TY - JOUR
T1 - Feasibility and ablation behavior of on-site HfSi2and HfSi2–HfO2repair coatings on C/C–SiC–ZrC composites
AU - Hu, Kaiyue
AU - Deng, Juanli
AU - Mao, Yuhao
AU - Kou, Sijie
AU - Wang, Botao
AU - Fan, Shangwu
N1 - Publisher Copyright:
© 2025 Elsevier Ltd and Techna Group S.r.l. All rights are reserved, including those for text and data mining, AI training, and similar technologies.
PY - 2025/12
Y1 - 2025/12
N2 - Protective coatings are indispensable for thermal protection systems, but damage during installation and service is often unavoidable. To restore the protective function of C/C–SiC–ZrC composites, an on-site repair strategy was developed using a non-sintered repair coating composed of polysilazane and HfSi2 particles. According to GJB323A-96 Standard with heat fluxes of 2.38 MW/m2, the ablation tests were investigated. Short-term exposure (10 s) induced the rapid oxidation of HfSi2, forming a dense HfO2 layer that sealed the surface and effectively hindered oxygen ingress. After 120 s, the repaired samples showed negative linear and mass ablation rates (−0.99 ± 0.07 μm/s and −0.50 ± 0.05 mg/s, respectively), indicating that the repaired coating still provided effective protection for the substrate. In contrast, uncoated composites suffered severe ablation with rates of 0.80 ± 0.17 μm/s and 1.00 ± 0.08 mg/s. Notably, the ablation rate of the repair coating was comparable to that of the in-situ coating, confirming the effectiveness of the proposed on-site repair strategy. Meanwhile, the HfSi2–HfO2 repair coating prepared through compositional and structural optimization further reduced the discrepancy between linear and mass ablation rates, confirming the effectiveness and reproducibility of the repair strategy.
AB - Protective coatings are indispensable for thermal protection systems, but damage during installation and service is often unavoidable. To restore the protective function of C/C–SiC–ZrC composites, an on-site repair strategy was developed using a non-sintered repair coating composed of polysilazane and HfSi2 particles. According to GJB323A-96 Standard with heat fluxes of 2.38 MW/m2, the ablation tests were investigated. Short-term exposure (10 s) induced the rapid oxidation of HfSi2, forming a dense HfO2 layer that sealed the surface and effectively hindered oxygen ingress. After 120 s, the repaired samples showed negative linear and mass ablation rates (−0.99 ± 0.07 μm/s and −0.50 ± 0.05 mg/s, respectively), indicating that the repaired coating still provided effective protection for the substrate. In contrast, uncoated composites suffered severe ablation with rates of 0.80 ± 0.17 μm/s and 1.00 ± 0.08 mg/s. Notably, the ablation rate of the repair coating was comparable to that of the in-situ coating, confirming the effectiveness of the proposed on-site repair strategy. Meanwhile, the HfSi2–HfO2 repair coating prepared through compositional and structural optimization further reduced the discrepancy between linear and mass ablation rates, confirming the effectiveness and reproducibility of the repair strategy.
KW - Ablation resistance
KW - C/C-ZrC-SiC composites
KW - HfSiand HfSi–HfOrepair coatings
KW - On-site repair coatings
KW - Oxyacetylene flame test
KW - Reactive melt infiltration (RMI)
UR - https://www.scopus.com/pages/publications/105025559303
U2 - 10.1016/j.ceramint.2025.11.231
DO - 10.1016/j.ceramint.2025.11.231
M3 - 文章
AN - SCOPUS:105025559303
SN - 0272-8842
VL - 51
SP - 65537
EP - 65550
JO - Ceramics International
JF - Ceramics International
IS - 30
ER -