飞行器新型碳基复合材料表面高温测量方法

doi:10.12060/j.issn.1000-7202.2014.05.13

宇航计测技术

飞行器新型碳基复合材料表面高温测量方法

赵博¹；芦静华¹；杜海辉¹；易卉¹；杨水旺¹

1、北京振兴计量测试研究所,北京 100074

出版日期:2014-10-15 发布日期:2014-10-15

A Method for Measuring the High Surface Temperature of New Carbon Composite Materials on Aircraft

ZHAO Bo¹；LU Jing-hua¹；DU Hai-hui¹；YI Hui¹；YANG Shui-wang¹

1、Beijing Zhenxing Institute of Metrology and Measurement, Beijing 100074

Online:2014-10-15 Published:2014-10-15

摘要/Abstract

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。

关键词: 高温测量, 新型碳基复合材料, 飞行器表面温度

Abstract: This paper deals with the high surface temperature measurement of the new carbon composite 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.

Key words: High temperature measurement, New carbon composite material, The surface temperature of aircraft

赵博；芦静华；杜海辉；易卉；杨水旺. 飞行器新型碳基复合材料表面高温测量方法[J]. 宇航计测技术, doi: 10.12060/j.issn.1000-7202.2014.05.13.

ZHAO Bo；LU Jing-hua；DU Hai-hui；YI Hui；YANG Shui-wang. A Method for Measuring the High Surface Temperature of New Carbon Composite Materials on Aircraft[J]. JOURNAL OF ASTRONAUTIC METROLOGY AND MEASUREMENT, doi: 10.12060/j.issn.1000-7202.2014.05.13.

飞行器新型碳基复合材料表面高温测量方法

A Method for Measuring the High Surface Temperature of New Carbon Composite Materials on Aircraft

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