Page 218 - Engineered Interfaces in Fiber Reinforced Composites
P. 218

200               Engineered interfaces in fiber  reinforced composites
                    interface with epoxy resins (Allred et al.,  1985). The high nitrogen content in the
                    form of  an amine group is usually accompanied by  a decrease in oxygen content
                    with  increase in  treatment  time. The treatment  also increases the  ILSS of  epoxy
                    matrix composites by 30% to 50% with associated dominant failure mechanisms of
                    fiber splitting and matrix cracking, in contrast to the apparent interface debonding
                    in untreated  counterparts (Brown et al.,  1991). Fig. 5.21 shows the increase in the
                    amine group and the corresponding ILSS with treatment time.
                      In addition, the increase in flexural strength of  treated  fiber composites can be
                    attributed to a lower extent of fiber buckling in the compressive face as a result of
                    improved  interfacial  bonding  (Brown  et  al.,  1992a). A  similar  improvement  in
                    mechanical properties is also reported for vinylester matrix composites (Brown et al.,
                    1992b), which  is associated with  enhanced fiber wettability rather  than  chemical
                    functionality. Improvements in retainability of composite flexural strength and ILSS
                    have  also  been  shown  under  water  aging  condition  for  plasma  treated  Twaron
                    aramid fibers (Verpoest and Springer, 1988; Janssens et al., 1989).
                      Coupling agents: The application of coupling agents to aramid fibers has not been
                    particularly  successful. Vaughan  (1 978) applied  onto  Kevlar  fibers several  silane
                    coupling  agents  that  were  developed  originally  for  glass  fibers  with  limited
                    improvement in the composite strength under both dry and water aging conditions.
                    Application  of  organotitanate  and  organozirconate  coupling  agents  (Sugerman
                    et  al.,  1989) also  shows only  a  slight  improvement in  flexural  strength  of  epoxy
                    matrix composites. The addition of coupling agents after oxygen plasma treatment
                    appears  to  be  a  good  combination  to maximize  the  benefits of  improvement in
                    interface bonding, as evidenced by the 250% increase in the fiber pull-out force for
                    Kevlar  49  fiber  reinforced  silicon rubber  matrix  composites, Table 5.11 (Inagaki























                                            Treatment  time  in min

                    Fig, 5.21. Surface amine concentration (0) of aramid fiber and ILSS (0) of epoxy matrix composites as a
                               function of ammonia plasma treatment time. After Brown et al. (1991).
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