Abstract
A self-healing, high performance, fibre reinforced polymer (FRP) composite material is demonstrated by employing a Lewis acid-catalysed epoxy self-healing agent (SHA) within a laminate manufactured using existing industrial methods. Thermal cure analysis and mechanical testing is employed to characterise the self-healed polymer. A bio-inspired series of vascules incorporated into an FRP composite material facilitates the delivery of SHAs to exposed fractured crack planes. Healing is effected by ring-opening polymerisation (ROP) of an epoxy resin using novel metal triflate catalysts injected after Mode I crack opening displacement. Strong adhesive compatibility with the host matrix confers full recovery of mechanical properties (>99% healing).
Original language | English |
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Pages (from-to) | 208-218 |
Number of pages | 11 |
Journal | Macromolecular Materials & Engineering |
Volume | 299 |
Issue number | 2 |
Early online date | 2 Jul 2013 |
DOIs | |
Publication status | Published - 3 Feb 2014 |
Keywords
- bio-inspired
- ductile failure
- epoxy
- ring-opening polymerisation
- self-healing
- AEROSPACE APPLICATIONS
- DAMAGE
- IMPACT
- SYSTEMS