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Fabrication of fiber reinforced ceramic composites by chemical vapor infiltration

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TLDR
In this paper, the authors presented a process, fabricated hardware, and demonstrated on a laboratory scale a process which permits CVD infiltration of an SiC fibrous preform with either an Si/sub 3/N/sub 4 or SiC matrix in 2 to 12 hours.
Abstract
Ceramic fiber-ceramic matrix composites were prepared using the chemical vapor deposition (CVD) process. Our major goal of significantly reducing the infiltration times was accomplished. We have conceived a process, fabricated hardware, and demonstrated on a laboratory scale a process which permits CVD infiltration of an SiC fibrous preform with either an Si/sub 3/N/sub 4/ or SiC matrix in 2 to 12 h. The process should be applicable to infiltration of fibrous preforms prepared by slurry molding, stacking of layers of cloth, or filament winding. Two types of composites (SiC-Si/sub 3/N/sub 4/ and SiC-SiC) have been produced at densities of about 2.0 Mg/m/sup 3/ which was near the desired range. A scheme has also been conceived whereby the new infiltration process could be used for fabrication of tubes or hollow cylinders. This is an important advance since the ability to fabricate tubes or hollow cylinders would offer the hope that the process could be used for fabrication of toughened, high-strength heat exchanger tubes, heat engine cylinder liners and valve guides. 19 references, 7 figures, 1 table.

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Patent

Continuous fiber reinforced composites and methods, apparatuses, and compositions for making the same

TL;DR: In this article, a process for continuous composite coextrusion is described, which consists of forming a material-laden composition comprising a thermoplastic polymer and at least 40 volume % of a ceramic or metallic particulate in a manner such that the composition can be used as a substantially cylindrical feed rod, forming a hole down the symmetrical axis of the feed rod; inserting the start of a continuous spool of ceramic fiber, metal fiber or carbon fiber through the hole in the feed tube; extruding the feed rods and spool simultaneously to form a continuous filament consisting
Journal ArticleDOI

Fibre-matrix interphases and interfaces in ceramic matrix composites processed by CVI

TL;DR: In this paper, the fiber-matrix interfacial zone plays a key role in the mechanical behaviour of Si-C(O)/SiC inverse composites fabricated by chemical vapour infiltration (CVI) from ex-polycarbosilane Si-c(O) fibres precoated with pyrocarbon or boron nitride.
Patent

Apparatus for use with cvi/cvd processes

TL;DR: In this paper, a preheater for heating a reactant gas inside a CVI/CVD furnace and a fixture for depositing a matrix within a stack of porous structures by a pressure gradient CVI-CVD process is described.
Patent

Pressure gradient CVI/CVD apparatus, process, and product

TL;DR: In this article, the field of high temperature composites made by the chemical vapor infiltration and deposition of a binding matrix within a porous structure has been studied, particularly suited for the simultaneous CVI/CVD processing of large quantities (hundreds) of aircraft brake disks.
Journal ArticleDOI

Strength Distribution of Reinforcing Fibers in a Nicalon Fiber/Chemically Vapor Infiltrated Silicon Carbide Matrix Composite

TL;DR: The strength distribution of fibers within a two-dimensional laminate ceramic/ceramic composite consisting of an eight harness satin weave of Nicalon continuous fiber within a chemically vapor infiltrated SiC matrix was determined from analysis of the fracture mirrors of the fibers as discussed by the authors.
References
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Journal ArticleDOI

High-strength silicon carbide fibre-reinforced glass-matrix composites

TL;DR: In this article, two fiber forms, a 140 μm diameter monofilament and a 10μm diameter filamentary yarn, were incorporated into a matrix of borosilicate glass.
Journal ArticleDOI

Silicon carbide yarn reinforced glass matrix composites

TL;DR: Continuous silicon carbide fiber yarn has been used as a reinforcement for borosilicate and 96% silica glass matrices as discussed by the authors, and the resultant composites exhibit excellent levels of strength and elastic modulus up to temperatures of 600 ˚ C and 1100 ǫ C, respectively.
Journal ArticleDOI

Analysis of the Chemical Vapor Deposition of Titanium Diboride II . Modeling the Kinetics of Deposition

TL;DR: In this paper, a simple linear rate expression was used to calculate an activation energy of the chemical kinetic mechanism for the chemical vapor deposition (CVD) of from,, and was experimentally determined as a function of CVD variables.
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