Tailoring microstructures of carbon fiber reinforced carbon aerogel-like matrix composites by carbonization to modulate their mechanical properties and thermal conductivities

The microstructure evolution of carbon fiber reinforced carbon aerogel-like matrix (C/CA) composites with carbonization temperature and its influence on their properties were investigated. The removal of residual organo-functional groups of the C/CA precursors is dominant when carbonized at 600-750 degrees C with a large volume shrinkage difference by 17-22% as compared to that at 1200 degrees C, while the rearrangement of novolac structures is dominant at 900-1200 degrees C with a slight volume shrinkage fluctuation of 6%. Resultantly, the amount of micropore first increases and then decreases, while the particle size experiences an opposite change. The microstructure correspondingly transforms from a completely amorphous state to a partially amorphous state with graphite crystallites in low-angle misorientation, and then with graphite-like entangling ribbons. Due to the reduced residual tensile stress and increased interfacial bonding, the resulting composites with a variable bulk density of 0.58-0.64 g cm-3 have much higher compressive strengths of 45.8-96.9 MPa than other reported carbon foams or aerogels with similar bulk densities. The increase of strength and modulus with carbonization temperature is mainly due to the smaller tensile stress, higher particle packing compactness, larger microcrystallite size and less residual organo-functional groups. The composites also present a relatively low thermal conductivity of 0.12-0.59 W m-1 K-1. The increase of thermal conductivity with temperature is related to the synergistic effect of reduced phonon scattering associated with smaller specific surface area, larger microcrystallite size and less organo-functional groups and improved phonon transfer associated with increased interparticle contact area.

Automated summary

This study investigates the microstructure evolution of carbon fiber reinforced carbon aerogel-like matrix composites and its influence on their properties. The results show that the carbonization temperature affects the volume shrinkage, micropore amount, particle size, and microstructure of the composites. The resulting composites exhibit higher compressive strengths and low thermal conductivity compared to other reported carbon foams or aerogels with similar bulk densities. The increase in strength and modulus with carbonization temperature is attributed to reduced tensile stress, improved particle packing compactness, larger microcrystallite size, and less residual organo-functional groups.