Thanks to their low density, good thermal, mechanical and tribological properties, composites made of carbon fibres and carbon matrix (C/C) are particularly adapted to the manufacturing of aircraft brake discs. Several methods have been developed to improve their performance. For instance, the introduction of silicon carbide within the matrix notably increases the friction coefficient. While carbon fibres enhance the toughness of the matrix, silicon carbide shows high hardness, thermal stability and low chemical reactivity, leading to superior friction properties. The purpose of the present study was to evaluate the influence of such matrix modification on the friction behaviour and to identify the related mechanisms. With C/C as a reference, four different hybrid matrix composites were elaborated. For the first one, the matrix consisted in carbon (C) and silicon carbide (SiC), deposited in alternated layers around the fibres. For the second one, it was constituted of C, SiC and free silicon (Si), randomly distributed. For the third one, the matrix was made of SiC only. For the fourth one, it was similar to the third one but with some additional free Si. These samples were submitted to structural and mechanical characterization, then to friction and wear tests using a pin-on-disc tribometer, at variable temperatures and humidity. Compared to C/C, they exhibited higher friction coefficients and wear rates, in line with the abrasive capacity of silicon carbide. For severe conditions, the friction coefficient sometimes dropped abruptly, through the occurrence of a mechanism close to lubrication. These results highlight both mechanical and physico-chemical effects of silicon carbide on the tribological properties of hybrid matrix composites at various energies. Finally, the influence of some free silicon within the matrix was discussed.
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