Authors: S. Rajesh, B. Vijaya Ramnath, C. Elanchezhian, C. Kavin, S. Sathish
Abstract: Silicon Carbide/GFRP reinforced matrix composite and SiC matrix composite has been developed by using hand layup and resin casting methods respectively. The GFRP reinforced polymer composite is made by sandwiching two layers of GFRP in between the SiC material. The resin used for the preparation the samples are epoxy and polyester, for both SiC/GFRP composite and SiC composite. An Arcan fixture with butterfly specimen is used to measure the fracture occurring in various modes of the polymer composite. The objective of the proposed testing method is to determine the variation in the stress value depending on the resin material as well as the influence of GFRP in the strength of SiC polymer composite. Results from the tests are analyzed to show that the epoxy resin is better for tensile strength, in both Sic/GFRP reinforced and SiC composite material.
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Authors: B. Vijaya Ramnath, S. Rajesh, Chinnadurai Elanchezhian, V. Vignesh, V. Vijai Rahul, V. Tamilselvan, S.U. Sathya Narayanan
Abstract: Silicon Carbide/GFRP reinforced matrix composite and SiC matrix composite has been developed by using hand layup and resin casting methods respectively. The GFRP reinforced polymer composite is made by sandwiching two layers of GFRP in between the SiC material. The resin used for the preparation the samples are epoxy and polyester, for both Sic/GFRP composite and SiC composite. An Arcan fixture with butterfly specimen is used to measure the fracture occurring in various modes of the polymer composite. The objective of the proposed testing method is to determine the variation in the stress value depending on the resin material as well as the influence of GFRP in the strength of SiC polymer composite. Results from the tests are analyzed to show that the polyester resin is better for shear strength, in both Sic/GFRP reinforced and SiC composite material.
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Authors: H. Moriyasu, J. Kita, H. Suemasu, Ian J. Davies, S. Koda, K. Itatani
Abstract: The effect of surface modified Si-Al-C® fibre with carbon interface (SA/C fibre) addition
on the densification of silicon carbide (SiC) composite was examined. An acid treatment (H2SO4
and HNO3) was carried out at 50°C for 3 h in order to add COO- group to the surface of SA/C fibre
and to enhance the dispersibility of SA/C fibre in the SiC powder due to the mixing operation in the
polar solvent. Commercially available ultrafine SiC powder (specific surface area: 47.5 m2∙g-1) was
mixed with acid-treated SA/C fibre and sintering aid (4.8 mass% Al4C3 and 1.2 mass% B4C) in the
presence of acetone. The relative density of the SiC composite with non-acid-treated SA/C fibre
addition hot-pressed at 1800°C for 1 h in Ar atmosphere under a pressure of 62 MPa was 98.4%,
whereas that of the SiC composite with acid-treated SA/C fibre addition increased to 98.7%.
Furthermore, the fracture toughness increased from 5.6 MPa∙m1/2 to 7.0 MPa∙m1/2 for the
acid-treated SA/C fibre addition.
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Authors: Zhen Lin Lu, Zhi Guo Xing, Hui Xie, Yong Xin Zhou
Abstract: The effect of SiC particles sizes on erosion wear behaviour of SiC/epoxy resin composite was studied on self-made slurry erosion wear tester. The results show that the erosion wear rate of SiC/epoxy resin composite would be decreased with the increase of SiC particle sizes. With the increase of impact angle, the erosion wear rate would be increased first, and then decreased, it would be peak value when the erosion wear test was carried out at 60° impact angle. When SiC particles were mixed with different sizes, the erosion wear rate of SiC/epoxy resin composite would be lowest. The erosion wear mechanism of SiC/epoxy resin composite was analyzed by observation of worn surface morphology.
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Abstract: Planning for a U.S. test blanket module to operate in the internationally-sponsored ITER
reactor has focused attention on the many coating and compatibility issues that will need to be
solved before fusion energy moves from concept to commercial reality. Examples are given for (1)
a dual-layer, electrically-resistant coating as a potential solution to reduce the
magnetohydrodynamic pressure drop with liquid Li and (2) materials compatibility issues with
eutectic Pb-Li for conventional alloys and SiC/SiC composites. Because of the reduced activity of
Li in Pb-Li, a wider range of functional materials can be considered in this system. Nevertheless, an
Al2O3 scale on FeCrAl was transformed to LiAlO2
after exposure to Pb-Li at 800°C.
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Authors: Marcio Florian, Rodrigo Fernando Costa Marques, Luiz Eduardo Carvalho, Carlos Alberto Alves Cairo, Nilso Barelli
Abstract: SiC fiber-reinforced SiC matrix composite (SiCf/SiC) is one of the leading candidates in
ceramic materials for engineering applications due to its unique combination of properties such as
high thermal conductivity, high resistance to corrosion and working conditions. Fiber-reinforced
composites are materials which exhibit a significant improvement in properties like ductility in
comparison to the monolithic SiC ceramic. The SiCf/SiC composite was obtained from a C/C
composite precursor using convertion reaction under high temperature and controlled atmosphere.
In this work, SiC phase presented the stacking faults in the structure, being not possible to calculate
the unit cell size, symmetry and bond lengths but it seem equal card number 29-1129 of JCPDS.
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Authors: Katsumi Yoshida, Hideki Matsumoto, Masamitsu Imai, Kazuaki Hashimoto, Yoshitomo Toda, Toyohiko Yano
Abstract: In this study, Tyranno SA fiber cloth was coated with carbon black and SiC powder
containing sintering aids by means of electrophoretic deposition method, and SiC/SiC composites
with three different fiber volume fractions were fabricated using the Tyranno SA cloth by
hot-pressing at 1700oC. The sufficient formation of the SiC matrix between each fiber could be
observed. The composite fractured in non-brittle manner, and bending strength decreased with
increasing fiber volume fraction. The crack propagation and fracture behavior depended on the fiber
volume fraction. These differences in bending strength and fracture behavior would be caused by
the difference in the interfacial bonding between fiber cloth and the matrix.
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