Hot corrosion in gas turbine components

被引：577

作者：

Eliaz, N ^{[1
]}

Shemesh, G ^{[1
]}

Latanision, RM ^{[1
]}

机构：

[1] MIT, HH Uhlig Corros Lab, Cambridge, MA 02139 USA

来源：

ENGINEERING FAILURE ANALYSIS | 2002年 / 9卷 / 01期

关键词：

corrosion; oxidation; turbine blade failures; failure analysis; fatigue failure;

D O I：

10.1016/S1350-6307(00)00035-2

中图分类号：

TH [机械、仪表工业];

学科分类号：

0802 ;

摘要：

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.

引用

页码：31 / 43

页数：13

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