Mechanical behaviour of thermoplastic composites spot-welded and mechanically fastened joints

A preliminary comparison

Journal Article (2016)
Author(s)

Tian Zhao (TU Delft - Structural Integrity & Composites)

G. Palardy (TU Delft - Structural Integrity & Composites)

I.F. Villegas (TU Delft - Structural Integrity & Composites)

C.D. Rans (TU Delft - Structural Integrity & Composites)

MJ Martinez (Clarkson University)

R. Benedictus (TU Delft - Aerospace Structures & Materials)

Research Group
Structural Integrity & Composites
Copyright
© 2016 T. Zhao, G. Palardy, I.F. Villegas, C.D. Rans, M.J. Martinez, R. Benedictus
DOI related publication
https://doi.org/10.1016/j.compositesb.2016.12.028
More Info
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Publication Year
2016
Language
English
Copyright
© 2016 T. Zhao, G. Palardy, I.F. Villegas, C.D. Rans, M.J. Martinez, R. Benedictus
Research Group
Structural Integrity & Composites
Issue number
1
Volume number
112
Pages (from-to)
224-234

Abstract

The in-plane and out-of-plane mechanical behaviour of both ultrasonically spot-welded and mechanically fastened joints was investigated by double-lap shear and pull-through tests, respectively. Spot-welded specimens showed comparable onset failure load and significantly higher joint stiffness compared to mechanical fasteners when carrying shear load. The failure modes and the damage within specimens were analysed after mechanical tests. Intralaminar failure and very limited damage on the out-most ply were found for welded specimens, whereas catastrophic through-the-thickness failure was observed for mechanically fastened joints. Based on the experimental outcomes, the mechanical performance and failure mechanisms of spot-welded joints were critically assessed in comparison to the mechanical fasteners .

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