TY - JOUR
T1 - Study on the ablation performance of SiC-coated high thermal conductivity three-dimensional C/C composites
AU - Zhang, Ruoxi
AU - Song, Qiang
AU - Li, Jingtong
AU - Zhou, Zhaofan
AU - Zhao, Yuanxiao
AU - Huang, Liye
AU - Li, Wei
AU - Shen, Qingliang
AU - Li, Hejun
N1 - Publisher Copyright:
© 2024 Elsevier Ltd
PY - 2024/6
Y1 - 2024/6
N2 - Carbon/carbon composites were prepared by densifying a three-dimensional preform made of mesophase pitch-based carbon fiber woven fabric lamination and PAN-based carbon fiber z-pin. Afterwards, SiC coating was prepared on them by pack cementation, and their ablation performances were investigated. Results show that the stacked of pitch-based carbon fiber woven fabrics in Z direction induces a high thermal conductivity of composites in in-plane direction and a sawtooth-structured surface of SiC coating, which helps to decrease the surface temperature (from 1778 to 1614 ℃) and the thermal stress of coating during ablation. Thus, a greatly improved ablation resistance is obtained for the coating in the X-Z plane, showing a mass ablation rate of − 0.01 mg/s and a linear ablation rate of − 0.12 µm/s, respectively, 90.9% and 105.2% lower than that of the X-Y plane. Our findings can provide a meaningful way for the development of high-performance ablation-resistant C/C composites.
AB - Carbon/carbon composites were prepared by densifying a three-dimensional preform made of mesophase pitch-based carbon fiber woven fabric lamination and PAN-based carbon fiber z-pin. Afterwards, SiC coating was prepared on them by pack cementation, and their ablation performances were investigated. Results show that the stacked of pitch-based carbon fiber woven fabrics in Z direction induces a high thermal conductivity of composites in in-plane direction and a sawtooth-structured surface of SiC coating, which helps to decrease the surface temperature (from 1778 to 1614 ℃) and the thermal stress of coating during ablation. Thus, a greatly improved ablation resistance is obtained for the coating in the X-Z plane, showing a mass ablation rate of − 0.01 mg/s and a linear ablation rate of − 0.12 µm/s, respectively, 90.9% and 105.2% lower than that of the X-Y plane. Our findings can provide a meaningful way for the development of high-performance ablation-resistant C/C composites.
KW - Ablation performance
KW - C/C composites
KW - High thermal conductivity
KW - SiC coating
UR - http://www.scopus.com/inward/record.url?scp=85181937380&partnerID=8YFLogxK
U2 - 10.1016/j.jeurceramsoc.2023.12.079
DO - 10.1016/j.jeurceramsoc.2023.12.079
M3 - 文章
AN - SCOPUS:85181937380
SN - 0955-2219
VL - 44
SP - 3797
EP - 3808
JO - Journal of the European Ceramic Society
JF - Journal of the European Ceramic Society
IS - 6
ER -