Hot corrosion in gas turbine components

Hot corrosion in gas turbine components
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DOI:
10.1016/s1350-6307(00)00035-2
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发表时间:
2002-02-01
影响因子:
4
通讯作者:
Latanision, RM
Latanision, RM
中科院分区:
工程技术2区
文献类型:
--
作者:
Eliaz, N;Shemesh, G;Latanision, RM

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本文综述了高温热腐蚀和低温热腐蚀的宏观和微观特征,并提出了高温热腐蚀和低温热腐蚀的机理。介绍了两个燃气涡轮机叶片失效的实例。不同的实用方法,以尽量减少热腐蚀的描述。(C)2002爱思唯尔科技有限公司版权所有。
The macroscopic and microscopic characteristics as well as the proposed mechanisms of Type I (high-temperature) and Type II (low-temperature) hot corrosion are reviewed. Two case histories of gas turbine blade failures are presented. Different practical approaches to minimize hot corrosion are described. (C) 2002 Elsevier Science Ltd. All rights reserved.