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首页> 外文期刊>Metallurgical and Materials Transactions, A. Physical Metallurgy and Materials Science >Comparison of the Microstructure, Tensile, and Creep Behavior for Ti-24Al-17Nb-0.66Mo (Atomic Percent) and Ti-24Al-17Nb-2.3Mo (Atomic Percent) Alloys
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Comparison of the Microstructure, Tensile, and Creep Behavior for Ti-24Al-17Nb-0.66Mo (Atomic Percent) and Ti-24Al-17Nb-2.3Mo (Atomic Percent) Alloys

机译:Ti-24Al-17Nb-0.66Mo(原子百分比)和Ti-24Al-17Nb-2.3Mo(原子百分比)合金的组织,拉伸和蠕变行为的比较

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摘要

The effect of small molybdenum additions, 0.66 and 2.3 at. pct, on the microstructure, tensile, and creep behavior of a nominally Ti-24Al-17Nb (at. pct) alloy was investigated. The alloy containing 2.3 at. pct Mo contained higher body-centered-cubic (bcc) phase volume fractions, which was expected as Mo stabilizes the bcc phase. Constant load, tensile-creep experiments were performed in the stress range of 29 to 275 MPa and the temperature range of 650 deg C to 710 deg C, in both air and vacuum environments. In-situ creep experiments were performed inside a scanning electron microscope chamber in order to identify the deformation evolution from surface observations. From these experiments, it was evident that alpha_2 intergranular cracking was prevalent and initiated the fracture process where the crack path followed the alpha_2 grain boundaries. The Ti-24Al-17Nb-2.3Mo (at. pct) alloy exhibited significantly lower creep rates than the Ti-24Al-17Nb-0.66Mo (at. pct) alloy, and this was associated with less contiguity of the alpha_2 phase.
机译:少量钼的影响为0.66和2.3 at。 pct,研究了名义上的Ti-24Al-17Nb(at。pct)合金的微观结构,拉伸和蠕变行为。该合金含2.3 at。 pct Mo包含更高的体心立方(bcc)相体积分数,这是由于Mo可以稳定bcc相而预期的。在空气和真空环境中,均在29至275 MPa的应力范围和650℃至710℃的温度范围内进行了恒定载荷,拉伸蠕变实验。为了在表面观察中识别变形演变,在扫描电子显微镜室内进行了原位蠕变实验。从这些实验中,很明显,α_2晶间裂纹是普遍存在的,并开始了断裂过程,其中裂纹路径遵循α_2晶界。 Ti-24Al-17Nb-2.3Mo(at。pct)合金的蠕变速率显着低于Ti-24Al-17Nb-0.66Mo(at。pct)合金,并且这与alpha_2相的邻接度较低有关。

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