Thermal fatigue behavior of C/C composites modified by SiC–MoSi2–CrSi2 coating

A SiC whisker reinforced high-temperature resistant phosphate adhesive for bonding carbon/carbon composites

“…Carbon/Carbon (C/C) composites have been widely studied as very promising high temperature structural materials due to their excellent properties such as low density, low coefficient of thermal expansion (CTE), good thermal shock resistance, high specific modulus and excellent mechanical properties at elevated temperature [1][2][3][4][5]. At present, C/C components with large sizes and complicate shapes are extensively used in the fields of aerospace, aviation and industry.…”

Improvement in thermal fatigue behavior of Si–Mo–Cr coated C/C composites through modification of the C/C-coating interface

“…Before thermal cycling, it can be seen that the coated samples without and with the transition layer all exhibit an obvious brittle fracture mode. After 15 thermal cycles in air, two kinds of coated C/C samples exhibit a bit pseudo-plastic fracture behavior [27]. Fig.…”

Double layer ZrSi2–ZrC–SiC/SiC oxidation protective coating for carbon/carbon composites

“…During thermal shock test, the interfaces between carbon fibres, pyrocarbon and coating is partially destroyed in the process of quick cooling from 1773 K to room temperature due to the mismatch of CTEs, resulting in the mechanical damage of the coated specimens. 24 Conclusion A double layer ZrSi 2 -ZrC-SiC/SiC coating has been prepared on the surface of C/C composites by a two-step pack cementation method. The isothermal oxidation resistance of the coating at 1173 and at 1773 K in air and thermal shock test were investigated.…”