摘要
本文针对飞行器新型碳基复合材料表面的高温测量问题,介绍了测量方法、传感器的安装方式、高温胶黏剂技术与工艺,传感器与热防护技术以及试验测试,并归纳了该方法的技术特点。
This paper deals with the high surface temperature measurement of the new carbon com-posite materials on aircraft, introduces the method measurement, the installation method of senor, the technique with high temperature adhesives, sensor and thermal protection, and summarizes the features of this method.
出处
《宇航计测技术》
CSCD
2014年第5期55-57,78,共4页
Journal of Astronautic Metrology and Measurement
关键词
高温测量
新型碳基复合材料
飞行器表面温度
High temperature measurement New carbon composite material The surface temper-ature of aircraft
