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Manufacture of 30 Fibre Preforms                    45

          2.5.3 %Pinning
          An alternate method to the standard stitching process was first described in late 1980's
          (Evans and Boyce, 1989; Boyce et al., 1989) and subsequently has been commercially
          developed  by  the  company  Aztex  (a  subsidiary  of  Foster-Miller)  as  Z-FiberTM
          technology (Freitas et  al.,  1996).  The  technology consists of  embedding previously
          cured reinforcement fibres into a thermoplastic foam that  is  then placed on top of  a
          prepreg, or dry fabric, lay-up and vacuum bagged.  Through judicious  choice of  the
          material, the foam will collapse as the temperature and pressure are increased, allowing
          the fibres to be slowly pushed into the lay-up (see Figure 2.36).  This method can be
          used during the normal autoclave cure of prepreg and for both prepreg and dry fabric
          can be performed whilst the lay-up is on the tool surface itself, thus saving extra steps in
          the  manufacturing  process.  A  version  of  this  technology  can  be  used  at  room
          temperatures as it utilises an ultrasonic horn that heats up a local area of the z-pin foam
          and preform, thus allowing a plunger to push the pre-cured reinforcement yarn into the
          lay-up.  Both methods have been successfully applied to carbodepoxy composites with
          silicon  carbide, boron  and  carbon reinforcement yarns.  Chapter 9  contains further
          details on this technology and the mechanical performance of z-pinned composites.


                                                           Heat and pressure
          Foam with embedded fibres   Vacuum bag








                         Tool

          Figure 2.36 Illustration of z-pinning process


          2.6 SUMMARY

          The  four  textile  processes  of  stitching,  weaving,  braiding  and  knitting,  have  the
          potential to significantly reduce the cost of manufacturing many composite components
          and prodhce structures that have improved mechanical performance in critical design
          cases such as impact. Each of these processes has been briefly described here and their
          advantages and limitations noted. The main aspects of these manufacturing techniques
          have been summarised in Table 2.1 and reviews of these textile processes can be found
          in  the  published  literature (KO, 1989b; Mouritz et  al.,  1999; Kamiya et  al.,  2000).
          However, one manufacturing issue that has only been only briefly mentioned here is the
          potential  of  each  manufacturing  process  to  cause  significant  damage  to  the
          reinforcement yarns and thus degrade the performance of the final composite. Although
          this issue as been partly explored for the stitching process (Mouritz et al., 1997; Mouritz
          and  Cox,  2000)  very  little  investigation  has  been  done  on  the  other  techniques
          mentioned here, although recent work has shown that the effects of processing damage
          can be significant for 3D weaving (Lee et al., in press).
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