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    直升机复合材料椅盆层压件富胶缺陷的超声检测

    Ultrasonic testing of excessive resin defects in laminated parts of composite material seat basins of helicopters

    • 摘要: 为探究直升机复合材料椅盆层压件大面积超声信号异常现象的成因,开展层压件对比试块的设计制作研究。通过对设计制作的预制缺陷对比试块超声检测信号的分析总结,得出分层、富胶两类缺陷所对应的超声信号特征区别。试验结果表明,不同缺陷的超声检测底波、缺陷波、杂波以及C扫图像均存在一定区别,通过对其的分析能达到准确判定分层与富胶缺陷的目的,并实现缺陷的精准定位定量,此判定方法可应用于椅盆层压件日常检测工作中。

       

      Abstract: To investigate the causes of large-area ultrasonic signal anomalies in helicopter composite chair basin laminates, research on the design and fabrication of comparative test blocks for laminates was conducted. Through analysis and summarization of ultrasonic testing signals from prefabricated defect comparative test blocks, the characteristic differences in ultrasonic signals corresponding to two types of defects, delamination and resin richness, were obtained. The experimental results showed that there were certain differences in the bottom wave, defect wave, clutter, and C-scan images of ultrasonic testing for different defects. Through analysis, accurate determination of delamination and resin richness defects could be achieved, and precise localization and quantification of defects could be realized. This determination method could be applied to daily inspection work of chair basin laminates.

       

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