Fabrication of high heat capacity ceramic matrix composite aircraft brakes using spark plasma sintering
US-2021101842-A1 · Apr 8, 2021 · US
US12071383B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-12071383-B2 |
| Application number | US-202117302009-A |
| Country | US |
| Kind code | B2 |
| Filing date | Apr 21, 2021 |
| Priority date | Apr 21, 2021 |
| Publication date | Aug 27, 2024 |
| Grant date | Aug 27, 2024 |
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A method for forming a high temperature coating includes forming a pre-sintered ceramic coating on a ceramic composite substrate. The pre-sintered ceramic coating includes a plurality of ceramic particles. The method further includes sintering at least a portion of the pre-sintered ceramic coating by heating the portion of the pre-sintered ceramic coating to a sintering temperature of the plurality of ceramic particles using joule heating. The sintering temperature is greater than about 1000 degrees Celsius (° C.).
Opening claim text (preview).
What is claimed is: 1. A method, comprising: forming a pre-sintered ceramic coating on a ceramic composite substrate, wherein the pre-sintered ceramic coating comprises a plurality of ceramic particles; contacting at least a portion of the pre-sintered ceramic coating with one or more contact electrical elements; delivering an electrical current through the one or more contact electrical elements to the ceramic composite substrate; and sintering at least the portion of the pre-sintered ceramic coating by heating the portion of the pre-sintered ceramic coating to a sintering temperature of the plurality of ceramic particles using joule heating induced in the ceramic composite substrate by the delivery of the electrical current through the one or more contact electrical elements to the ceramic composite substrate, wherein the sintering temperature is greater than about 1000 degrees Celsius (° C.). 2. The method of claim 1 , further comprising: contacting the portion of the pre-sintered ceramic coating with one or more contact heating elements; and powering the one or more contact heating elements to heat the portion of the pre-sintered ceramic coating. 3. The method of claim 2 , wherein the one or more contact heating elements comprise one or more high temperature electrode heating elements. 4. The method of claim 2 , further comprising moving the pre-sintered ceramic coating relative to the one or more contact heating elements to cause the one or more contact heating elements to contact a different portion of the pre-sintered ceramic coating. 5. The method of claim 2 , further comprising compressing the portion of the pre-sintered ceramic coating while heating the portion of the pre-sintered ceramic coating. 6. The method of claim 5 , wherein compressing the portion of the pre-sintered ceramic coating comprises compressing the portion of the pre-sintered ceramic using a roller, wherein the method further comprises advancing the roller to heat another portion of the pre-sintered ceramic coating. 7. The method of claim 1 , wherein the plurality of ceramic particles comprises at least one of a carbide ceramic, a boride ceramic, or a nitride ceramic. 8. The method of claim 1 , wherein the plurality of ceramic particles comprises a rare earth disilicate ceramic. 9. The method of claim 1 , further comprising forming a crystallized metal carbide undercoat on a surface of the ceramic composite substrate. 10. The method of claim 1 , wherein forming the pre-sintered ceramic coating further comprises applying a ceramic mixture on a surface of the ceramic composite substrate, wherein the ceramic mixture includes the plurality of ceramic particles.
Local sintering, e.g. laser sintering · CPC title
Total pressure below 1 atmosphere, e.g. vacuum · CPC title
Carbides · CPC title
Silicates other than clay, e.g. water glass · CPC title
for obtaining at least two superposed coatings having different compositions · CPC title
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