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MicrostructureofTitaniumafterHydrogenationWangYu;WangPeixuan;ZhangJianwei(王宇)(王佩璇)(张建伟)UniversityofScienceandTechnologyBeijin... 相似文献
83.
Ming-Wei Lu Kun–Lin Lin Chien-Cheng Lin 《International Journal of Applied Ceramic Technology》2021,18(3):739-748
Various proportions of ZrO2/CaTiO3 powders were mixed and hot pressed at 1500°C/30 min for Ti casting. The hot-pressed ZrO2/CaTiO3 composites were reacted with pure Ti at 1700°C/10 min in Ar. The interfacial reaction between Ti and ZrO2/CaTiO3 composites was investigated through X-ray diffraction, scanning electron microscopy, transmission electron microscopy, and energy-dispersive X-ray spectroscopy. The ZrO2/CaTiO3 composites with less than 10 vol.%, CaTiO3, and a minor amount of residual TiO2 were found. When the content of ZrO2 was increased to larger than 10 vol.%, two Ca2Zr5Ti2O16 and CaZrTi2O7 phases appeared in the composites. The amount of CaTiO3 and CaZrTi2O7 in the composites gradually decreased as the amount of ZrO2 increased. When Ti came in contact with ZrO2/CaTiO3 composites with less than 10 vol.% ZrO2, the resulting eutectic reaction produced a liquid phase and induced melting. When ZrO2 was increased to more than 30 vol.% in the composites, Ca2Zr5Ti2O16 and CaZrTi2O7 changed completely to CaZrO3, Ti2O, CaO, and ZrO2. With more than 30 vol.% ZrO2, no other reaction phases occurred in the Ti side after contact with the ZrO2/CaTiO3 composites, which is conducive for producing ceramic composites for Ti casting applications. 相似文献
84.
The true stress--strain curves of TC16 alloy with a wide range of strain rates were investigated under uniaxial quasi-static tension and uniaxial dynamic compression with the lnstron 8032 test machine and the split Hopkinson bar respectively. The results indicate that the true stress increases with increasing strain rate, while decreases with increasing temperature. Under the 105 s^-1 high strain rate and temperature higher than 673 K, the true stress would even be less than that under quasi-static condition. A new method incorporating TCl6's stress strain curve developing item was proposed to determine the coefficients in J-C model easily and to avoid the estimation of the adiabatic temperature rising. The Johnson-Cook dynamic constitutive relationship for TC16 was obtained for the first time. Good agreement was obtained between the model prediction and the experimental stress--strain curves for TC16 under both quasi-static and dynamic loadings. 相似文献
85.
The effects of α and β phase interactions on the tensile and creep deformation behavior of β titanium alloys was studied using
Ti-6.0wt.% Mn and Ti-8.1wt.%V as the model two-phase alloys, and Ti-13.0wt.%Mn and Ti-14.8wt.%V as the single-phase β alloys.
The β phase of α-βTi-8.1V deforms by stress-induced hexagonal martensite (α′), while slip and twinning occurs in the single-phase
β alloy with the same chemistry as the β phase. No stress-induced martensite was observed in the β or α-βTi-Mn alloys. This
behavior is modeled in terms of a number of factors, including elastic interaction stresses between the α and β phases, coherency
between the α phase and hexagonal martensite, and β phase stability.
This paper was presented at the Beta Titanium Alloys of the 00’s Symposium sponsored by the Titanium Committee of TMS, held
during the 2005 TMS Annual Meeting & Exhibition, February 13–16, 2005 in San Francisco, CA. 相似文献
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88.
纯铝等径角挤技术(I)——显微组织演化 总被引:15,自引:4,他引:15
研究了纯铝在 3种 (A、B和C)不同等径角挤工艺中的显微组织演化。结果表明 :纯铝经过等径角挤压变形后 ,其显微组织特征与加工路线有很大的关系。提出了立方元素扭转模型 ,分析了 3种不同加工路线的剪切面和剪切方向 ,较好地解释了采用 3种不同路线挤压后材料显微组织的演化规律。在路线C(各道次挤压间试样旋转 180°)中 ,每次挤压样品总是在相同的剪切面上发生剪切 ,每相邻道次之间的剪切方向相反 ,前一次变形产生的剪切应变被随后紧接着的下一次挤压所抵消 ,这导致了多余的剪切应变 ;在路线A(各道次挤压间试样不旋转 )中 ,有两个相交成 6 0°的剪切面 ,剪切交替地在两个剪切面上进行 ;在路线B(各道次挤压间试样旋转 90°)中 ,存在 4个不同的剪切面和剪切方向 ,挤压交替地在 4个剪切面上进行 ,X ,Y和Z平面上的晶粒都发生了剪切 ,这有利于等轴晶结构的形成 相似文献
89.
热处理对Ti-Al-Sn-Zr-Mo-Si-X系合金性能的影响 总被引:2,自引:0,他引:2
研究了热处理对3种Ti-Al-Sn-zr-Mo-Si-X(X为ⅤB,ⅥB族一种或几种元素)系合金(A、B、C)室温拉伸性能的影响,对优化合金的热处理制度及优选热处理制度下3种合金的疲劳裂纹扩展行为也进行了探讨。结果表明,优选热处理制度下A、C合金的裂纹扩展速率差别不大,B合金560℃时效处理后,裂纹扩展速率比540℃时效处理的小。在相同热处理制度下,比较3种合金裂纹扩展速率的结果表明,IgΔK在1.2~1.5范围内B合金的抗疲劳裂纹扩展性能较优。 相似文献
90.