TY - JOUR
T1 - Morphology-driven Cu gradient distribution induces varied anti-ablation performance in C/C–ZrC composites
AU - Sun, Yingjun
AU - Guo, Lingjun
AU - Zhang, Xin
AU - Liu, Huimin
AU - Zhang, Yi
AU - Li, Hejun
AU - Yin, Xuemin
N1 - Publisher Copyright:
© 2025 Elsevier Ltd.
PY - 2026/2
Y1 - 2026/2
N2 - Conventional carbon/carbon-zirconium carbide (C/C–ZrC) composites, though promising for ultra-high-temperature applications, often struggle to balance active cooling and passive oxidation protection, as uncontrolled metal redistribution during service leads to structural instability and premature ablation failure. In this study, copper (Cu) gradient-modified C/C–ZrC composites were fabricated via reactive melt infiltration (RMI) using a layered powder-laying strategy with Cu powders of distinct morphologies to achieve programmable Cu distribution. Two opposite gradient architectures were designed: a Cu-decreasing (ZCI) and a Cu-increasing (ZCS) configuration along the infiltration direction. Microstructural and ablation analyses revealed that the Cu gradient markedly altered the infiltration-reaction pathway and ZrC grain evolution. In ZCS prepared with spherical Cu powders, a dissolution-recipitation mechanism generated fine spherical ZrC grains and a Cu-rich basal layer that sustained heat absorption and conduction, forming a dense bilayer ZrO2 structure that effectively suppressed oxygen diffusion. Benefiting from this architecture, the ZCS composite exhibited the lowest mass ablation rate of −0.39 mg/s under a 4.18 MW/m2 oxy-acetylene flame for 30 s, along with superior surface integrity and thermal stability. This work establishes a direct mechanistic link between Cu gradient architecture and ablation resistance, providing a controllable design paradigm for next-generation active-passive synergistic thermal protection systems.
AB - Conventional carbon/carbon-zirconium carbide (C/C–ZrC) composites, though promising for ultra-high-temperature applications, often struggle to balance active cooling and passive oxidation protection, as uncontrolled metal redistribution during service leads to structural instability and premature ablation failure. In this study, copper (Cu) gradient-modified C/C–ZrC composites were fabricated via reactive melt infiltration (RMI) using a layered powder-laying strategy with Cu powders of distinct morphologies to achieve programmable Cu distribution. Two opposite gradient architectures were designed: a Cu-decreasing (ZCI) and a Cu-increasing (ZCS) configuration along the infiltration direction. Microstructural and ablation analyses revealed that the Cu gradient markedly altered the infiltration-reaction pathway and ZrC grain evolution. In ZCS prepared with spherical Cu powders, a dissolution-recipitation mechanism generated fine spherical ZrC grains and a Cu-rich basal layer that sustained heat absorption and conduction, forming a dense bilayer ZrO2 structure that effectively suppressed oxygen diffusion. Benefiting from this architecture, the ZCS composite exhibited the lowest mass ablation rate of −0.39 mg/s under a 4.18 MW/m2 oxy-acetylene flame for 30 s, along with superior surface integrity and thermal stability. This work establishes a direct mechanistic link between Cu gradient architecture and ablation resistance, providing a controllable design paradigm for next-generation active-passive synergistic thermal protection systems.
KW - Ablation behavior
KW - C/C composites
KW - Gradient structure
KW - Layered powder-laying strategy
KW - Reactive melt infiltration
UR - https://www.scopus.com/pages/publications/105021868784
U2 - 10.1016/j.carbon.2025.121063
DO - 10.1016/j.carbon.2025.121063
M3 - 文章
AN - SCOPUS:105021868784
SN - 0008-6223
VL - 247
JO - Carbon
JF - Carbon
M1 - 121063
ER -