Microstructure and Mechanical Properties of an Ultrahigh-strength Titanium alloy Ti-4.5Al-5Mo-5V-6Cr-1Nb Prepared Using Laser Directed Energy Deposition and Forging: A Comparative Study

Junwei Yang , Haibo Tang , Peiyuan Wei , Hongwei Gao , Jiawei Wang , Haixin Huo , Yanyan Zhu
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引用次数: 4

Abstract

The application of titanium alloys in aerospace put forward the requirement for higher strength. Additive manufacturing is a promising method for the efficient and economical processing of titanium alloys. However, research on the additive manufacturing of ultrahigh-strength titanium alloys is still limited. The mechanisms of microsegregation for high alloying elements and poor plasticity are still not clear. In this study, an ultrahigh-strength titanium alloy Ti–4.5Al–5Mo–5V–6Cr–1Nb (TB18) was prepared using two methods: laser direct energy deposition (LDED) and forging. The LDEDed alloy contains three zones with similar grain morphologies but different microstructure. The microsegregation of the alloy is limited due to the rapid solidification and almost eliminated after the thermal cycle and solution treatment. With stress relief treatment, the LDEDed alloy exhibits anisotropic mechanical properties. After solution and aging treatments, its ultimate strength is enhanced; however, its plasticity is relatively lower than that of the wrought alloy with equally high strength. The excellent balance of the strength and plasticity of the wrought alloy can be ascribed to the formation of αWGB and multiscale α laths, which provides enlightenment for optimizing the properties of the LDEDed alloy.

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激光定向能沉积与锻造制备超高强度钛合金Ti-4.5Al-5Mo-5V-6Cr-1Nb的组织与力学性能对比研究
钛合金在航空航天领域的应用对其强度提出了更高的要求。增材制造是一种高效、经济地加工钛合金的有前途的方法。然而,对超高强度钛合金增材制造的研究仍然有限。合金元素含量高、塑性差的微观偏析机制尚不清楚。本研究采用激光直接能量沉积(LDED)和锻造两种方法制备了超高强度钛合金Ti–4.5Al–5Mo–5V–6Cr–1Nb(TB18)。LDED合金包含三个具有相似晶粒形态但不同微观结构的区域。合金的微偏析由于快速凝固而受到限制,并且在热循环和固溶处理后几乎消除。经过应力消除处理后,LDED合金表现出各向异性的力学性能。经过固溶和时效处理后,其极限强度得到增强;然而,其塑性相对低于具有同样高强度的锻造合金。变形合金的强度和塑性之间的良好平衡可归因于αWGB和多尺度α板条的形成,这为优化LDED合金的性能提供了启示。
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