TY - JOUR
T1 - The improvement on ablative properties of 1D high thermal conductivity carbon/carbon composites by constructing heterogeneous layered preforms
AU - Wang, Guanyu
AU - Zhang, Ruoxi
AU - Yang, Mohan
AU - Ding, Siyuan
AU - Yang, Yuyang
AU - Song, Qiang
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 - 2025/11
Y1 - 2025/11
N2 - The 1D C/C reinforced by intermediate-phase pitch-based carbon fibers (CFMP) has high thermal conductivity along the fiber direction, enabling rapid heat dissipation, which is crucial for enhancing the ablation resistance of C/C composites. However, the low mechanical properties between the bundles increase the risk of exfoliation damage. To address this issue, this work proposes introducing plain PAN-based carbon fiber (CFPAN) cloth into the 1D CFMP preform to construct CFPAN and CFMP heterogeneous layered preforms. A comparative study on the properties of C/C composites with different layups reveals that when the layup was CFPAN/CFMP/CFMP, the inter-bundle bending strength and interlaminar shear strength increased by 174.53 % and 10.86 %. Meanwhile, the thermal conductivities reached 361.54 W/(m‧K) and 18.23 W/(m‧K) in the in-plane and out-of-plane directions, achieving a good balance between mechanical and thermal properties. Consequently, the composite exhibited optimal ablation resistance: the linear ablation rate and mass ablation rate were 0.74 mg/s and 3.3 μm/s after 60 s of ablation, 68.8 % and 34.3 % lower than those of 1D C/C, respectively, and the ablation surface temperature was only 2053 °C. The analysis suggests that the significantly improved ablation performance is mainly attributed to the enhanced interlaminar shear strength and efficient in-plane heat dissipation. This work provides guidance for preparing high performance ablation-resistant and high thermal conductivity C/C composites.
AB - The 1D C/C reinforced by intermediate-phase pitch-based carbon fibers (CFMP) has high thermal conductivity along the fiber direction, enabling rapid heat dissipation, which is crucial for enhancing the ablation resistance of C/C composites. However, the low mechanical properties between the bundles increase the risk of exfoliation damage. To address this issue, this work proposes introducing plain PAN-based carbon fiber (CFPAN) cloth into the 1D CFMP preform to construct CFPAN and CFMP heterogeneous layered preforms. A comparative study on the properties of C/C composites with different layups reveals that when the layup was CFPAN/CFMP/CFMP, the inter-bundle bending strength and interlaminar shear strength increased by 174.53 % and 10.86 %. Meanwhile, the thermal conductivities reached 361.54 W/(m‧K) and 18.23 W/(m‧K) in the in-plane and out-of-plane directions, achieving a good balance between mechanical and thermal properties. Consequently, the composite exhibited optimal ablation resistance: the linear ablation rate and mass ablation rate were 0.74 mg/s and 3.3 μm/s after 60 s of ablation, 68.8 % and 34.3 % lower than those of 1D C/C, respectively, and the ablation surface temperature was only 2053 °C. The analysis suggests that the significantly improved ablation performance is mainly attributed to the enhanced interlaminar shear strength and efficient in-plane heat dissipation. This work provides guidance for preparing high performance ablation-resistant and high thermal conductivity C/C composites.
KW - Ablative properties
KW - C/C composites
KW - Heterogeneous layered preforms
KW - Mechanical properties
UR - https://www.scopus.com/pages/publications/105017592340
U2 - 10.1016/j.ceramint.2025.09.285
DO - 10.1016/j.ceramint.2025.09.285
M3 - 文章
AN - SCOPUS:105017592340
SN - 0272-8842
VL - 51
SP - 55651
EP - 55663
JO - Ceramics International
JF - Ceramics International
IS - 27
ER -