Ultrasonic Testing of Carbon Fiber Reinforced Resin Matrix Composite Material Structure
摘 要
随着复合材料结构及其制件在航空航天领域中的广泛应用, 对复合材料的无损检测技术也提出了更高的要求。通过制作埋有不同大小人工缺陷的碳纤维增强树脂基复合材料的胶接结构、层压结构和蜂窝夹层结构试块, 并对这些试块进行超声检测试验, 分析了如何设置超声检测参数才能有效检出预埋缺陷的方法。结果表明: 选取合适的检测设备和检测参数, 能够全部检出人工预埋缺陷, 验证了超声方法对碳纤维复合材料结构检测的有效性。
Abstract
With the composite structure and its parts being widely used in aerospace, higher requirement for the nondestructive testing technology has been put forward. Different sizes of artificial defects were buried in glued buried structure,laminated structure, and honeycomb sandwich structure in the carbon fiber reinforced resin matrix composite material test blocks, and these test blocks were tested with ultrasonic and the way how to set the parameters to detect embedded defect effectively was discussed. The results showed that through properly selecting the appropriate detection equipment and testing parameters, all the embedded artificial defects could all be detected.
中图分类号 TG115.28 DOI 10.11973/wsjc201610015
所属栏目 试验研究
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收稿日期 2016/6/24
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备注刘晶晶(1982-), 女, 硕士, 工程师, 主要从事无损检测科研与情报工作。
引用该论文: LIU Jing-jing. Ultrasonic Testing of Carbon Fiber Reinforced Resin Matrix Composite Material Structure[J]. Nondestructive Testing, 2016, 38(10): 64~66
刘晶晶. 碳纤维增强树脂基复合材料结构的超声检测[J]. 无损检测, 2016, 38(10): 64~66
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参考文献
【1】曲亚林,宁宁,詹绍正. 蜂窝夹芯结构的无损检测技术[J].航空制造技术, 2011(20): 78-81.
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