Method to process a ceramic matrix composite (CMC) with a protective ceramic coating

US11787159B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-11787159-B2
Application numberUS-202117229154-A
CountryUS
Kind codeB2
Filing dateApr 13, 2021
Priority dateApr 19, 2017
Publication dateOct 17, 2023
Grant dateOct 17, 2023

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  7. Citations and related patents

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Abstract

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A method of producing a ceramic matrix composite including a protective ceramic coating thereon comprises applying a surface slurry onto an outer surface of an impregnated fiber preform. The surface slurry includes particulate ceramic solids dispersed in a flowable preceramic polymer comprising silicon, and the impregnated fiber preform comprises a framework of ceramic fibers loaded with particulate matter. The flowable preceramic polymer is cured, thereby forming on the outer surface a composite layer comprising a cured preceramic polymer with the particulate ceramic solids dispersed therein. The cured preceramic polymer is then pyrolyzed to form a porous ceramic layer comprising silicon carbide, and the impregnated fiber preform and the porous ceramic layer are infiltrated with a molten material comprising silicon. After infiltration, the molten material is cooled to form a ceramic matrix composite body with a protective ceramic coating thereon.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method of producing a ceramic matrix composite having a protective ceramic coating, the method comprising: applying a first surface slurry onto an outer surface of an impregnated fiber preform comprising a framework of ceramic fibers loaded with particulate matter, the first surface slurry comprising particulate ceramic solids dispersed in a solvent; drying the first surface slurry to form a dried porous layer comprising the particulate ceramic solids; infiltrating a flowable preceramic polymer comprising silicon into the dried porous layer; curing the flowable preceramic polymer to form a composite layer on the outer surface, the composite layer comprising a cured preceramic polymer with the particulate ceramic solids dispersed therein; pyrolyzing the cured preceramic polymer to form a porous ceramic layer comprising silicon carbide on the outer surface; applying a second surface slurry onto the porous ceramic layer to fill cracks formed during pyrolysis, the second surface slurry comprising ceramic particles dispersed in an aqueous or organic solvent; drying the second surface slurry to form a surface layer on the porous ceramic layer; infiltrating the impregnated fiber preform, the porous ceramic layer, and the surface layer with a molten material comprising silicon; and after infiltration with the molten material, cooling the molten material to form a ceramic matrix composite body with a protective ceramic coating thereon and with a densified surface layer on the protective ceramic coating, wherein the densified surface layer comprises a higher amount of residual silicon than the protective ceramic coating. 2. The method of claim 1 , wherein curing the flowable preceramic polymer comprises heating at a temperature in a range from about 150° C. to about 400° C., and wherein the pyrolyzing comprises heating the composite layer to a temperature in a range from about 850° C. to about 1300° C. 3. The method of claim 2 , wherein the curing further comprises applying pressure. 4. The method of claim 1 , wherein the flowable preceramic polymer comprises an organosilicon polymer and/or an inorganic silicon polymer. 5. The method of claim 1 , wherein the flowable preceramic polymer has a viscosity in a range from about 10 cp to about 1000 cp. 6. The method of claim 1 , wherein the porous ceramic layer includes other ceramic phases in addition to silicon carbide. 7. The method of claim 1 , further comprising machining the surface layer prior to the infiltration. 8. The method of claim 1 , wherein the surface layer has a thickness from about 0.03 mm to about 0.3 mm. 9. The method of claim 1 , wherein the surface layer and the porous ceramic layer together have a thickness from about 0.08 mm to about 1.3 mm. 10. The method of claim 1 , wherein the second surface slurry comprises a solids loading from about 10 vol. % to about 70 vol. %. 11. The method of claim 1 , wherein the ceramic particles comprise silicon carbide and/or silicon nitride, and wherein the second surface slurry further comprises one or more reactive elements selected from the group consisting of: graphite, diamond, carbon black, molybdenum, and tungsten. 12. The method of claim 11 , wherein the densified surface layer comprises: ceramic reaction products from reactions between the molten material and the one or more reactive elements in the surface layer; and the silicon carbide and any other ceramic phases present in the surface layer prior to the infiltration. 13. The method of claim 1 , wherein the densified surface layer has a multilayer structure comprising sublayers with different residual silicon contents. 14. The method of claim 1 , further comprising, prior to applying the first surface slurry to the outer surface of the impregnated fiber preform, placing a carbon fiber mat onto the outer surface. 15. The method of claim 1 , further comprising, prior to the infiltration, machining the porous ceramic layer. 16. The method of claim 1 , wherein the ceramic matrix composite body comprises silicon carbide fibers embedded in a silicon carbide matrix, and wherein the protective ceramic coating comprises silicon carbide with 20 vol. % or less residual silicon. 17. A method of producing a ceramic matrix composite having a protective ceramic coating, the method comprising: applying a first surface slurry onto an outer surface of an impregnated fiber preform comprising a framework of ceramic fibers loaded with particulate matter, the first surface slurry comprising particulate ceramic solids dispersed in a solvent; drying the first surface slurry to form a dried porous layer comprising the particulate ceramic solids; infiltrating a flowable preceramic polymer comprising silicon into the dried porous layer; curing the flowable preceramic polymer to form a composite layer on the outer surface, the composite layer comprising a cured preceramic polymer with the particulate ceramic solids dispersed therein; pyrolyzing the cured preceramic polymer to form a porous ceramic layer comprising silicon carbide on the outer surface; applying a second surface slurry onto the porous ceramic layer to fill cracks formed during pyrolysis, the second surface slurry comprising ceramic particles dispersed in an aqueous or organic solvent; drying the second surface slurry to form a surface layer on the porous ceramic layer; infiltrating the impregnated fiber preform, the porous ceramic layer, and the surface layer with a molten material comprising silicon; and after infiltration with the molten material, cooling the molten material to form a ceramic matrix composite body with a protective ceramic coating thereon and with a densified surface layer on the protective ceramic coating, wherein the densified surface layer has a multilayer structure comprising sublayers with different residual silicon contents. 18. A method of producing a ceramic matrix composite having a protective ceramic coating, the method comprising: applying a first surface slurry onto an outer surface of an impregnated fiber preform comprising a framework of ceramic fibers loaded with particulate matter, the first surface slurry comprising particulate ceramic solids dispersed in a solvent comprising water, ethanol, methanol, isopropyl alcohol, methyl ethyl ketone, and/or toluene; drying the first surface slurry to evaporate the solvent and form a dried porous layer comprising the particulate ceramic solids; infiltrating a flowable preceramic polymer comprising silicon into the dried porous layer; curing the flowable preceramic polymer to form a composite layer on the outer surface, the composite layer comprising a cured preceramic polymer with the particulate ceramic solids dispersed therein; pyrolyzing the cured preceramic polymer to form a porous ceramic layer comprising silicon carbide on the outer surface; infiltrating the impregnated fiber preform and the porous ceramic layer on the outer surface thereof with a molten material comprising silicon; and after infiltration with the molten material, cooling the molten material to form a ceramic matrix composite body with a protective ceramic coating thereon.

Assignees

Inventors

Classifications

  • B32B18/00Primary

    Layered products essentially comprising ceramics, e.g. refractory products · CPC title

  • based on non-oxide ceramics · CPC title

  • based on carbon, e.g. graphite · CPC title

  • based on silicon carbide · CPC title

  • obtained from {Si-containing} polymer precursors {or organosilicon monomers} · CPC title

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What does patent US11787159B2 cover?
A method of producing a ceramic matrix composite including a protective ceramic coating thereon comprises applying a surface slurry onto an outer surface of an impregnated fiber preform. The surface slurry includes particulate ceramic solids dispersed in a flowable preceramic polymer comprising silicon, and the impregnated fiber preform comprises a framework of ceramic fibers loaded with partic…
Who is the assignee on this patent?
Rolls Royce High Temperature Composites Inc
What technology area does this patent fall under?
Primary CPC classification B32B18/00. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Oct 17 2023 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 2 related publications on this page (citations in our corpus or others sharing the same primary CPC).