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 fiber-reinforced plastic with four different bonding cases were 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 behavior 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 fiber 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 |
|---|---|
| Article number | 225 |
| Number of pages | 19 |
| Journal | Journal of Composites Science |
| Volume | 5 |
| Issue number | 9 |
| Early online date | 24 Aug 2021 |
| DOIs | |
| Publication status | Published online - 24 Aug 2021 |
Bibliographical note
Funding Information:The authors gratefully thank the EPSRC Future Composites Manufacturing Research Hub for its financial contribution to this project. EPSRC reference number: EP/P006701/1. Acknowledgments: Swiss CMT + Freilacke for the provision of the powder epoxy (PE6405).
Funding Information:
Funding: The authors gratefully thank the EPSRC Future Composites Manufacturing Research Hub for its financial contribution to this project. EPSRC reference number: EP/P006701/1.
Publisher Copyright:
© 2021 by the authors. Licensee MDPI, Basel, Switzerland.
Funding
Funding Information: The authors gratefully thank the EPSRC Future Composites Manufacturing Research Hub for its financial contribution to this project. EPSRC reference number: EP/P006701/1. Acknowledgments: Swiss CMT + Freilacke for the provision of the powder epoxy (PE6405). Funding Information: Funding: The authors gratefully thank the EPSRC Future Composites Manufacturing Research Hub for its financial contribution to this project. EPSRC reference number: EP/P006701/1. Publisher Copyright: © 2021 by the authors. Licensee MDPI, Basel, Switzerland.
Keywords
- co-curing
- lap shear strength
- powder epoxy
- Z-pinning
- out-of-autoclave manufacturing
- Powder epoxy
- Lap shear strength
- Out-of-autoclave manufacturing
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Polymer/fibre through-thickness-reinforcement for carbon-fibre reinforced polymer composites
Moses, W. (Author), McIlhagger, A. (Supervisor) & Archer, E. (Supervisor), Mar 2023Student thesis: Doctoral Thesis
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