Abstract

Thermoplastic multilayer composites with different fiber orientations per layer were prepared with polypropylene and aramid fibers as reinforcing material. The prepregs were prepared in a continuous impregnation system using the dry powder method in a fluidized bed. The specimens were laminated by compression molding, tensile tested and their fracture area was analyzed by microscopy. The mechanical performance of the laminates was influenced by the fiber orientation at the different layers. The fibers at 0° conferred high stiffness to the composite, limiting the maximum deformation and promoting failure. The laminates with 0o layers showed a fragile and sudden fracture oriented at 90° to the aplied load, even with low fiber content. The plies oriented at  45° balanced the stress and contributed to higher levels of deformation during the test due to fiber rotation towards the loading direction, also, no post-yield stiffening was found as in thermoset composites due to the ductile nature of the thermoplastic matrix; these layers limited the crack propagation in the transverse direction, canceling the in-plane shear stress. The fibers at 90° acted as filler due to poor interface and did not contribute to the improvement of the composite mechanical performance. The evidence shows no delamination in the materials due to the tenacious nature of the thermoplastic matrix, neither saw-toothed or plateau region was found in the stress-strain curves in contrast to thermoset laminates.

Highlights

  • Fiber reinforced thermoset composites are well-known to possess high stiffness and strength

  • The present study addresses the effects of the dimensional scaling and continuous fiber orientation on the tensile properties of thermoplastic composites of Twaron fiber/polypropylene

  • The tested tensile specimens were subjected to Soxhlet extraction to measure the fiber volume fraction of the laminates (ASTM C613-14, 2014)

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Summary

INTRODUCTION

Fiber reinforced thermoset composites are well-known to possess high stiffness and strength. Non-linear stress–strain behavior can be achieved with angle-ply laminates, whilst suppressing the damage mechanisms that normally cause premature failure They showed that, using thin plies, delamination is suppressed for all angles allowing considerable pseudo-ductile strains to develop. Pulungan et al (2017) used unidirectional tapes from SABIC Innovative Plastics to produce [90]8 glass fiber/polypropylene thermoplastic laminates, they proposed a micromechanical approach to predict damage mechanisms and their interactions in laminates under transverse tension using 3D finite element model They studied the microscopic failure mechanisms and their effect on the mesoscale response and found that fiber-matrix interfacial strength affects the stiffness and the strength of the composite significantly. The failure pattern of these materials was studied and related to the composite structure and performance

MATERIALS AND METHODS
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