Ceramic component
US-2015045200-A1 · Feb 12, 2015 · US
US10472713B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10472713-B2 |
| Application number | US-201615168268-A |
| Country | US |
| Kind code | B2 |
| Filing date | May 31, 2016 |
| Priority date | May 31, 2016 |
| Publication date | Nov 12, 2019 |
| Grant date | Nov 12, 2019 |
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A method of fabricating a ceramic matrix composite includes infiltrating pores of a porous structure with a preceramic matrix polymer using a composite molding technique. The porous structure includes fibers and an exposed carbon coating on the fibers. The preceramic matrix polymer wets the exposed carbon coating. The preceramic matrix polymer is then pyrolyzed to convert the preceramic matrix polymer to a ceramic matrix.
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What is claimed is: 1. A method of fabricating a ceramic matrix composite, the method comprising: infiltrating pores of a porous structure with a preceramic matrix polymer using a composite molding technique, the porous structure including fibers and an exposed carbon coating on the fibers, the preceramic matrix polymer wetting the exposed carbon coating wherein the exposed carbon coating is discontinuous and has a thickness of less than approximately 10 nanometers; and pyrolyzing the preceramic matrix polymer to convert the preceramic matrix polymer to a ceramic matrix. 2. The method as recited in claim 1 , wherein the ceramic matrix has residual pores, and further comprising infiltrating the residual pores with preceramic infiltration polymer and pyrolyzing the preceramic infiltration polymer to convert the preceramic infiltration polymer to additional ceramic matrix. 3. The method as recited in claim 1 , wherein the fibers have a fiber diameter D and the exposed carbon coating has a thickness T, and a ratio of D/T is in a range of 20000-100. 4. The method as recited in claim 3 , wherein the range is 15000-200. 5. The method as recited in claim 3 , wherein the ratio is greater than or equal to 20000-10000. 6. The method as recited in claim 1 , wherein the fibers are silicon carbide fibers. 7. The method as recited in claim 1 , wherein the exposed carbon coating includes graphite. 8. A method of fabricating a ceramic matrix composite, the method comprising: modifying a wetting property between a preceramic matrix polymer and fibers of a porous structure by providing an exposed carbon coating on the fibers, wherein the wetting property controls a pore structure of the preceramic matrix polymer once pyrolyzed to convert the preceramic matrix polymer to a ceramic matrix and wherein the exposed carbon coating is discontinuous and has a thickness of less than approximately 10 nanometers; infiltrating pores of the porous structure with the preceramic matrix polymer, the preceramic matrix polymer wetting the carbon coating according to the modified wetting property; and pyrolyzing the preceramic matrix polymer to convert the preceramic matrix polymer to the ceramic matrix that has the pore structure according to the modified wetting property. 9. The method as recited in claim 8 , wherein the modifying of the wetting property includes decreasing wetting. 10. The method as recited in claim 8 , wherein the ceramic matrix has residual pores, and further comprising infiltrating the residual pores with preceramic infiltration polymer and pyrolyzing the preceramic infiltration polymer to convert the preceramic infiltration polymer to additional ceramic matrix. 11. The method as recited in claim 8 , wherein the fibers have a fiber diameter D and the exposed carbon coating has a thickness T, and a ratio of D/T is in a range of 20000-100. 12. The method as recited in claim 11 , wherein the ratio is greater than or equal to 20000-1000.
Liquid infiltration of green bodies or pre-forms · CPC title
Coatings characterised by their thickness · CPC title
with a discontinuous coating layer · CPC title
by wet chemical techniques · CPC title
Carbon · CPC title
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