Abstract

The present work describes the mechanical characterization combined with the thermal degradation kinetics of Carbon Fiber Reinforced Polymers (CFRP). The thermal degradation kinetics of CFRP have never been studied in the past. In that regard, the present work focuses on studying the thermal degradation kinetics of CFRP tested mechanically at different environmental conditions. Tensile tests were performed on the specimens with different lay-ups at room temperature, elevated temperature (71 °C), and cryogenic conditions (−54 °C), and the same specimens were used for thermal degradation kinetic studies. Mechanical tests show different responses respect to the different environmental conditions and different fibers orientation. On the other hand, the thermogravimetric results, mass loss, and derivative mass loss, show no significant difference in the degradation of CFRP tested at different temperatures. However, the thermal degradation kinetics shows more insight into the degradation pattern of the materials. The activation energy of degradation shows that the degradation of materials subjected to elevated conditions increases rapidly in the later stages of degradation, suggesting the formation of high char yield. The varying activation energy has been related to different degradation mechanisms. Lastly, the morphology of the materials was studied under SEM to understand the structural change in the material after tested in different weather conditions.

Highlights

  • In recent years, Carbon Fiber Reinforced Polymers (CFRP) have been widely used in aerospace applications

  • The properties of the CFRPs are based on both the polymers and the carbon fibers used as the reinforcement

  • In aerospace and naval application, the epoxy resins are commonly used as the matrix for preparing CFRP prepreg

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Summary

Introduction

Carbon Fiber Reinforced Polymers (CFRP) have been widely used in aerospace applications. They are advantageous over their metallic alloy counterparts owing to their mechanical properties and high strength to weight ratio. They have a low thermal expansion, high fatigue resistance, and good corrosion resistance under different environmental conditions [1]. The properties of the CFRPs are based on both the polymers and the carbon fibers used as the reinforcement. In aerospace and naval application, the epoxy resins are commonly used as the matrix for preparing CFRP prepreg (carbon fibers have excellent mechanical properties). They have an ultimate tensile strength and tensile modulus which are comparable with steel and aluminum and can exceed the Materials 2019, 12, 63; doi:10.3390/ma12010063 www.mdpi.com/journal/materials

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