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Hole integrity of carbon fibre reinforced epoxy composites using combined punching and drilling techniques

机译:碳纤维增强环氧复合材料的孔完整性使用组合冲压和钻孔技术

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摘要

Drilling is the most common technique in the hole making of composite panels. Based on the previous study, punching was proposed to replace drilling. This study aims to investigate the effect of hole-making techniques, i.e. new combined technique and conventional drilling technique to the hole quality and performance by conducting experiment based on surface roughness and bearing strength, respectively. The surface roughness measurement was performed oversampling with 3.6-mm thickness at four quadrant points along the hole wall. A bearing test was conducted according to ASTM D5961 procedure-A double shear with a single-pin fastener. The failure modes resulting from an experiment are quantified and compared. It was found that there is a slight difference in the initial ply failure load (IPFL) between the conventional drilling and both combined technique for 0.65% and 7.90%, respectively. However, the difference is still low, i.e. less than 10%. The results confirmed that the use of the combined technique is almost similar to the conventional drilling alone in terms of bearing strength, failure mode, and surface roughness.
机译:钻孔是复合板孔制作中最常见的技术。基于先前的研究,提出了冲压以取代钻孔。本研究旨在研究空穴制造技术的影响,即通过基于表面粗糙度和轴承强度进行实验的新组合技术和常规钻孔技术对空穴质量和性能。在沿着孔壁的四个象限点处以3.6毫米厚度进行表面粗糙度测量。根据ASTM D5961进行轴承测试步骤 - 用单引脚紧固件进行双剪切。用实验产生的失效模式量化并进行比较。发现常规钻孔和组合技术之间的初始帘布层损失负荷(IPFL)分别具有0.65%和7.90%的初始帘布层损伤载荷(IPFL)略有差异。然而,差异仍然很低,即小于10%。结果证实,在轴承强度,故障模式和表面粗糙度方面,使用组合技术几乎与单独的钻井相似。

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