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FeAtures




          the prepared flame retarded SR-PPCs still outperforms that   When  considering  all  the  examined  mechanical
          of a common polypropylene. As expected, high ductility   characteristics of the prepared SR-PPCs, it can be
          indices are accompanied with the plastic deformation of   concluded  that  good  balance between  the  strength,
          the non-reinforced ePP samples, while decreased ductility   stiffness, and impact resistance was reached as a result of
          factors are characteristic for the SRPCs with more rigid   combining high tenacity fibres with elastomer matrix. Up
          rupture.                                              to 10% FR content, the composites keep this advantageous
                                                                mechanical performance, but at 15% FR loading loss of
          Figure 8
                                                                mechanical properties occurs. To further investigate the
                                                                change in the structure of the composites as a function of
                                                                increasing FR content, SEM micrographs were taken from
                                                                the fracture surfaces. During SEM observation (Figure 10),
                                                                prominent  fibre-matrix  adhesion  was  observed  for  all
                                                                SR-PPCs; the hPP fibres are properly impregnated by the
                                                                matrix material. It is also visible that the polar FR particles
                                                                are well dispersed in the ePP matrix. Nevertheless, when
                                                                exposed to tensile stress, the FR particles became easily
                                                                detached from the apolar matrix, and therefore as fault
                                                                locations  decreased  the  tensile  strength  of  the  flame
                                                                retarded  samples  (see  in  Figure  6).  Based  on  the  SEM
          Comparison of (A) perforation energy and (B) ductility factor of injection   images, it became also obvious that in the SR-PP_FR15
          moulded flame retarded non‐reinforced and self‐reinforced PP samples  composite, the structure of the reinforcing hPP fibres got
          Common Charpy impact tests could not be performed     damaged during processing likely due to the increased
          on the ePP-based samples because the elastomer-based   thermo-mechanical and abrasive stress caused by the FR
          specimens did not break during testing; therefore, tensile   particles being present at 30 wt% in the matrix. At lower
          impact test was performed to further characterize the   FR loading (20 wt%) of the matrix (Figure 10B), however,
          impact resistance. It can be seen in Figure 9 that the   the hPP fibres seem to be intact. It is proposed that in the
          tensile impact strength shows decreasing tendency with   case of the SR-PP_FR15 composite, the high amount of FR
          increasing FR content for both types of injection moulded   particles causes significant changes in the shear forces and
          samples. It is proposed that the FR particles function as   thermal conditions during injection moulding, which result
          defect location in the matrix and thereby decrease the   in undesirable molecular relaxation, structural damage,
          mechanical resistance. Considering the tensile impact   and partial melting of the reinforcing hPP fibres during
          strength results, the non-reinforced samples outperform   processing and consequently in remarkable property loss
          their self-reinforced counterparts because during failure   of this composite.
          plastic deformation absorbs more energy than fibre pull-  Figure 10
          out or breakage (see also in Figure 7).

          Figure 9








                                                                SEM  micrographs  taken  from  the  fracture  surface  of  (A)  SR‐PP,  (B)
                                                                SR‐PP_FR10, and (C) SR‐PP_FR15 samples






          Comparison of the tensile impact strength (notched) of injection
          moulded flame retarded non‐reinforced and self‐reinforced PP samples

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