TY - JOUR
T1 - Effects of different loading methods on thermal expansion behaviors of 2D cross-ply carbon/carbon composites from 850°C to 2300°C
AU - Luo, Wenfei
AU - Fu, Yewei
AU - Zhang, Shouyang
AU - Li, Hejun
AU - Cheng, Jing
AU - Xue, Lizhen
PY - 2014/9
Y1 - 2014/9
N2 - 2D cross-ply carbon/carbon (C/C) composites were prepared by isothermal chemical vapor infiltration (ICVI) process. Thermal expansion behaviors of 2D cross-ply C/C composites and effects of static loading and fatigue loading conditions on coefficient of thermal expansion (CTE) of the C/C composites from 850°C to 2300°C were studied. In static test cases, different damage levels were produced inside samples by displacement-controlled three-point bending loading. Meanwhile, flexural fatigue experiments were conducted under stress level of 70%, cycling numbers (N) of 105 and 106 at a sinusoidal loading frequency of 15 Hz. Afterwards, the thermal expansion behaviors were investigated. It showed that CTE of the C/C composites after static loading and fatigue loading had a decrease compared with CTE of the as-prepared C/C composites. After static loading, there was a larger decrease in CTE for the C/C composites with more severe damage levels. Moreover, the influence of damage on CTE reached to the greatest at around 1550°C. The largest decline percentage of the C/C composites after static loading and fatigue loading was 30% and 85% in contrast to the as-prepared C/C composites, respectively. In addition, weakening interfacial strength of the C/C composites was the main effect on the large decrease of CTE after the fatigue loading.
AB - 2D cross-ply carbon/carbon (C/C) composites were prepared by isothermal chemical vapor infiltration (ICVI) process. Thermal expansion behaviors of 2D cross-ply C/C composites and effects of static loading and fatigue loading conditions on coefficient of thermal expansion (CTE) of the C/C composites from 850°C to 2300°C were studied. In static test cases, different damage levels were produced inside samples by displacement-controlled three-point bending loading. Meanwhile, flexural fatigue experiments were conducted under stress level of 70%, cycling numbers (N) of 105 and 106 at a sinusoidal loading frequency of 15 Hz. Afterwards, the thermal expansion behaviors were investigated. It showed that CTE of the C/C composites after static loading and fatigue loading had a decrease compared with CTE of the as-prepared C/C composites. After static loading, there was a larger decrease in CTE for the C/C composites with more severe damage levels. Moreover, the influence of damage on CTE reached to the greatest at around 1550°C. The largest decline percentage of the C/C composites after static loading and fatigue loading was 30% and 85% in contrast to the as-prepared C/C composites, respectively. In addition, weakening interfacial strength of the C/C composites was the main effect on the large decrease of CTE after the fatigue loading.
KW - C. Fatigue
KW - C. Thermal expansion
KW - C/C composites
KW - Damage
UR - http://www.scopus.com/inward/record.url?scp=84903884300&partnerID=8YFLogxK
U2 - 10.1016/j.ceramint.2014.03.098
DO - 10.1016/j.ceramint.2014.03.098
M3 - 文章
AN - SCOPUS:84903884300
SN - 0272-8842
VL - 40
SP - 12545
EP - 12551
JO - Ceramics International
JF - Ceramics International
IS - 8 PART A
ER -