Abstract
Large composite structures manufactured out-of-autoclave require the assembly and bonding of multiple parts. A one-shot cure manufacturing method is demonstrated using powder epoxy. Lap shear plates were manufactured from powder epoxy and glass fibre reinforced plastic with four different bonding cases assessed: secondary bonding using standard adhesive film, secondary bonding using powder epoxy, co-curing and co-curing plus a novel Z-pinning method. This work investigates the lap shear strength of the four cases in accordance with ISO 4587:2003. Damage mechanisms and fracture behaviour were explored using Digital Image Correlation (DIC) and Scanning Electron Microscopy (SEM) respectively. VTFA400 adhesive had a load at break 24.8% lower than secondary bonding using powder epoxy. Co-curing increased the load at break by 7.8% compared to powder epoxy secondary bonding, with the co-cured and pinned joint resulting in a 45.4% increase. In the co-cured and co-cured plus pinned cases, DIC indicated premature failure due to resin spew. SEM indicated shear failure of resin areas and a large amount of fibre pullout in both these cases, with pinning delaying fracture phenomena resulting in increased lap joint strength. This highlights the potential of powder epoxy for the co-curing of large composite structures out-of-autoclave.
Original language | English |
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Article number | 225 |
Journal | Journal of Composites Science |
Volume | 5 |
Issue number | 9 |
Early online date | 24 Aug 2021 |
DOIs | |
Publication status | E-pub ahead of print - 24 Aug 2021 |
Keywords / Materials (for Non-textual outputs)
- Co-curing
- lap shear strength
- powder epoxy
- Z-pinning
- out-of-autoclave
- manufacturing