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

A preliminary comparison

Journal Article (2016)
Author(s)

Tian Zhao (TU Delft - Aerospace Engineering)

Genevieve Palardy (TU Delft - Aerospace Engineering)

Irene Fernandez Villegas (TU Delft - Aerospace Engineering)

Calvin Rans (TU Delft - Aerospace Engineering)

Marcias Martinez (Clarkson University)

Rinze Benedictus (TU Delft - Aerospace Engineering)

Research Group
Structural Integrity & Composites
DOI related publication
https://doi.org/10.1016/j.compositesb.2016.12.028 Final published version
More Info
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Publication Year
2016
Language
English
Research Group
Structural Integrity & Composites
Journal title
Composites Part B: Engineering
Issue number
1
Volume number
112
Pages (from-to)
224-234
Downloads counter
398
Collections
Institutional Repository

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 .