Wee Sunguk, Kim Keekeun, Park Kibum, Seok Changsung
Department of Mechanical Engineering, Sungkyunkwan University, Suwon 16419, Korea.
Materials (Basel). 2021 Nov 18;14(22):6971. doi: 10.3390/ma14226971.
Higher fatigue and creep resistance at high temperatures are the essential properties for materials such as those used in gas turbines for power generation and aircraft turbines. Therefore, the nickel-based superalloy CMSX-4 was developed through single-crystal casting to satisfy these requirements. In this study, the CMSX-4 creep test results reported by previous researchers were used to mathematically derive an equation to estimate the amount of creep damage occurring under variable load conditions. In addition, low-cycle fatigue tests were performed, and the effect of creep damage occurring during fatigue on material failure was described.
对于用于发电燃气轮机和航空涡轮机等的材料而言,在高温下具有更高的抗疲劳和抗蠕变性能是其基本特性。因此,通过单晶铸造开发了镍基高温合金CMSX-4以满足这些要求。在本研究中,利用先前研究人员报告的CMSX-4蠕变试验结果,通过数学推导得出一个方程,用于估算在可变载荷条件下发生的蠕变损伤量。此外,还进行了低周疲劳试验,并描述了疲劳过程中发生的蠕变损伤对材料失效的影响。