燃气轮机热障涂层高温腐蚀研究综述

刘永葆; 刘建华; 余又红; 贺星; 刘莉

doi:10.3969/j.issn.1673-3185.2017.02.014

燃气轮机热障涂层高温腐蚀研究综述

doi: 10.3969/j.issn.1673-3185.2017.02.014

刘永葆^1,,
刘建华^1, ,,
余又红¹,
贺星¹,
刘莉²

1.
海军工程大学动力工程学院, 湖北武汉 430033
2.
宜春学院物理科学与工程技术学院, 江西宜春 336000

详细信息

作者简介:
刘永葆, 男, 1967年生, 博士, 教授。研究方向:燃气轮机监测、控制与故障诊断。E-mail:yongbaoliu@aliyun.com

通信作者:
刘建华 (通信作者), 男, 1983年生, 博士生。研究方向:燃气轮机监测、控制与故障诊断。E-mail:ljh363418@sina.cn

中图分类号: U668.3;TK47
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出版历程
- 收稿日期: 2016-07-25
- 网络出版日期: 2017-03-13
- 刊出日期: 2017-04-01

Review of hot corrosion of thermal barrier coatings of gas turbine

Yongbao LIU^1
,,
Jianhua LIU^{1
, ,},
Youhong YU¹,
Xing HE¹,
Li LIU²

1.
College of Power Engineering, Naval University of Engineering, Wuhan 430033, China
2.
College of Physics Science and Engineering Technology, Yichun University, Yichun 336000, China

燃气轮机热障涂层高温腐蚀研究综述由刘永葆，等创作，采用知识共享署名4.0国际许可协议进行许可。

摘要

摘要: 目的为了梳理燃气轮机热障涂层服役过程中的高温腐蚀问题，方法对燃气轮机热障涂层腐蚀类型和提高抗腐蚀性能的方法分别进行了归纳分析，并展望了提高热障涂层抗腐蚀性能的发展方向。结果经归纳分析，燃气轮机热障涂层腐蚀类型主要包括：陶瓷层高温相变、粘结层氧化、盐雾腐蚀、CMAS腐蚀以及燃料杂质腐蚀。提高热障涂层抗腐蚀性能的方法主要有：发展新的抗高温腐蚀涂层材料、进行涂层表面防腐处理、改变涂层系统结构以及提高燃气轮机辅助清洁功能。结论未来开发性能优异的新材料仍是提高热障涂层抗腐蚀性能的主要方向，而改进涂层结构设计、材料纳米化对提升热障涂层抗腐蚀性能有很大潜力。随着陶瓷基复合材料的发展，对涂层的高温腐蚀研究将逐步从热障涂层转向环境障涂层（EBC）。
- 燃气轮机 /
- 热障涂层 /
- 高温腐蚀 /
- 综述
Abstract: The review was done in order to make clear the problem of the hot corrosion of the Thermal Barrier Coatings (TBCs) during gas turbine serving. This paper summarizes the factors resulting from the hot corrosion of TBCs during turbine service and classifies methods for enhancing the corrosive resistance of TBCs. A prospective methodology for improving corrosion resistance is also formulated. The main types of corrosion coating include phase reaction, oxidizing of the bond coating, salt-fog corrosion, CMAS corrosion and fuel impurity corrosion. So far, methods for improving the corrosion resistance of TBCs include developing new coating materials, anticorrosive treatment on the surface of TBCs, modifying the stacking configuration and improving the cleansing functions of the gas turbines. In the future, developing new materials with excellent performance will still be the main direction for boosting the improvement of the hot corrosion resistance of TBCs. Simultaneously, improving the tacking configuration and nanotechnology of TBC coatings are potential approaches for improving corrosion resistance. With the development of a Ceramic Matrix Composite (CMC), the focus of the hot corrosion of TBCs may turn to that of Environmental Barrier Coatings (EBCs).
- gas turbine /
- thermal barrier coatings /
- hot corrosion /
- review

HTML全文

图 1 典型TBC涂层结构系统^[2]

Figure 1. Typical structure of TBCs^[2]

下载: 全尺寸图片幻灯片

图 2 复合涂层结构系统^[65]

Figure 2. Composite structure of TBCs^[65]

下载: 全尺寸图片幻灯片

图 3 涡轮叶片极限温度的发展^[66-67]

Figure 3. Tendency of the temperature limitation of the turbine blade^[66-67]

下载: 全尺寸图片幻灯片

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