Preparation and Characterization of SiO2/Carbon Foam and SIC/Carbon Foam Composites

被引:0
|
作者
Wu Xiao-Dong [1 ,2 ]
Shao Gao-Feng [1 ,2 ]
Cui Sheng [1 ,2 ]
Wang Ling [3 ]
Shen Xiao-Dong [1 ,2 ]
机构
[1] Nanjing Tech Univ, Coll Mat Sci & Engn, State Key Lab Mat Oriented Chem Engn, Nanjing 210009, Jiangsu, Peoples R China
[2] Nanjing Tech Univ Suqian, AdvMat Inst, Nanjing, Jiangsu, Peoples R China
[3] AVIC Composite Corp Ltd, Natl Key Lab Adv Composite, Beijing 101300, Peoples R China
关键词
carbon foam; SiO2; silicon carbide; thermal stability; thermal conductivity; compressive strength; MESOPOROUS SILICON-CARBIDE; LOW THERMAL-CONDUCTIVITY; CARBON FOAMS; AEROGEL; TEMPERATURE; FABRICATION; PYROLYSIS; RESIN;
D O I
暂无
中图分类号
O61 [无机化学];
学科分类号
070301 ; 081704 ;
摘要
The synthesis and characterization of carbon foam supported silica aerogel (SiO2/Carbon foam) and silicon carbide composite (SiC/Carbon foam) are presented in this study. The phase composition, microstructure, thermal and mechanical properties are investigated by XRD, SEM, LFA Laser Flashmeasurements, and Universal Material Testing.The resulting SiO2/Carbon foam composite shows a higher compressive strength (14.95 MPa) and a smaller thermal conductivity (0.44 W .m(-1).K-1) at room temperature, in comparison with the pristine carbon foam. The SiC/Carbon foam composite maintains a compressive strength of 14.66 MPa, and possesses a low high-temperature thermal conductivity (2.18 W.m(-1).K-1 at 1 200 degrees C). Mass loss does not begin until 610 degrees C for the SiC/Carbon foam composite, and complete carbon combustion does not occur until 844 degrees C, indicating a much better thermal stability than the pristine carbon foam in oxidizing atmosphere.
引用
收藏
页码:1252 / 1260
页数:9
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