摘要
对国内外航空发动机热端部件测控技术水平作了简要论述。着重介绍了高温环境下的温度、热流、应变和涡轮间隙等的测量方法及发展趋势。
The current status of testing technology for aeroengine hot end components in China and oversea is briefed in this paper. Emphasis is given to the testing procedures for the temperature, hot flow, strain and turbine gaps in the high temperature envi-roments.
出处
《航空科学技术》
1997年第6期26-28,共3页
Aeronautical Science & Technology
