Effects of inkjet printed toughener on delamination suppression in drilling of carbon fibre reinforced plastics (CFRPs)

Yu Shi, Xiaonan Wang*, Fuji Wang, Tianyu Gu, Pengheng Xie, Yu Jia

*Corresponding author for this work

Research output: Contribution to journalArticlepeer-review

11 Citations (Scopus)
14 Downloads (Pure)

Abstract

Delamination has been recognised as the predominant damage induced during the drilling of carbon fibre reinforced plastics (CFRPs). It could significantly reduce the bearing capacity and shorten the service life of the designed component. To enhance the delamination resistance of CFRPs for different applications, great affords have been done to improve their interlaminar fracture toughness. However, due to the difficulty in accurately controlling the amount of the toughener applied in the interface, effect of the toughener content on the toughening efficiency is rarely studied. In this work, an experimental research was developed to investigate the performance of the toughener on the improvement of delamination resistance in the drilling of CFRPs and parametrically optimise the toughener content with the consideration of different feed rates. Specifically, poly(methyl methacrylate) (PMMA) solutions with various concentrations were selected to add on the CFRP prepreg, and co-cured together with layups. The inkjet printing technology was adopted to deposit the PMMA solutions for precisely controlled toughener contents. Through drilling experiments on the toughened CFRPs, it was found that the optimal content of the PMMA solution was 10 wt% to offer the least delamination, in particular, for the situation under the highest feed rate condition. The toughing mechanisms were also concluded by analysing the histories of the thrust force and torque in the drilling process. The results of this study is significantly contribute to the locally toughening of the composite interfaces and the improvement of the drilling quality, which is specifically helpful to strengthen the joint property for the structural design stage for the aircraft.

Original languageEnglish
Article number112339
JournalComposite Structures
Volume245
Issue number1
Early online date7 Apr 2020
DOIs
Publication statusPublished - 1 Aug 2020

Bibliographical note

© 2020, Elsevier. Licensed under the Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International http://creativecommons.org/licenses/by-nc-nd/4.0/

Funding

This work is financially supported by the National Key R&D Program of China (Grant No. 2018YFA0702803 ), the Liaoning Revitalization Talents Program (Grant No. XLYC1801008 ) and the State Scholarship Fund of China offered by China Scholarship Council ( CSC ). It also acknowledges the support of facilities for the inkjet printing and manufacturing of composite in Chester Smart Composite Group, University of Chester. The authors wish to thank the anonymous reviewers for their comments which lead to improvements of this paper.

Keywords

  • CFRP
  • Delamination
  • Feed rate
  • Inkjet printing
  • PMMA content
  • Toughen

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