Abstract

The purpose of this study was to manufacture hybrid composites from fabrics with superior ballistic performance, and to analyze their viscoelastic and mechanical response. Therefore, composites in hybrid lay-up modes were manufactured from Vectran, Kevlar and aluminum fiber-woven fabrics through a vacuum assisted resin transfer molding. The specimens were consequently analyzed using static three-point bending, as well as by dynamic mechanical analysis (DMA). Apart from DMA, time–temperature superposition (TTS) analysis was performed by all available models. It was possible to study the intrinsic viscoelastic behavior of hybrid ballistic laminates, with TTS analysis gained from creep testing. A polynomic mathematical function was proposed to provide a high accuracy for TTS curves, when shifting out of the linearity regimes is required. The usual Williams–Landel–Ferry and Arrhenius models proved not useful in order to describe and model the shift factors of the acquired curves. In terms of static results, the highly nonlinear stress–strain curve of both composites was obvious, whereas the differential mechanism of failure in relation to stress absorption, at each stage of deformation, was studied. SEM fractography revealed that hybrid specimens with Kevlar plies are prone to tensile side failure, whereas the hybrid specimens with Vectran plies exhibited high performance on the tensile side of the specimens in three-point bending, leading to compressive failure owing to the high stress retained at higher strains after the maximum bending strength was reached.

Highlights

  • It was found that by increasing the hybrid ratio of laminates reinforced with high modulus polyimide and carbon fibers, in an epoxy resin matrix, that a higher tensile modulus can be achieved, whereas the tensile failure strength is decreased [3]

  • Hybrid composite specimens were manufactured with Kevlar, aluminum/glass fibers and Vectran fiber plies

  • Three-point bending results showed that the hybrid composite laminates exhibited a progressive failure mode consisting of fiber failure, debonding, and delamination

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Summary

Introduction

The use of hybrid composite laminates can lead to interesting properties owing to the combination of reinforcement materials [2]. It was found that by increasing the hybrid ratio of laminates reinforced with high modulus polyimide and carbon fibers, in an epoxy resin matrix, that a higher tensile modulus can be achieved, whereas the tensile failure strength is decreased [3]. A study of eco-friendly hybrid composites with banana and sisal reinforcements concluded, that a significant loss of mechanical strength occurred when compared to the composites with single type of reinforcement [5]. Kevlar/epoxy resin composite reinforced with nano-silica particles possessed superior mechanical properties compared with Kevlar composites [6]

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