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| 飞行器新型碳基复合材料表面高温测量方法 | |
| 引用本文： | 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, 2014, 34(5): 55-57. DOI: 10.12060/j.issn.1000-7202.2014.05.13 |
| 作者姓名： | 赵博 芦静华 杜海辉 易卉 杨水旺 |
| 作者单位： | 1、北京振兴计量测试研究所,北京 100074 |
| 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 |
A Method for Measuring the High Surface Temperature of New Carbon Composite Materials on Aircraft |
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| 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, 2014, 34(5): 55-57. DOI: 10.12060/j.issn.1000-7202.2014.05.13 | |
| Authors: | ZHAO Bo LU Jing-hua DU Hai-hui YI Hui YANG Shui-wang |
| Affiliation: | 1、Beijing Zhenxing Institute of Metrology and Measurement, Beijing 100074 |
| Abstract: | 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. |
| Keywords: | High temperature measurement New carbon composite material The surface temper-ature of aircraft |
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