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Ceramic matrix composite

About: Ceramic matrix composite is a research topic. Over the lifetime, 7807 publications have been published within this topic receiving 117020 citations.


Papers
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Journal ArticleDOI
TL;DR: In this paper, a ZrC-SiC matrix was fabricated by means of a liquid precursor conversion method, using an organic zirconium-containing polymeric precursor and polycarbosilane.

46 citations

Journal ArticleDOI
TL;DR: In this paper, a double-layer SiC fiber reinforced composite with ZMI-SiCf/Si3N4 as lossy layer and SLF-SLF-SLCF/SLCN 4 as impedance matching layer has been constructed via the chemical vapor infiltration method.

46 citations

Journal ArticleDOI
TL;DR: In this paper, a numerical approach was developed to simulate the mechanism of matrix crack deflection at the fiber/matrix interface in brittle matrix composites, and the fracture behavior of a unit cell (microcomposite) consisting of a single fibre surrounded by a cylindrical tube of matrix was studied with the help of a finite element model.
Abstract: This paper describes a numerical approach developed to simulate the mechanism of matrix crack deflection at the fibre/matrix interface in brittle matrix composites. For this purpose, the fracture behaviour of a unit cell (microcomposite) consisting of a single fibre surrounded by a cylindrical tube of matrix was studied with the help of a finite element model. A fracture mechanics approach was used to design a criterion for deflection at the fibre/matrix interface of an annular crack present in the matrix. The analysis of the fracture behaviour of SiC/SiC and SiC/glass ceramics microcomposites shows that the introduction of a low modulus and low toughness interfacial layer at the fibre/matrix interface (e.g. a carbon coating) greatly favours matrix crack deflection at the interphase/fibre interface.

46 citations

Patent
18 Jul 1985
TL;DR: A thin, refractory, intermediate adhesive layer of laminar structure is deposited in oriented fashion on the reinforcing fibers by chemical vapor deposition, this intermediate layer having a greater elongation at break than the matrix and having a thickness of between 0.2 and 3 micrometers.
Abstract: A thin, refractory, intermediate adhesive layer of laminar structure is deposited in oriented fashion on the reinforcing fibers by chemical vapor deposition, this intermediate layer having a greater elongation at break than the matrix and having a thickness of between 0.2 and 3 micrometers; the material forming the intermediate layer can be laminar pyrocarbon or boron nitride; the ceramic matrix is then infiltered, preferably by chemical vapor deposition, inside the pores of the reinforcement.

46 citations

Journal ArticleDOI
TL;DR: In this paper, a spark plasma sintering (SPS) technique was used to improve the mechanical properties of the HA-Yttria stabilized zirconia (YSZ) composites.

46 citations


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Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202394
2022236
2021300
2020344
2019433
2018354