摘要
根据燃气涡轮发动机的工作环境及化学反应的原理，本文详细讨论了因腐蚀介质──Ｎａ２ＳＯ４、ＮａＣｌ、Ｖ２Ｏ５引起的燃气涡轮发动机高温部件热腐蚀的机理。
In accordance with the working conditions of the gas turbine engine and the principles of chemical reaction, this paper discusses in detail the mechanism of hot corrosion caused by corrosive media - Na2SO4, NaCl and V2O5 in the high temperature parts of the gas turbine engine.
出处
《中国民航学院学报》
1994年第1期45-53,共9页
Journal of Civil Aviation University of China
关键词
燃气涡轮发动机
高温部件
热腐蚀
航空发动机
gas turbine engine
high temperature parts
hot corrosion mechanism of chemical
reaction
