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Chapter 9


             Z-Pinned Composites









             9.1 INTRODUCTION

             The technology of reinforcing composites in the through-thickness direction with small
             pins was first evaluated in the 1970s. Thin steel pin wires were inserted at offset angles
             of  k45O into carbodepoxy prepreg laminates to  improve the  delamination toughness
             (Huang et al., 1978). The pins used were very thin, with a diameter of only 0.25 mm, to
             minimise damage  to  the  laminates.  The  steel  pins  were  effective in  increasing the
             interlaminar  shear  strength  and  delamination resistance.  However,  initially  it  was
             neither practical nor cost-effective to  insert thin  pins over a  large area of  composite
             material, and  therefore the technology was not  immediately taken-up by  the  aircraft
             composites industry.
                Z-pinning technology was developed further in the early  1990s by Aztex Inc. The
             technology  involves  embedding  small  diameter  pins,  known  as  Z-fibersTM, into
             com  osites to produce a  3D fibre network  structure, as illustrated in Figure 9.1. Z-
             fiberL   technology  is  the  newest  of  the  various  techniques  for  producing  3D
             composites, and already it has a wide variety of potential applications in engineering
             structures.  An  important  potential  use  of  Z-fibersTM is  for  the  attachment  and
             reinforcement of composite joint structures such as lap joints, T-joints and rib stiffeners.
             Z-pins are being used to fasten hat-stiffened sections to the composite skins in selected
             parts of the F/A-18 Hornet fighter aircraft.  Z-fibersTM can be used in composite joints
             in place of bolted fasteners or rivets to provide a more evenly distributed load over the
             joint area. Z-fibersTM can also be used for the local reinforcement of composite panels
             to reduce the incidence of edge delaminations as well as the reinforcement of sandwich
             panels to minimise the likelihood of skin peeling and debonding.














             Figure 9.1 Schematic illustration of a z-pinned composite


             The relatively recent development of  Z-fibersTM has  meant  that  z-pinned composites
             have not been explored in detail.  In this chapter the current state of  knowledge of z-
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