳;应力峰值随着应变速率的增大而增大,随着温度的升高而呈减小趋势.
参考文献
[1] | 颜鸣皋 .钛合金在航空领域的应用与发展[J].航空科学技术,2007,2:1-5. |
[2] | 段庆文.钛在军事航空领域的战略地位[J].钛工业进展,2002(06):28-29. |
[3] | 钱九红.航空航天用新型钛合金的研究发展及应用[J].稀有金属,2000(03):218-223. |
[4] | 全宏声 .Beta钛合金在航空航天工业中的应用逐步扩大[J].材料工程,1994,10:35-40. |
[5] | 朱知寿,王新南,童路,曹春晓.中国航空结构用新型钛合金研究[J].钛工业进展,2007(06):28-32. |
[6] | BOYER R R .Design properties of a high-strength titanium alloy Ti-10V-2Fe-3Al[J].Journal of Metals,1980,132(03):61-65. |
[7] | RYDSTAL H;DUERIG T W;BOER C R .Hot-die forging of Ti-10V-2Fe-3Al[J].Journal of Metals,1979,169(07):641-646. |
[8] | BURKE J;MAHRABIAN R.Advances in metal processing[M].New York:Plenum Press,1981:133-134. |
[9] | Nengping Jin;Hui Zhang;Yi Han .Hot deformation behavior of 7150 aluminum alloy during compression at elevated temperature[J].Materials Characterization,2009(6):530-536. |
[10] | 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. |
[11] | 林高用,张辉,郭武超,彭大暑.7075铝合金热压缩变形流变应力[J].中国有色金属学报,2001(03):412-415. |
[12] | 蒙春标,张辉,吴文祥,李落星.3104铝合金高温热压缩变形流变行为研究[J].热加工工艺,2008(12):1-4. |
[13] | Yinghua Lin;Cunningham G.A. III .A new approach to fuzzy-neural system modeling[J].IEEE Transactions on Fuzzy Systems: A Publication of the IEEE Neural Networks Council,1995(2):190-198. |
[14] | JUANG C F;LIN C T .A on-line self-constructing neural fuzzy inference network for system modeling[J].IEEE Transactions on Systems Man and Cybernetics,1998,5(02):12-32. |
[15] | KIM J;KASABOV N .Adaptive neuro-fuzzy inference systems and their application to nonlinear dynamical systems[J].Neural Networks,1999,12:1301-1319. |
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