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Patent

Process of producing ceramic matrix composites

TLDR
In this article, a process for producing a silicon-containing CMC article that exhibits improved physical, mechanical, and microstructural properties at elevated temperatures exceeding the melting point of silicon is described.
Abstract
A process for producing a silicon-containing CMC article (10) that exhibits improved physical, mechanical, and microstructural properties at elevated temperatures exceeding the melting point of silicon. The process entails producing a body containing a ceramic reinforcement material (14,16) in a solid matrix that comprises solid elemental silicon and/or silicon alloy and a ceramic matrix material (18). The ceramic matrix composite article (10) is produced by at least partially removing the solid elemental silicon and/or silicon alloy from the solid matrix and optionally reacting at least part of the solid elemental silicon and/or silicon alloy in the solid matrix to form one or more refractory materials. The solid elemental silicon and/or silicon alloy is sufficiently removed from the body to enable the ceramic matrix composite article (10) to structurally and chemically withstand temperatures above 1405°C.

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Citations
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Patent

Process of producing ceramic matrix composites and ceramic matrix composites formed thereby

TL;DR: In this paper, a process for producing a silicon-containing CMC article is described, which involves depositing one or more coating layers on silicon carbide (SiC) fibers, drawing the coated SiC fibers through a slurry to produce slurry-coated fiber material, and then processing the slurrycoated SiC fiber material to form unidirectional prepreg tapes.
Patent

Ceramic matrix composite turbine engine

TL;DR: In this article, a transition section for a turbine engine is provided that includes one or more components constructed of a ceramic matrix composite, fluidly connecting a high pressure turbine and a low-pressure turbine within the gas turbine engine.
Patent

Method of producing a melt-infiltrated ceramic matrix composite article

TL;DR: A process for producing silicon-containing CMC articles is described in this paper, where a fiber reinforcement material is impregnated with the slurry composition to yield a preform, which is then heated to form a porous preform that contains the SiC matrix and porosity.
Patent

Non-Integral Turbine Blade Platforms and Systems

TL;DR: In this article, a turbine blade platform may be disposed between two turbine blades and the platform may include a first exterior side configured to interface with a first turbine blade and a second exterior side disposed generally opposite the first turbine side.
Patent

Methods and materials for forming in-situ cavities for silicon-based ceramic matrix composite components

TL;DR: In this paper, the authors described methods and materials for forming in-situ features in a ceramic matrix composite component with cooling features, which comprises forming a preform tape, laying up said preform to a desired shape, placing a high-temperature resistant fugitive material insert of preselected geometry in the preform template, compacting the pre-form template of the desired shape and burning out the template.
References
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Patent

Fiber-containing composite

TL;DR: In this paper, the mixture is formed into a preform which is infiltrated with a molten solution of boron and silicon producing a composite containing borone nitride coated fibrous material.
Patent

Article and method for making complex shaped preform and silicon carbide composite by melt infiltration

TL;DR: In this article, small diameter silicon carbide-containing fibers are provided in a bundle such as a fiber tow that can be formed into a structure where the radii of curvature is not limited to 10-20 inches.
Patent

Ceramic matrix composite and method of manufacturing the same

TL;DR: In this paper, a method of manufacturing fiber composite ceramic is presented, in which large number of BN-coated SiC fibers are gathered to form yarns, or yarns are woven to form a two-dimensional or three-dimensional fabric, and a preform is formed by the yarns or the fabric, a molten Si is impregnated into the compact to form an SiC matrix between fibers.
Patent

Filament-containing composite

TL;DR: In this paper, Boron nitride is coated on filaments of elemental carbon and/or silicon carbide, the coated filaments are contacted with an infiltration-promoting material containing elemental carbon to produce a preform wherein the filament are substantially parallel and each filament is enveloped with infiltrate-promote material.
Patent

Method of making a ceramic composite by infiltration of a ceramic preform

TL;DR: In this article, a method for making a composite ceramic article by infiltration of a sintered ceramic preform with an infiltrate phase is presented, where a silicon carbide preform is first infiltrated with carbon to coat the lamelli of the preform, then the carbon is infiltrated with molten silicon, whereby the molten silicon and carbon react to form silicon carbides in the interlamellar regions.