TY - JOUR
T1 - Effect of matrix gas phase deposition cycles on the microstructure and properties of 2D C/SiC
AU - Luan, Xin'gang
AU - Tian, Min
AU - Xu, Xingya
AU - Cheng, Laifei
AU - Riedel, Ralf
PY - 2014/1/10
Y1 - 2014/1/10
N2 - Effects of processing on the microstructure and property of carbon fiber reinforced silicon carbide matrix composites, namely 2D C/SiC composites, have been investigated with respect to micro-crack evolution, strength change and mass loss, etc. Several 2D C/SiC materials prepared with different chemical vapour infiltration (CVI) cycles of SiC were studied. Raman spectroscopy was employed to measure the residual stress in the matrix of the C/SiC composite based on the shift of the position of the LO band of SiC. Two kinds of mircocracks were found during the preparation of C/SiC. One type of cracks originating from the corners of braided holes barely changes during the whole processing, the other type arising between the braided holes decreases with increasing matrix volume. The former is most responsible for carbon fibers oxidation at elevated temperature. The evaluation of the microstructure and properties of the material is discussed in terms of the internal stress changed with the deposition of the matrix.
AB - Effects of processing on the microstructure and property of carbon fiber reinforced silicon carbide matrix composites, namely 2D C/SiC composites, have been investigated with respect to micro-crack evolution, strength change and mass loss, etc. Several 2D C/SiC materials prepared with different chemical vapour infiltration (CVI) cycles of SiC were studied. Raman spectroscopy was employed to measure the residual stress in the matrix of the C/SiC composite based on the shift of the position of the LO band of SiC. Two kinds of mircocracks were found during the preparation of C/SiC. One type of cracks originating from the corners of braided holes barely changes during the whole processing, the other type arising between the braided holes decreases with increasing matrix volume. The former is most responsible for carbon fibers oxidation at elevated temperature. The evaluation of the microstructure and properties of the material is discussed in terms of the internal stress changed with the deposition of the matrix.
KW - A. Ceramic-matrix composites (CMCs)
KW - B. Matrix cracking
KW - C. Crack
KW - D. Scanning electron microscopy (SEM)
KW - E. Chemical vapour infiltration (CVI)
UR - http://www.scopus.com/inward/record.url?scp=84888311071&partnerID=8YFLogxK
U2 - 10.1016/j.compscitech.2013.11.001
DO - 10.1016/j.compscitech.2013.11.001
M3 - 文章
AN - SCOPUS:84888311071
SN - 0266-3538
VL - 90
SP - 117
EP - 122
JO - Composites Science and Technology
JF - Composites Science and Technology
ER -