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Article

Delamination of Fibre Metal Laminates Due to Drilling: Experimental Study and Fracture Mechanics-Based Modelling

by
Francisco Marques
1,
Filipe G. A. Silva
2,
Tiago E. F. Silva
2,*,
Pedro A. R. Rosa
3,
António T. Marques
2,4 and
Abílio M. P. de Jesus
2,4
1
Palbit S.A., Product Development Department, 3854-908 Branca, Portugal
2
INEGI, Faculty of Engineering, University of Porto, Rua Dr. Roberto Frias 400, 4200-465 Porto, Portugal
3
IDMEC, Instituto Superior Tecnico, University of Lisbon, Avenida Rovisco Pais 1, 1049-001 Lisboa, Portugal
4
DEMEc, Faculty of Engineering, University of Porto, Rua Dr. Roberto Frias 400, 4200-465 Porto, Portugal
*
Author to whom correspondence should be addressed.
Metals 2022, 12(8), 1262; https://doi.org/10.3390/met12081262
Submission received: 30 May 2022 / Revised: 22 July 2022 / Accepted: 23 July 2022 / Published: 27 July 2022
(This article belongs to the Special Issue Machining: State-of-the-Art 2022)

Abstract

Fibre metal laminates (FML) are significantly adopted in the aviation industry due to their convenient combination of specific strength, impact resistance and ductility. Drilling of such materials is a regular pre-requisite which enables assembly operations, typically through rivet joining. However, the hole-making operation is of increased complexity due to the dissimilarity of the involved materials, often resulting in defects (i.e., material interface delamination), which can significantly compromise the otherwise excellent fatigue strength. This work explores the potential of three different drill geometries, operating under variable cutting speeds and feeds on CFRP-AA laminates. In addition, the usage of sacrificial back support is investigated and cutting load, surface roughness and delamination extension are examined. In order to predict delamination occurrence, ADCB tests are performed, enabling the calculation of fracture energy threshold. Drill geometry presents a very significant influence on delamination occurrence. The usage of specific step-tools with secondary cutting edge showed superior performance. Despite its simplicity, the applied critical force threshold model was able to successfully predict interface delamination with good accuracy.
Keywords: fibre metal laminates; drilling; cutting tool; modelling fibre metal laminates; drilling; cutting tool; modelling

Share and Cite

MDPI and ACS Style

Marques, F.; Silva, F.G.A.; Silva, T.E.F.; Rosa, P.A.R.; Marques, A.T.; de Jesus, A.M.P. Delamination of Fibre Metal Laminates Due to Drilling: Experimental Study and Fracture Mechanics-Based Modelling. Metals 2022, 12, 1262. https://doi.org/10.3390/met12081262

AMA Style

Marques F, Silva FGA, Silva TEF, Rosa PAR, Marques AT, de Jesus AMP. Delamination of Fibre Metal Laminates Due to Drilling: Experimental Study and Fracture Mechanics-Based Modelling. Metals. 2022; 12(8):1262. https://doi.org/10.3390/met12081262

Chicago/Turabian Style

Marques, Francisco, Filipe G. A. Silva, Tiago E. F. Silva, Pedro A. R. Rosa, António T. Marques, and Abílio M. P. de Jesus. 2022. "Delamination of Fibre Metal Laminates Due to Drilling: Experimental Study and Fracture Mechanics-Based Modelling" Metals 12, no. 8: 1262. https://doi.org/10.3390/met12081262

APA Style

Marques, F., Silva, F. G. A., Silva, T. E. F., Rosa, P. A. R., Marques, A. T., & de Jesus, A. M. P. (2022). Delamination of Fibre Metal Laminates Due to Drilling: Experimental Study and Fracture Mechanics-Based Modelling. Metals, 12(8), 1262. https://doi.org/10.3390/met12081262

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