Abstract
This paper presents a method of joining carbon-fibre plies and rigid cellular foam core with stitching for producing light-weight composite structures. After resin infusion and consolidation, the stitched sandwich panel exhibits superior damage tolerance as well as improved transverse properties due to the presence of through-thickness fibre reinforcement. First part of the paper deals with the conceptual development of a multi-needle stitching machine for rigid foams. A needle penetration model for computing the penetration forces has been reported - there is a good agreement between the experimental and theoretical penetration force-displacement curves. A number of sandwich panels with orthogonal and bias stitch orientations have been developed and examined for stitch quality with the aid of X-ray tomography. The paper also presents results from quasi-static indentation, three-point bending and transverse compression tests, on both the stitched and unstitched sandwich panels. © 2012 Springer Science+Business Media B.V.
Original language | English |
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Pages (from-to) | 553-568 |
Number of pages | 15 |
Journal | Applied Composite Materials |
Volume | 20 |
Issue number | 4 |
DOIs | |
Publication status | Published - Aug 2013 |
Keywords
- Damage tolerance
- Multi-needle stitching
- Rigid foam
- Sandwich structures
- Through-thickness