热处理工艺对Al0.1CoCrFeNiV0.4高熵合金组织与力学性能的影响

    Effects of Heat Treatment on Microstructure and Mechanical Properties of Al0.1CoCrFeNiV0.4 High-entropy Alloy

    • 摘要: 采用电弧熔炼法制备Al0.1CoCrFeNiV0.4合金,利用XRD、SEM、维氏硬度和拉伸试验对铸态和不同热处理后的合金进行检测。研究发现,合金的铸态样品为结构均匀且单一的FCC相固溶体。热处理使得合金发生了相变,在800℃及以上温度,合金中的一部分FCC相基体转变为BCC相结构。随着热处理时长的增加,合金中先后出现BCC相的析出和消失。合金的硬度和拉伸与压缩屈服强度随热处理温度和热处理时长的增加大体呈出先上升后下降的趋势,与BCC相的含量变化趋势大致相同。随热处理温度和热处理时长的增加,合金的拉伸断口形貌由韧性韧窝断裂先转变为韧性与脆性断裂相结合,再转变为韧性断裂。合金在900℃~6 h热处理后具有最大的屈服强度、拉伸极限强度、应变硬化率、较高的硬度和低应变下最高的压缩应变硬化率,因此,900℃~6 h为该合金最佳的热处理工艺。

       

      Abstract: Al0.1CoCrFeNiV0.4 alloy was prepared by arc melting and subsequently examined in its as-cast state and after different heat treatments by using XRD, SEM, Vickers hardness, and tensile tests. It is found that the cast sample of the alloy is a structural homogeneity and single FCC phase solid solution. The application of heat treatment results in a phase transformation of the alloy. At temperatures exceeding 800 ℃, a portion of the FCC phase matrix undergo a structural change to a BCC phase structure. As the duration of the heat treatment is extended, the precipitation and subsequent disappearance of the BCC phase occurs in a successive manner within the alloy. The hardness, tensile yield strength, and compressive yield strength of the alloys demonstrate a general trend of initial increase followed by subsequent decrease with theincrease of heat treatment temperature and duration. This trend is approximately parallel to that of the content of the BCC phase. The tensile fracture morphology of the alloy exhibits a transition from toughness to brittle fracture and subsequently to ductile fracture with an increase in heat treatment temperature and duration. The alloy exhibits the highest yield strength,tensile ultimate strength, strain hardening rate, hardness, and compressive strain hardening rate at low strain following heat treatment at 900 ℃-6 h. Therefore, 900 ℃-6 h is the optimal heat treatment process for this alloy.

       

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