| 对某机复合材料件加载试验无损检测跟踪研究 |
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| 引用本文： | 黄承恭,朱金荣,廉京活.对某机复合材料件加载试验无损检测跟踪研究[J].直升机技术,1997(4). |
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| 作者姓名： | 黄承恭 朱金荣 廉京活 |
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| 作者单位： | 中国直升机设计研究所，中国直升机设计研究所，国营122厂 景德镇 333001，景德镇 333001，哈尔滨 150066 |
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| 摘 要： | 加载至破坏无损检测跟踪研究在国内是首次进行,本文是在试验报告的基础上进行编写的,为使读者能了解全貌,有意对某机复合材料结构和跟踪检测情况作了介绍。重点是对试验结果进行分析,从而确定检测方法的有效性和预加载荷值的大小。并对复合材料的破坏机理作了介绍,这对今后复合材料新研件及质量控制有重大意义。
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| 关 键 词： | 复合材料 检测 |
AN TRACK INVESTIGANTION TO NONSTRUCTIVE INSPECTION OF LOADING TEST OF SOME COMPOSITES |
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| Authors: | Huang Chenggong Zhu Jingrong |
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| Abstract: | Composite structure and tracking measure of a certain type helicopter are introduced purposely in the article which is compiled according to the test paper in which traddng reseach of nonstructive testing loading up to fracture has been completed for the fast time in china to make readers to understand research whole process. Test results have been analysed emphatically to determine measuring method efficiency and pre-loading value. Fracture condition of the composite has been introduced also, which is of important significance to future developed composite component and quality cotrol. |
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| Keywords: | Composit Testing |
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