Abstract

The elevated temperature resistance and even fire resistance of carbon fiber-reinforced polymer composites were critical concerns in many applications. These properties of a carbon fiber-reinforced polymer depend not only on the degradation of the polymer matrix but also on that of the carbon fibers under elevated temperatures. In this study, influences of elevated temperatures (by 700°C for 30 min) in air on the mechanical properties and microstructures of a carbon fiber were investigated experimentally. It was found that the tensile strength and modulus as well as the diameters of the carbon fibers were reduced remarkably when the treatment temperatures exceeded 500°C. At the same time, the content of the structurally ordered carbonaceous components on the surface of carbon fibers and the graphite microcrystal size were reduced, while the graphite interlayer spacing ( d002) was enhanced. The deteriorated tensile modulus was attributed to the reduced graphite microcrystal size and the reduced thickness of the skin layer of the carbon fiber, while the degraded tensile strength was mainly attributed to the weakened cross-linking between the graphite planes.

Highlights

  • Carbon fiber–reinforced polymer (CFRP) composites are widely used in modern industries, such as aerospace, automobiles, and the rehabilitation of civil structures

  • This study focused on the effect of elevated temperatures on the mechanical and structural properties of the carbon fibers in air

  • Rs obtained from the Raman spectra reflects the ordering of crystallite structures of the skin of the carbon fiber, and La acquired from wide-angle X-ray diffraction (WAXD) represents the graphite crystallite plane width along the fiber axis direction

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Summary

Introduction

Carbon fiber–reinforced polymer (CFRP) composites are widely used in modern industries, such as aerospace, automobiles, and the rehabilitation of civil structures. The preferred orientation angle φ will be used to calculate the shear property (shear modulus GXY and shear stress τXY) between the graphite planes (see section “Correlation between the structures and the tensile properties”).

Results
Conclusion

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