Abstract

This paper reports on the production and evaluation of a new class of “Z-axis” composite sandwich panel where the core consists of a dense array of vertically-aligned, 3 mm long E-glass fibre composite “beams”. The E-glass fibre bundles were aligned using electrostatic charging. A procedure was developed to retain the orientation of the short-fibre bundles whilst they were impregnated and cured with an epoxy/amine resin system. The skins were manufactured from 4-ply carbon/epoxy prepregs with a layup sequence of (0,90)s. The out-of-plane compressive strength of these Z-axis composites was found to be 25.2 and 15.2 times greater than equivalent sandwich panels made with Nomex® and aluminium honeycomb cores respectively. Their compressive strength was found to increase in proportion to the density of the core. Buckling and fracture of the vertically-aligned Z-axis composite were the predominant failure modes observed. The shear and flexural properties of the Z-axis composites were comparable to equivalent honeycomb sandwich panels manufactured from Nomex® and aluminium honeycomb cores.

Highlights

  • A sandwich composite panel consists of a lightweight core bonded to two stiff and strong reinforced outer skins

  • The current paper reports on a method to manufacture a new class of sandwich composite where the core consists of a dense array of vertically-aligned 3 mm long E-glass fibre bundles

  • The bundle tends to align along the electric field and it levitates towards the grounded upper electrode as the electrostatic force exceeds the weight of the bundle

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Summary

Introduction

A sandwich composite panel consists of a lightweight core bonded to two stiff and strong reinforced outer skins. Cross-ply carbon fibre skins, in an epoxy/amine resin system, was selected for manufacturing the conventional honeycomb sandwich and the Z-axis composites; this was done to enable a direct comparison between the different classes of core materials. In the first series of experiments, Araldite-Rapid, a 2-part resin (Huntsman Advanced Materials, UK), was used for bonding the Z-axis preforms and the honeycombs to the carbon fibre composite skins. Production of shear test specimens: Six each of the NomexVR and aluminium honeycomb sandwich composites were manufactured in the same manner as described previously In this instance the length and width was 100 x 50 mm respectively. Production of flexural test specimens: The NomexVR , aluminium and Z-axis sandwich composite panels were manufactured as described previously for the compression and shear test specimens. The flexural stiffness and the shear rigidity were calculated as specified in ASTM standard D7250 [35]

Results and discussion
Conclusions
28. Carbon fibre skins
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