Nanocomposite TiBCN coatings are promising advanced materials owing to their high hardness, wear resistance, and corrosion resistance. This study investigated the thermal stability and oxidation resistance of a TiB0.19C0.37N0.44 coating deposited on WC-Co cemented carbide by chemical vapor deposition (CVD). The as-deposited TiB0.19C0.37N0.44 coating consisted of nanocrystalline Ti(C,N) and Ti(B,C) phases embedded in an amorphous CN/BN matrix. The incorporation of B atoms into the TiCN coating induced the formation of stacking faults, and the hardness of the TiB0.19C0.37N0.44 coating reached 39.1 GPa. The coating maintained its original phase structure after vacuum annealing at temperatures up to 1200 °C. At 1300 °C, B atoms reacted with the WC-Co substrate to form the CoWB phase. With increasing vacuum annealing temperature, the coating hardness decreased continuously. This behavior is attributed to stress release, grain coarsening, B atom diffusion, and degradation of the nanocomposite structure. During oxidation, the coating exhibited a relatively slow oxidation rate at 600–700 °C. However, after oxidation at 800 °C, the reaction of C and B atoms with oxygen led to the formation and volatilization of CO and B2O3, generating pores and microcracks. In summary, the TiB0.19C0.37N0.44 coating maintains a stable phase structure after vacuum annealing below 1300 °C, whereas it undergoes complete oxidation after air annealing at 900 °C. These findings indicate that the TiB0.19C0.37N0.44 coating possesses considerable potential for high-temperature cutting applications.
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