Boron nitride aerogel interface coating precursor for ceramic matrix composites

US12157704B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-12157704-B2
Application numberUS-202218084932-A
CountryUS
Kind codeB2
Filing dateDec 20, 2022
Priority dateDec 20, 2022
Publication dateDec 3, 2024
Grant dateDec 3, 2024

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Abstract

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A method of forming a ceramic matrix composite (CMC) comprises applying a boron nitride (BN) aerogel to a fibrous material to form a pretreated fibrous material, depositing, using chemical vapor infiltration (CVI), a BN interface coating (IFC) on the pretreated fibrous material, and depositing a matrix on the BN IFC and the pretreated fibrous material.

First claim

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The invention claimed is: 1. A method of forming a ceramic matrix composite (CMC), the method comprising: applying a boron nitride (BN) aerogel to a fibrous material to form a pretreated fibrous material; depositing, using chemical vapor infiltration (CVI), a BN interface coating (IFC) on the pretreated fibrous material; and depositing a matrix on the BN IFC and the pretreated fibrous material. 2. The method of claim 1 , wherein the step of applying the BN aerogel comprises: immersing the fibrous material in a bath of water and hexagonal BN (h-BN) to form a slurry-coated fibrous material; and freeze-drying the slurry coated fibrous material. 3. The method of claim 2 , wherein the fibrous material comprises a sheet of ceramic fibers. 4. The method of claim 3 , wherein the step of immersing the fibrous material comprises: pulling the sheet through the bath of water and h-BN under tension. 5. The method of claim 3 and further comprising: forming a pre-preg sheet by injecting the sheet with a polymer resin and curing the sheet. 6. The method of claim 5 , wherein the polymer resin comprises one of polyvinyl alcohol and polyvinyl butyral. 7. The method of claim 5 and further comprising: forming plies from the pre-preg sheet; and laying up the plies into a preform. 8. The method of claim 7 and further comprising: prior to depositing the BN IFC, consolidating the BN aerogel by heating the preform to a temperature ranging from 1200° C. to 1500° C. 9. The method of claim 2 , wherein the fibrous ceramic material comprises a preform. 10. The method of claim 9 and further comprising: prior to depositing the BN IFC, consolidating the BN aerogel by heating the preform to a temperature ranging from 1200° C. to 1500° C. 11. The method of claim 2 , wherein the fibrous material comprises an individual tow. 12. The method of claim 11 , wherein the step of immersing the fibrous material comprises: pulling the tow through the bath of water and h-BN under tension. 13. The method of claim 12 and further comprising: sizing the tow; and weaving the tow into a sheet. 14. The method of claim 13 and further comprising: forming plies from the sheet; and laying up the plies into a preform. 15. The method of claim 14 and further comprising: prior to depositing the BN IFC, consolidating the BN aerogel by heating the preform to a temperature ranging from 1200° C. to 1500° C. 16. The method of claim 2 , wherein the BN aerogel comprises BN nanotubes and BN nanosheets. 17. The method of claim 2 , wherein the BN IFC comprises h-BN. 18. The method of claim 2 , wherein the step of depositing the matrix comprises at least one of chemical vapor infiltration, slurry infiltration, melt infiltration, and polymer infiltration and pyrolysis. 19. The method of claim 2 , wherein the matrix comprises silicon carbide (SiC). 20. The method of claim 2 and further comprising: prior to the step of depositing the matrix, depositing, using CVI, an oxidation resistant coating on the pretreated fibrous material, the oxidation resistant coating comprising at least one of silicon-doped BN, SiC, and carbon.

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What does patent US12157704B2 cover?
A method of forming a ceramic matrix composite (CMC) comprises applying a boron nitride (BN) aerogel to a fibrous material to form a pretreated fibrous material, depositing, using chemical vapor infiltration (CVI), a BN interface coating (IFC) on the pretreated fibrous material, and depositing a matrix on the BN IFC and the pretreated fibrous material.
Who is the assignee on this patent?
Raytheon Tech Corp, Rtx Corp
What technology area does this patent fall under?
Primary CPC classification C04B35/62868. Mapped technology areas include Chemistry & Metallurgy.
When was this patent published?
Publication date Tue Dec 03 2024 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 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).