TY - JOUR
T1 - Ablation behavior of the ZrC coating on C/C composite with the construction of thermal dispersal network
AU - Zhong, Lei
AU - Guo, Lingjun
AU - Huang, Jinguo
AU - Liu, Ningkun
AU - Li, Yunyu
AU - Li, Hejun
N1 - Publisher Copyright:
© 2022
PY - 2023/5/1
Y1 - 2023/5/1
N2 - In this work, the coating and the matrix are connected as a whole by the continuous fibers. To achieve this goal, the C/C composite with carbon fibers in its surface region is prepared by the directional deposition of pyrolytic carbon (PyC). Compared with the conventional C/C composite that has a porous structure in the whole bulk, the as-prepared composite has a higher efficiency of polymer infiltration and pyrolysis (PIP) process (an improvement of about 88%). The carbon fiber network would provide the thermal channels for the coating during the ablation, which would reduce the ablation temperature (a decrease of about 180 °C) and thermal gradient in the coating, and then the thermal stress would decrease during the ablation, showing the good anti-ablation performance (the linear ablation rate of which is about 68.4% and 39.7% lower than pure C/C composite and conventional C/C-ZrC composite).
AB - In this work, the coating and the matrix are connected as a whole by the continuous fibers. To achieve this goal, the C/C composite with carbon fibers in its surface region is prepared by the directional deposition of pyrolytic carbon (PyC). Compared with the conventional C/C composite that has a porous structure in the whole bulk, the as-prepared composite has a higher efficiency of polymer infiltration and pyrolysis (PIP) process (an improvement of about 88%). The carbon fiber network would provide the thermal channels for the coating during the ablation, which would reduce the ablation temperature (a decrease of about 180 °C) and thermal gradient in the coating, and then the thermal stress would decrease during the ablation, showing the good anti-ablation performance (the linear ablation rate of which is about 68.4% and 39.7% lower than pure C/C composite and conventional C/C-ZrC composite).
KW - Ablation
KW - C-reinforced ZrC coating
KW - Carbon-carbon composites
KW - Chemical vapor deposition
KW - Thermal stress
UR - https://www.scopus.com/pages/publications/85145694669
U2 - 10.1016/j.ceramint.2022.12.270
DO - 10.1016/j.ceramint.2022.12.270
M3 - 文章
AN - SCOPUS:85145694669
SN - 0272-8842
VL - 49
SP - 13903
EP - 13915
JO - Ceramics International
JF - Ceramics International
IS - 9
ER -