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High-temperature-tensile-deformatidn behavior of Ti-6Al-4V alloy with the acicular α' martensite microstructure

机译:具有针状α'马氏体微观结构的Ti-6Al-4V合金的高温 - 拉伸畸形行为

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Titanium alloys are widely used in aerospace components, with the most widely used alloy being (α+β)-type Ti-6Al-4V (hereafter designated as Ti-64) alloy owing to its high specific strength and high formability associated with superplasticity. This work examines the tensile deformation behavior of the Ti-64 alloy with the acicular α' martensite microstructure tested at from 700°C to 900°C. Higher tensile-elongation and higher strain-rate-sensitivity value are seen in the Ti-64 alloy with the a' martensite microstructure as compared to that with the lamellar (α+β) microstructure. During deformation of the α' martensite microstructure at 700°C or 800°C, acicular microstructure evolves into fine equiaxed (α+β) structure, whereas there is no apparent change in microstructure in the case of the lamellar (α+β) starting microstructure. This result indicates that dynamic globularization during deformation is strongly enhanced in the acicular a' martensite starting microstructure, thereby leading to higher tensile elongatioa
机译:钛合金广泛用于航空航天部件,由于其具有高比强度和高塑性的高成形性,具有最广泛使用的合金(α+β)型(α+β) - 型Ti-6Al-4V(以下称为Ti-64)合金。这项工作检测Ti-64合金的拉伸变形行为与在700℃至900℃下测试的针状α'马氏体微观结构。在Ti-64合金中,与具有层状(α+β)微结构相比,在Ti-64合金中可以在Ti-64合金中看到较高的拉伸伸长和较高的应变速率敏感值。在700℃或800℃下的α'马氏体微观结构的变形期间,针状微观结构演变成精细等式(α+β)结构,而在层状(α+β)的情况下,微观结构的显而易见的变化微观结构。该结果表明,在针状A'马氏体开始微观结构中,变形过程中的动态球形化强烈增强,从而导致更高的拉伸绵羊

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