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镍基单晶高温合金/热障涂层体系的应用研究进展

刘砚飞 钟燕 陶稀鹏 田伟 郭会明 梁伟

材料工程2025,Vol.53Issue(9):1-10,10.
材料工程2025,Vol.53Issue(9):1-10,10.DOI:10.11868/j.issn.1001-4381.2023.000862

镍基单晶高温合金/热障涂层体系的应用研究进展

Research progress in application of nickel-based single crystal superalloy/thermal barrier coating system

刘砚飞 1钟燕 2陶稀鹏 3田伟 2郭会明 2梁伟2

作者信息

  • 1. 中国科学技术大学 材料科学与工程学院,沈阳 110016||中国航发四川燃气涡轮研究院 材料与工艺技术研究室,成都 610500
  • 2. 中国航发四川燃气涡轮研究院 材料与工艺技术研究室,成都 610500
  • 3. 中国科学院金属研究所,沈阳 110016
  • 折叠

摘要

Abstract

In the pursuit of achieving a superior thrust-to-weight ratio and service reliability for advanced aero engines,increasingly stringent requirements are continually imposed on the material and process selection for turbine blades.Turbine blades featuring nickel-based single crystal superalloys with thermal barrier coatings have emerged as a hallmark of advanced aero engines.The research and development of nickel-based single crystal superalloys and thermal barrier coating materials,coupled with the evaluation of nickel-based single crystal superalloy/thermal barrier coating systems,are pivotal in ensuring the safe and reliable performances of turbine blades.This topic is among the hottest in the field.This paper provides a comprehensive introduction to the research and application of nickel-based single crystal superalloys and thermal barrier coating materials for turbine blades.It summarizes the evaluation methods and failure mechanisms of single crystal superalloy/thermal barrier coating systems.Finally,the research focuses on nickel-based single crystal superalloy/thermal barrier coating systems are highlighted,aiming to serve as a valuable reference for fully harnessing the potential of these systems.

关键词

镍基单晶高温合金/热障涂层/评价/界面/失效机理

Key words

nickel-based single crystal superalloy/thermal barrier coating/evaluation/interface/failure mechanism

分类

矿业与冶金

引用本文复制引用

刘砚飞,钟燕,陶稀鹏,田伟,郭会明,梁伟..镍基单晶高温合金/热障涂层体系的应用研究进展[J].材料工程,2025,53(9):1-10,10.

材料工程

OA北大核心

1001-4381

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