Ceramic matrix composite and method and article of manufacture

US10370301B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10370301-B2
Application numberUS-201414210928-A
CountryUS
Kind codeB2
Filing dateMar 14, 2014
Priority dateMar 15, 2013
Publication dateAug 6, 2019
Grant dateAug 6, 2019

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  1. Title

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  2. Abstract

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  5. First independent claim

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Abstract

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A ceramic matrix composite having improved operating characteristics includes a barrier layer.

First claim

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What is claimed is: 1. A ceramic matrix composite comprising: a matrix; and a fiber preform embedded within the matrix; wherein the matrix includes a rigidization layer comprising silicon carbide on the fiber preform, an infiltration layer on the rigidization layer, and a barrier layer sandwiched between the rigidization layer and the infiltration layer, the barrier layer comprising silicon nitro-carbide or silicon nitride. 2. The ceramic matrix composite of claim 1 wherein the ceramic matrix composite material has a porosity of less than about 5 volume percent of the total ceramic matrix composite. 3. The ceramic matrix composite of claim 1 wherein the fiber preform comprises silicon carbide or silicon nitro-carbide fibers, and further comprising a fiber interface coating between the fiber preform and the rigidization layer, the fiber interface coating comprising boron nitride or pyrolytic carbon. 4. The ceramic matrix composite of claim 1 wherein the barrier layer has a thickness of between about 0.1 μm and about 10 μm. 5. The ceramic matrix composite of claim 1 wherein the barrier layer has a thickness of between about 1 μm and about 2 μm. 6. The ceramic matrix composite of claim 1 wherein the barrier layer comprises between about 2 volume percent and about 10 volume percent of the total ceramic matrix composite. 7. The ceramic matrix composite of claim 1 wherein the barrier layer comprises a combination barrier layer including an underlayer comprising the silicon nitro-carbide or silicon nitride and an overlayer comprising pyrolytic carbon. 8. The ceramic matrix composite of claim 1 wherein the barrier layer comprises silicon-nitro-carbide and pyrolytic carbon. 9. The ceramic matrix composite of claim 1 wherein the fiber preform comprises about 15 volume percent to about 45 volume percent of the total ceramic matrix composite; and wherein the rigidization layer comprises between about 15 volume percent and about 40 volume percent of the total ceramic matrix composite. 10. The ceramic matrix composite of claim 1 wherein the preform comprises fiber formed from a compound selected from the group consisting of: silicon-carbide and silicon nitro-carbide; and wherein the ceramic matrix composite further comprises a fiber interface coating generally encapsulating the fiber, the fiber interface coating comprising between about 0.1 volume percent and about 10 volume percent of the total ceramic matrix composite; and wherein the fiber interface coating is deposited by chemical vapor infiltration and comprises one or more compounds selected from the group consisting of: boron nitride and pyrolytic carbon. 11. The ceramic matrix composite of claim 1 wherein the infiltration layer comprises slurry additives and melt additives; wherein the slurry additives comprise silicon-carbide particulates and the melt additives comprise silicon; wherein the slurry additives comprise between about 10 volume percent and about 55 volume percent of the total ceramic matrix composite; and wherein the melt additives comprise between about 5 volume percent and about 20 volume percent of the total ceramic matrix composite; wherein the rigidization layer comprises a silicon-carbide layer deposited by chemical vapor infiltration; wherein the barrier layer is deposited by chemical vapor infiltration; wherein the preform comprises fibers selected from the group consisting of: silicon-carbide fibers, silicon-nitro-carbide fibers, carbon fibers, and oxide ceramic fibers; and wherein the fibers are selected from the group consisting of: stoichiometric fibers, non-stoichiometric fibers, and a combination of stoichiometric fibers and non-stoichiometric fibers. 12. An article of manufacture made of a ceramic matrix composite comprising a matrix; and a fiber preform embedded within the matrix; wherein the matrix includes a rigidization layer comprising silicon carbide on the fiber preform, an infiltration layer on the rigidization layer, and a barrier layer sandwiched between the rigidization layer and the infiltration layer, the barrier layer comprising silicon nitro-carbide or silicon nitride.

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What does patent US10370301B2 cover?
A ceramic matrix composite having improved operating characteristics includes a barrier layer.
Who is the assignee on this patent?
Rolls Royce Corp
What technology area does this patent fall under?
Primary CPC classification C04B35/806. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Aug 06 2019 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).