Sealing role of Ti-rich phase in HfC-ZrC-TiC coating for C/C composites during ablation above 2100 °C

Traditional HfC, ZrC, and HfC-ZrC coatings cannot resist long-term ablation above 2100 °C because their oxides (HfO 2 and ZrO 2 ) express a loose structure and poor anti-oxygen infiltration ability after ablation. While Ti-rich oxides with a lower melting point can seal this loose structure during ablation. In this work, a HfC-ZrC-TiC multi-phases coating was proposed to solve the ablation failure problem of these coatings. It was prepared by supersonic atmospheric plasma spraying and tested by ablation with a heat flux of 2.38 MW/m 2 . With time ranging from 30 s to 120 s, the mass and linear ablation rates decreased from 0.85 mg/s to 0.18 mg/s and from 2.58 µm/s to 0.71 µm/s, respectively. All positive values indicated an increase in all coating thicknesses, so this coating can effectively protect C/C composites for more than 120 s. The surface of the coating was mainly composed of a loose oxide m-(Hf, Zr, Ti)O 2 skeleton within 120 s. As oxide skeletons had been gradually destroyed by mechanical denudation, the liquid phase of (Hf, Zr)TiO 4 was formed under oxide skeletons to fill pores. Then the surface of the oxide layer was dense after 120 s. The self-healing ability of the HfC-ZrC-TiC coating improved the ablation resistance of C/C composites above 2100 °C. • The HfC-ZrC-TiC coating can effectively protect C/C composites for more than 120 s during ablation above 2100 °C. • A loose oxide m-(Hf, Zr, Ti)O 2 skeleton was appeared and destroyed by mechanical denudation within 120 s. • The sealing role of Ti-rich phase ((Hf, Zr)TiO 4 ) can fill pores and cracks, so the coating was dense after 120 s.