Method for repairing ceramic matrix composite (CMC) articles

US10406640B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-10406640-B2
Application numberUS-201514974802-A
CountryUS
Kind codeB2
Filing dateDec 18, 2015
Priority dateDec 22, 2014
Publication dateSep 10, 2019
Grant dateSep 10, 2019

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Abstract

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A method for repairing a ceramic matrix composite (CMC) article including a ceramic material in a matrix including a metal alloy, wherein a localized region of the metal alloy has a defect. The method includes applying heat to the localized region for a time sufficient to increase the temperature of the metal alloy in the localized region above the melt temperature thereof and cause the metal alloy in the localized region to flow and seal the crack.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method comprising repairing a ceramic matrix composite (CMC) article comprising a reinforcing material in a matrix comprising a metal alloy, wherein at least one of a localized matrix region or a localized interphase region of the CMC article comprises a defect chosen from matrix cracking, debonding of the reinforcing material and the matrix, delamination of the reinforcing material and the matrix, and combinations thereof, the method comprising: heating the at least one localized region to increase the temperature of an interstitial metal alloy in the localized matrix region or localized interphase region to about 1400° C. to about 1700° C. to cause the interstitial metal alloy in the localized region to re-melt, flow and heal the defect. 2. The method of claim 1 , wherein the metal alloy is chosen from Si, B, Al, Y, Ti, Zr, oxides thereof, and mixtures and combinations thereof. 3. The method of claim 1 , wherein the reinforcing material is chosen from aluminum oxide (Al 2 O 3 ), mullite (Al 6 Si 2 O 13 ), zirconium oxide (ZrO 2 ), carbon (C), graphite, silicon carbide (SiC), silicon carbon nitride, silicon nitride, and mixtures and combinations thereof. 4. The method of claim 1 , wherein the reinforcing material comprises fibers. 5. The method of claim 1 , wherein the localized region is heated by at least one of a laser, an electric arc, an intense radiation source, electron beam, and a microwave generator. 6. The method of claim 1 , wherein the matrix material comprises Si and the reinforcing material comprises SiC fibers. 7. The method of claim 1 , wherein the article is in an inert atmosphere. 8. The method of claim 1 , wherein the article is at atmospheric pressure. 9. The method of claim 1 , further comprising cooling the article. 10. A method for repairing a ceramic matrix composite (CMC) article, wherein the article comprises: (a) a matrix material of a metal alloy selected from the group consisting of Si, B, Al, Y, Ti, Zr, oxides thereof, and mixtures and combinations thereof; and (b) a reinforcing material in the matrix material, wherein the reinforcing material comprises fibers selected from the group consisting of aluminum oxide (Al 2 O 3 ), mullite (Al 6 Si 2 O 13 ), zirconium oxide (ZrO 2 ), carbon (C), graphite, silicon carbide (SiC), silicon carbon nitride, silicon nitride, and mixtures and combinations thereof; the method comprising: applying heat to at least one of a localized matrix region or a localized interphase region of the article comprising a defect chosen from matrix cracking, debonding of the reinforcing material and the matrix, delamination of the reinforcing material and the matrix, and combinations thereof, wherein the heat is applied for a time sufficient cause the matrix material in the localized region to re-melt, flow and remediate the defect. 11. The method of claim 10 , wherein the heat is applied by at least one of a laser, an electric arc, an intense radiation source, electron beam, and microwave generator. 12. The method of claim 10 , wherein the heat is applied by at least one laser. 13. The method of claim 10 , wherein the matrix material comprises Si and the reinforcing material comprises woven SiC fibers, and wherein the matrix material in the localized region is heated to about 1400° C. to about 1700° C. 14. A method for repairing a ceramic matrix composite (CMC) article, wherein the article comprises a Si matrix material and a reinforcing material in the matrix material, wherein the reinforcing material comprises fibers chosen from aluminum oxide (Al 2 O 3 ), mullite (Al 6 Si 2 O 13 ), zirconium oxide (ZrO 2 ), carbon (C), graphite, silicon carbide (SiC), silicon carbon nitride, silicon nitride, and mixtures and combinations thereof; the method comprising: applying heat to at least one of a localized matrix region or a localized interphase region a of the article wherein at least one of the localized matrix region or the localized interface region comprise a defect chosen from matrix cracking, debonding of the reinforcing material and the matrix, delamination of the reinforcing material and the matrix, and combinations thereof, wherein the heat is applied for a time sufficient to cause interstitial matrix material in the localized region to re-melt and flow; and adding Si matrix material in the at least one localized matrix region or localized interface region, wherein the added Si matrix material is heated above the melt temperature thereof and flows into the localized region to remediate the defect. 15. The method of claim 14 , wherein the heat is applied by at least one of a laser, an electric arc, an intense radiation source, electron beam, and a microwave generator. 16. The method of claim 14 , wherein reinforcing material comprises woven SiC fibers, and wherein the Si matrix material in the localized region is heated to about 1400° C. to about 1700° C.

Assignees

Inventors

Classifications

  • Liquid infiltration of green bodies or pre-forms · CPC title

  • Silicon carbide · CPC title

  • Non-oxidic, e.g. borides, carbides, silicides or nitrides · CPC title

  • Zirconia · CPC title

  • Silica and alumina, including aluminosilicates, e.g. mullite · CPC title

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What does patent US10406640B2 cover?
A method for repairing a ceramic matrix composite (CMC) article including a ceramic material in a matrix including a metal alloy, wherein a localized region of the metal alloy has a defect. The method includes applying heat to the localized region for a time sufficient to increase the temperature of the metal alloy in the localized region above the melt temperature thereof and cause the metal a…
Who is the assignee on this patent?
Rolls Royce High Temperature Composites Inc
What technology area does this patent fall under?
Primary CPC classification B23P6/04. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Sep 10 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).