Wei Yan, Dai Hua, Chen Li, Wang Xian, Cai Hongzhong, Zhang Jiankang, Xu Ying, Wang Xingqiang, Guo Junmei, Yuan Zhentao, Wang Xiao
Yunnan Precious Metals Laboratory Co., Ltd., Kunming 650106, China.
Kunming Institute of Precious Metals, Kunming 650106, China.
Molecules. 2024 Sep 3;29(17):4171. doi: 10.3390/molecules29174171.
To meet the demands for high-temperature performance and lightweight materials in aerospace engineering, the Au-Ni solder is often utilized for joining dissimilar materials, such as TiAl-based alloys and Ni-based high-temperature alloys. However, the interaction between Ti and Ni can lead to the formation of brittle phases, like TiNi, TiNi, and TiNi, which diminish the mechanical properties of the joint and increase the risk of crack formation during the welding process. Cu doping has been shown to enhance the mechanical properties and high-temperature stability of the Au-Ni brazed joint's central area. Due to the difficulty in accurately controlling the solid solution content of Cu in the Au-Ni alloy, along with the high cost of Au, traditional experimental trial-and-error methods are insufficient for the development of Au-based solders. In this study, first principles calculations based on density functional theory were employed to analyze the effect of Cu content on the stability of the Au-2.0Ni-xCu (x = 0, 0.25, 0.5, 0.75, 1.0, 1.25 wt%) alloy phase structure. The thermal properties of the alloy were determined using Gibbs software fitting. The results indicate that the Au-2.0Ni-0.25Cu alloy exhibits the highest plastic toughness (B/G = 5.601, ν = 0.416, Cauchy pressure = 73.676 GPa) and a hardness of 1.17 GPa, which is 80% higher than that of Au-2.0Ni. This alloy balances excellent strength and plastic toughness, meeting the mechanical performance requirements of brazed joints. The constant pressure specific heat capacity (C) of the Au-2.0Ni-xCu alloy is higher than that of Au-2.0Ni and increases with Cu content. At 1000 K, the C of the Au-2.0Ni-0.25Cu alloy is 35.606 J·mol·K, which is 5.88% higher than that of Au-2.0Ni. The higher C contributes to enhanced high-temperature stability. Moreover, the linear expansion coefficient (CTE) of the Au-2.0Ni-0.25Cu alloy at 1000 K is 8.76 × 10·K, only 0.68% higher than Au-2.0Ni. The lower CTE helps to reduce the risk of solder damage caused by thermal stress. Therefore, the Au-2.0Ni-0.25Cu alloy is more suitable for brazing applications in high-temperature environments due to its excellent mechanical properties and thermal stability. This study provides a theoretical basis for the performance optimization and engineering application of the Au-2.0Ni-xCu alloy as a gold-based solder.
为满足航空航天工程对高温性能和轻质材料的需求,金镍焊料常被用于连接异种材料,如钛铝基合金和镍基高温合金。然而,钛和镍之间的相互作用会导致脆性相的形成,如TiNi、TiNi和TiNi,这会降低接头的机械性能,并增加焊接过程中裂纹形成的风险。已表明铜掺杂可提高金镍钎焊接头中心区域的机械性能和高温稳定性。由于难以精确控制金镍合金中铜的固溶体含量,以及金的成本较高,传统的实验试错方法不足以开发金基焊料。在本研究中,采用基于密度泛函理论的第一性原理计算来分析铜含量对Au-2.0Ni-xCu(x = 0, 0.25, 0.5, 0.75, 1.0, 1.25 wt%)合金相结构稳定性的影响。使用吉布斯软件拟合确定合金的热性能。结果表明,Au-2.0Ni-0.25Cu合金具有最高的塑性韧性(B/G = 5.601,ν = 0.416,柯西压力 = 73.676 GPa)和1.17 GPa 的硬度,比Au-2.0Ni高80%。该合金平衡了优异的强度和塑性韧性,满足钎焊接头的机械性能要求。Au-2.0Ni-xCu合金的定压比热容(C)高于Au-2.0Ni,并随铜含量增加。在1000 K时,Au-2.0Ni-0.25Cu合金的C为35.606 J·mol·K,比Au-2.0Ni高5.88%。较高的C有助于提高高温稳定性。此外,Au-2.0Ni-0.25Cu合金在1000 K时的线性膨胀系数(CTE)为8.76×10·K,仅比Au-2.0Ni高0.68%。较低的CTE有助于降低热应力导致焊料损坏的风险。因此,Au-2.0Ni-0.25Cu合金因其优异的机械性能和热稳定性更适合在高温环境下的钎焊应用。本研究为Au-2.0Ni-xCu合金作为金基焊料的性能优化和工程应用提供了理论依据。