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Non-destructive characterization of bondlines in composite adhesive joints

机译:复合粘合剂接头中粘结层的非破坏性表征

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摘要

Aerospace structures use polymeric composite materials extensively.These composite materials are normally bonded together by adhesives to form structural parts.The existence of any kind of defects or discontinuities in the bonds is completely undesirable for such applications.Ultrasonic imaging (UI) is a widely used technique for non-destructive evaluation (NDE) and can be adopted to evaluate the integrity of such adhesively-bonded joints.However,characterization of adhesive bonds in composite materials using UI has deficiencies due to problems such as high acoustic attenuation and high signal-to-noise ratio.These problems can be attributed to the inhomogeneity in composite structures.The present study addresses the problems of detection of disbonds and porosity in adhesively bonded carbon fiber reinforced composite panels.Five sets of adhesively-joined carbon/epoxy composites with different adherend surface preparations were fabricated and subjected to UI.The panels contained known defects in the bondline of the samples.UI results are interpreted to identify various existing defects such as voids,cracks and disbonds in the joints.Attenuation coefficient values for all types of composites are utilized to ascertain the validity of the image analysis.
机译:航空航天结构广泛使用聚合物复合材料,这些复合材料通常通过粘合剂粘结在一起以形成结构部件,粘结中不存在任何类型的缺陷或不连续性对于此类应用是完全不希望的,超声成像(UI)已被广泛使用无损评估(NDE)技术,可用于评估此类粘合接头的完整性。然而,由于UI的高声衰减和高信这些问题可以归因于复合材料结构的不均匀性。本研究解决了粘合碳纤维增强复合材料板中脱胶和孔隙率的检测问题。五套不同粘合物的粘合碳/环氧复合材料制作了表面制剂并进行了UI处理。解释UI结果以识别各种现存的缺陷,例如接缝中的空隙,裂纹和粘连。使用所有类型复合材料的衰减系数值来确定图像分析的有效性。

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