Li Gang, Meng Xiangran, Geng Chunpin, Wang Chongshuo, Ren Haifang, Guo Xiaoying, Li Sinan, Tao Ying
College of Mines, Liaoning Technical University, Fuxin 123000, China.
School of Materials Science and Engineering, Yingkou Institute of Technology, Yingkou 115000, China.
Materials (Basel). 2025 Feb 8;18(4):755. doi: 10.3390/ma18040755.
CoCrFeNi high-entropy alloys represent a novel structural material with considerable application potential in a variety of fields, including aerospace, automobiles, ships, machining, energy, soft magnetic materials, and hydrogen storage materials. The present study investigates the impact of the Al element on the structure and properties of the alloy. The preparation of the AlCrCoFeNi ( = 0.1, 0.2, 0.3, 0.4, 0.5) powders involved the use of a variety of elemental metal powders as raw materials and a mechanical alloying process at 350 rpm for 40 h. The sintering of the alloy powders was subsequently conducted using spark plasma sintering at 1000 °C. The microstructure of the alloys was analyzed using XRD, SEM, and EDS, and the properties were analyzed using a universal testing machine, a hardness measurement, friction and wear measurement, and an electrochemical workstation. The study shows that when = 0.1, the crystal structure of AlCrCoFeNi consists of a double FCC phase and a trace amount of σ phase. As the aluminum content increases, part of the FCC phase begins to transform to BCC. When = 0.2~0.5, the alloy consists of a double FCC phase and a BCC phase and a trace amount of a sigma phase. As the BCC phase in the alloy increases, the tensile strength of the alloy increases, the ability to deform plastically decreases, and the hardness increases. The highest ultimate tensile strength of 1163.14 MPa is exhibited by AlCrCoFeNi, while the minimum elongation is 26.98% and the maximum hardness value is 412.6 HV. In the initial stage of friction measurement, the wear mechanism of AlCrCoFeNi is adhesive wear. However, as the test time progresses, an oxide layer begins to form on the alloy's surface, leading to a gradual increase in the friction coefficient. At this stage, the wear mechanism becomes a combination of both adhesive and abrasive wear. Once the oxidation process and the wear process have reached a dynamic equilibrium, the friction coefficient stabilizes, and the wear mechanism transitions to a state of abrasive wear. The AlCrCoFeNi alloy demonstrates the lowest friction coefficient and wear rate, exhibiting values of 0.513 and 0.020 × 10 mm/Nm, respectively, while the AlCrCoFeNi alloy demonstrates the highest performance, with a self-corrosion voltage of 0.202 V in a 3.5 wt.% NaCl solution. The experimental findings demonstrate that, in the presence of a decline in the Cr element within a high-entropy alloy, an augmentation in the Al element can facilitate the transition of the FCC phase to the BCC phase within the alloy, thereby enhancing its mechanical properties. However, in the AlCrCoFeNi HEAs, the presence of the Cr-rich and Cr-poor phases invariably results in selective corrosion in a neutral NaCl solution. The corrosion resistance of this alloy is weaker than that of a single-phase solid solution alloy with a similar chemical composition that only undergoes pitting corrosion.
CoCrFeNi高熵合金是一种新型结构材料,在航空航天、汽车、船舶、机械加工、能源、软磁材料和储氢材料等多个领域具有可观的应用潜力。本研究考察了Al元素对该合金结构和性能的影响。制备AlCrCoFeNi(= 0.1、0.2、0.3、0.4、0.5)粉末时,使用了多种元素金属粉末作为原料,并在350转/分钟的转速下进行40小时的机械合金化过程。随后,采用放电等离子烧结在1000℃对合金粉末进行烧结。利用X射线衍射仪(XRD)、扫描电子显微镜(SEM)和能谱仪(EDS)对合金的微观结构进行分析,并使用万能试验机、硬度测量仪、摩擦磨损测量仪和电化学工作站对性能进行分析。研究表明,当 = 0.1时,AlCrCoFeNi的晶体结构由双FCC相和微量σ相组成。随着铝含量增加,部分FCC相开始转变为BCC相。当 = 0.2~0.5时,合金由双FCC相、BCC相和微量σ相组成。随着合金中BCC相增加,合金的抗拉强度增加,塑性变形能力降低,硬度增加。AlCrCoFeNi的最高抗拉强度为1163.14MPa,最小伸长率为26.98%,最大硬度值为412.6HV。在摩擦测量初期,AlCrCoFeNi的磨损机制为粘着磨损。然而,随着测试时间的推进,合金表面开始形成氧化层,导致摩擦系数逐渐增加。此时,磨损机制变为粘着磨损和磨粒磨损的组合。一旦氧化过程和磨损过程达到动态平衡,摩擦系数稳定,磨损机制转变为磨粒磨损状态。AlCrCoFeNi合金的摩擦系数和磨损率最低,分别为0.513和0.020×10⁻³mm²/Nm,而AlCrCoFeNi合金性能最佳,在3.5wt.%NaCl溶液中的自腐蚀电位为0.202V。实验结果表明,在高熵合金中Cr元素含量下降的情况下,Al元素的增加可促进合金中FCC相向BCC相的转变,从而提高其力学性能。然而,在AlCrCoFeNi高熵合金中,富Cr相和贫Cr相的存在总会导致在中性NaCl溶液中发生选择性腐蚀。该合金的耐蚀性比具有相似化学成分且仅发生点蚀的单相固溶体合金弱。