This paper describes the manufacturing method and properties of a superalloy as a gas turbine blade material and a thermal barrier coating to protect it. The development process of superalloy and characteristics of each casting method were introduced. In particular, the single crystal superalloys were analyzed for creep and tensile properties with temperature according to chemical composition. In addition, the theories of creep life prediction models were summarized and comparative analysis was performed. Finally, the manufacturing processes of thermal barrier coatings were introduced, and the characteristics and effects of mechanical, thermal, and durability characteristics of each manufacturing process are described. We believe that this comprehensive review will help not only the gas turbine industry/community, but also material scientists, measurement physicists/engineers, and theorists interested in superalloys and high-temperature ceramics.

中文翻译：

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燃气轮机用高温合金和热障涂层的机械热性能研究进展

本文介绍了高温合金作为燃气轮机叶片材料和用于对其进行保护的隔热涂层的制造方法和性能。介绍了高温合金的发展过程以及每种铸造方法的特点。特别地，根据化学组成分析了单晶高温合金随温度的蠕变和拉伸性能。另外，总结了蠕变寿命预测模型的理论并进行了比较分析。最后，介绍了隔热涂层的制造工艺，并描述了每种制造工艺的机械特性，热特性和耐久性特性的影响。我们认为，这项全面的审查不仅将对燃气轮机行业/社区有所帮助，还将对材料科学家，