Composites of carbon fiber-reinforced silicon carbide (Cf/SiC) with ultra-high temperature ceramics (UHTCs) exhibit superior resistance to oxidation and ablation under high temperatures. Components in large-scale applications often have complex geometries, making it crucial to understand the oxidation and ablation behaviors of curved and non-uniform surfaces. In this study, a Cf/SiC-ZrB2 composite was fabricated into a 300 mm cylindrical shape using filament winding and liquid silicon infiltration processes. The resulting specimens exhibited a uniform microstructure, with SiC and ZrB2 crystals evenly distributed across the top and bottom surfaces, demonstrating the feasibility of producing large-scale composites. The specimens underwent an oxyacetylene torch test at 2,100 K for 5 min to assess their ablation and oxidation performance. The results revealed significant variation in the oxide layer due to the non-flat surface, with the layer thickness gradually decreasing as the oblique angle was reduced. Additionally, the presence of high-melting-point ZrO2 in the oxide layer near the torch center was attributed to the migration and solidification of molten SiO2. This suggests that large and complex Cf/SiC incorporating UHTCs can effectively form a protective oxide layer, even under conditions where SiO2 displacement occurs. The findings underscore the importance of integrating geometric considerations into the design of ultra-high temperature ceramic composites to achieve the thermal and ablation resistance required for advanced high-temperature applications.