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Effect of processing parameter changes on the adhesion of plasma-treated carbon fiber reinforced epoxy composites

机译:工艺参数变化对等离子处理碳纤维增强环氧复合材料粘合力的影响

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Atmospheric plasma treatment for the surface preparation of adhesively bonded composite joints appears promising as a replacement to current surface preparation techniques. However, questions remain regarding the sensitivity and optimization of various plasma processing parameters on final composite bond properties. In this study, we continue to investigate how plasma surface treatment processing variables ultimately affect the surface chemistry and bonding behavior of a graphite-epoxy composite. The plasma power level, the working distance of the plasma head, the carrier gas (helium) flow rate, the duration of plasma exposure, and the active gas (oxygen) concentration within the plasma were varied and correlated to surface chemistry variations using X-ray photoelectron spectroscopy (XPS). The carboxyl concentration on the surface was then measured as a function of these changes and correlated to lap shear strengths. In addition, samples were monitored using XPS to evaluate the decay behavior of the surface treatment as a function of time. Treated specimens in both inert and air environments exhibited similar decay profiles. Large changes were not observed until after 24 days of out-time. The effects of plasma treatment, duration of plasma exposure, and out-time on the crack delamination resistance (G_(IC)) of bonded parts were assessed. G_(IC) measurement indicated that solvent wiped bonded specimens exhibited a purely adhesive failure with unstable crack growth. Specimens with abrasion treatment exhibited reduced performance with cracks initiated in the adhesive traveling through both the adhesive-composite interface as well as the outer surface plies of the composite substrate. We believe damage to the composite substrate due to surface preparation caused this failure mode. On the other hand, plasma-treated specimens exhibited consistent failure modes for all treatments above 12 passes. The failures were entirely cohesive with the very high bond strength promoting crack propagation only within the adhesive. The G_(IC) values indicated that the plasma-treated composites were two times as resistant to fracture as conventionally prepared specimens.
机译:大气等离子体处理用于粘合复合材料接头的表面处理似乎有望替代当前的表面处理技术。但是,关于各种等离子体处理参数对最终复合材料粘结性能的敏感性和最优化问题仍然存在。在这项研究中,我们将继续研究等离子体表面处理工艺变量最终如何影响石墨-环氧树脂复合材料的表面化学和键合行为。改变等离子体功率水平,等离子体头的工作距离,载气(氦气)流速,等离子体暴露的持续时间以及等离子体内的活性气体(氧气)浓度,并使用X-将其与表面化学变化相关联射线光电子能谱(XPS)。然后根据这些变化测量表面上的羧基浓度,并将其与搭接剪切强度相关联。另外,使用XPS监测样品,以评估表面处理随时间的衰减行为。在惰性和空气环境中处理过的标本都显示出相似的衰减曲线。直到停工24天后才观察到较大的变化。评估了等离子处理,等离子暴露持续时间和超时时间对粘合零件的抗龟裂性(G_(IC))的影响。 G_(IC)测量表明,用溶剂擦拭的粘结试样表现出纯的粘合破坏,且裂纹扩展不稳定。经过磨蚀处理的样品表现出降低的性能,其中裂纹在粘合剂行进穿过粘合剂-复合材料界面以及复合材料基材的外表面层时引发裂纹。我们认为,由于表面处理而导致的复合材料基材损坏导致了这种失效模式。另一方面,经等离子体处理的样品在12次以上通过的所有处理中均显示出一致的破坏模式。失效与高粘结强度完全粘合在一起,从而仅在粘合剂内促进裂纹扩展。 G_(IC)值表明,经等离子体处理的复合材料的抗断裂性是常规制备样品的两倍。

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