Study on the thermal expansion properties of C/C composites
Source abstract
Abstract
Two different woven (2D and 3D) carbon/carbon composites (C/C) and a block carbon have been prepared by chemical vapor infiltration (CVI). The effects of the density and porosity of composites, preform architectures and heat treatment on the thermal expansion properties of the C/C composites were investigated. It is revealed that the coefficient of thermal expansion (CTE) of C/C composites is negative below 100 °C, and the CTE values are inversely proportion to its porosity. Comparing with 2D C/C composites, 3D C/C composites have a better thermal stability. Heat treatment can increase the thermal stability of composites by changing interfacial thermal stress. The thermal expansion behavior of C/C composites is considered as the result of interaction between fibers and matrix.
Source: openaire · Quality: candidate unverified · Source record ↗
Research context
OpenAlex topics: Advanced ceramic materials synthesis · Advanced materials and composites · Thermal properties of materials
SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.
References (6)
Show source-provided references
1. Xue H, Li H-J, Hou X-H et al (2004) New Carbon Mater (Chinese) 19(4):289
2. Siron O, Chollon G, Tsuda H, Yamauchi H, Maeda K, Kosaka K (2000) Carbon 38:136910.1016/S0008-6223(99)00270-5 ↗
3. Baxter RI, Rawlings RD, Iwashita N, Sawada Y (2000). Carbon 38:44110.1016/S0008-6223(99)00125-6 ↗
4. Oh SM, Lee JY (1988) Carbon 26:76910.1016/0008-6223(88)90098-X ↗
5. Li H-J, Hou X-H, Chen Y-X (2000) Carbon 38(3):42310.1016/S0008-6223(99)00122-0 ↗
6. Cheng L, Xu Y, Zhang L, Zhang Q (2002) Carbon 41:166610.1016/S0008-6223(03)00125-8 ↗