CFRP层压板钻孔过程出口分层破坏模型

Iker Urresti Espilla , Iñigo Llanos , Luis Norberto López de Lacalle
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引用次数: 0

摘要

CFRP部件的钻削是飞机制造业的关键制造工艺。机身结构和机身蒙皮通常采用铆接方式组装,这需要对复合材料部件进行预钻孔。然而,由于材料的不均匀性和各向异性,钻进CFRP可能具有挑战性,这可能导致分层、纤维拔出和未切割纤维等重大缺陷。特别是,孔出口处的推出分层被认为是至关重要的,因为它会损害组件的结构健康,甚至导致它们被丢弃。因此,开发预测推出分层的监测和建模技术对该行业具有重要意义。在这方面,本工作引入了一个预测CFRP钻孔过程中出口分层和推力演变的理论模型。将结果与从实验钻孔试验中获得的零件分层和推力数据进行了比较。结果表明,所提出的模型可以为CFRP钻削工艺优化提供有价值的见解,使航空航天工业能够改进当前的钻削实践,以实现CFRP部件的无分层钻削。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
Exit delamination failure modelling during drilling of CFRP laminates
Drilling of CFRP components is a key manufacturing process in the aircraft manufacturing industry. Airframe structures and fuselage skins are often assembled using riveted joints, which require pre-drilling of composite parts. However, drilling CFRP can be challenging due to the inhomogeneous and anisotropic nature of the material, which can lead to major defects such as delamination, fiber pull-out and uncut fibers. In particular, push-out delamination at the hole exit is considered critical, as it can compromise the structural health of the components and even lead to their rejection. Therefore, the development of monitoring and modeling techniques to predict push-out delamination is of great importance to the industry. In this regard, the present work introduces a theoretical model for the prediction of exit delamination and thrust force evolution during CFRP drilling. The results are evaluated in comparison to part delamination and thrust force data obtained from experimental drilling tests. The results indicate that the proposed model can provide valuable insight into the CFRP drilling for process optimization, enabling the aerospace industry to improve current drilling practices towards delamination free drilling of CFRP components.
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CiteScore
3.80
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