TY - JOUR
T1 - Research on continuous fiber reinforced silicon carbide composites
AU - Xu, Yongdong
AU - Cheng, Laifei
AU - Zhang, Litong
AU - Yin, Hongfeng
PY - 2002/4
Y1 - 2002/4
N2 - Silicon carbide textile composites reinforced with continuous carbon and silicon carbide fiber were fabricated by chemical vapor infiltration. The densities of C/SiC composites and SiC/SiC composites after the 30 h infiltration are 2.1 g·cm-3 and 2.5 g·cm-3 respectively. The flexural strength values of C/SiC composites and SiC/SiC composites are 450 MPa and 860 MPa respectively, which are not reduced as the temperature is increased from room temperature to 1600°C. Accordingly, the fracture toughness values are 20 MPa·m1/2 and 41.5 MPa·m1/2, the fracture work values are 10 kJ·m-2 and 28.1 kJ·m-2, and the dynamic impact fracture toughness values are 62.0 kJ·m-2 and 36.0 kJ·m-2, respectively. After thermal shock tests between 300°C and 1300°C for 50 times, the flexural strength is retained by 96.4%. It is indicated that the thermal shock is not a controlling factor for the failure of C/SiC and SiC/SiC materials. Compared with C/SiC composites, SiC/SiC composites exhibit superior oxidation resistance. Especially, both C/SiC and SiC/SiC thruster chambers have successfully passed the test of rocket engine.
AB - Silicon carbide textile composites reinforced with continuous carbon and silicon carbide fiber were fabricated by chemical vapor infiltration. The densities of C/SiC composites and SiC/SiC composites after the 30 h infiltration are 2.1 g·cm-3 and 2.5 g·cm-3 respectively. The flexural strength values of C/SiC composites and SiC/SiC composites are 450 MPa and 860 MPa respectively, which are not reduced as the temperature is increased from room temperature to 1600°C. Accordingly, the fracture toughness values are 20 MPa·m1/2 and 41.5 MPa·m1/2, the fracture work values are 10 kJ·m-2 and 28.1 kJ·m-2, and the dynamic impact fracture toughness values are 62.0 kJ·m-2 and 36.0 kJ·m-2, respectively. After thermal shock tests between 300°C and 1300°C for 50 times, the flexural strength is retained by 96.4%. It is indicated that the thermal shock is not a controlling factor for the failure of C/SiC and SiC/SiC materials. Compared with C/SiC composites, SiC/SiC composites exhibit superior oxidation resistance. Especially, both C/SiC and SiC/SiC thruster chambers have successfully passed the test of rocket engine.
KW - Carbon/silicon carbide composites
KW - Ceramic matrix composites
KW - Chemical vapor infiltration
KW - Silicon carbide/silicon carbide composites
UR - https://www.scopus.com/pages/publications/0036526403
M3 - 文章
AN - SCOPUS:0036526403
SN - 0454-5648
VL - 30
SP - 184
EP - 188
JO - Kuei Suan Jen Hsueh Pao/Journal of the Chinese Ceramic Society
JF - Kuei Suan Jen Hsueh Pao/Journal of the Chinese Ceramic Society
IS - 2
ER -