Ceramic matrix composite including silicon carbide fibers in a ceramic matrix comprising a max phase compound
A ceramic matrix composite includes continuous silicon carbide fibers in a ceramic matrix comprising silicon carbide and a MAX phase compound having a chemical composition M n+1 AX n , where M is a transition metal selected from the group consisting of: Ti, V, Cr, Sc, Zr, Nb, Mo, Hf, and Ta; A is a group-A element selected from the group consisting of: Al, Si, P, S, Ga, Ge, As, Cd, In, Sn, Tl and Pb; and X is carbon or nitrogen, with n being an integer from 1 to 3.
1. A ceramic matrix composite comprising:
a ceramic matrix including silicon carbide and a MAX phase compound having a chemical composition M n+1 AX n , where
M is selected from the group consisting of: Ti, V, Cr, Sc, Zr, Nb, Mo, Hf, and Ta,
A is selected from the group consisting of: Al, Si, P, S, Ga, Ge, As, Cd, In, Sn, Tl and Pb,
X is carbon or nitrogen, and
n is an integer from 1 to 3; and
continuous silicon carbide fibers in the ceramic matrix,
wherein the MAX phase compound is present in the ceramic matrix at a concentration of at least about 30 wt. %.
2. The ceramic matrix composite of claim 1 , wherein the concentration of the MAX phase compound is from about 60 wt. % to about 99 wt. %.
3. The ceramic matrix composite of claim 1 , wherein the MAX phase compound is selected from the group consisting of: Ti 2 CdC, Sc 2 InC, Ti 2 GaC, Ti 2 InC, Ti 2 TlC, V 2 AlC, V 2 GaC, Cr 2 GaC, Ti 2 AlN, Ti 2 GaN, Ti 2 InN, V 2 GaN, Cr 2 GaN, Ti 2 GeC, Ti 2 SnC, Ti 2 PbC, V 2 GeC, Cr 2 AlC, Cr 2 GeC, V 2 PC, V 2 AsC, Ti 2 SC, Zr 2 InC, Zr 2 TlC, Nb 2 AlC, Nb 2 GaC, Nb 2 InC, Mo 2 GaC, Zr 2 InN, Zr 2 TlN, Zr 2 SnC, Zr 2 PbC, Nb 2 SnC, Nb 2 PC, Nb 2 AsC, Zr 2 SC, Nb 2 SC, Hf 2 InC, Hf 2 TlC, Ta 2 AlC, Ta 2 GaC, Hf 2 SnC, Hf 2 PbC, Hf 2 SnN, Hf 2 SC, Ti 3 AlC 2 , V 3 AlC 2 , Ti 3 SiC 2 , Ti 3 GeC 2 , Ti 3 SnC 2 , Ta 3 AlC 2 , Ti 4 AlN 3 , V 4 AlC 3 , Ti 4 GaC 3 , Ti 4 SiC 3 , Ti 4 GeC 3 , Nb 4 AlC 3 , and Ta 4 AlC 3 .
4. The ceramic matrix composite of claim 3 , wherein the MAX phase compound is selected from the group consisting of: Ti 2 AlC, Ti 2 AlN, Ti 3 SiC 2 , Ti 4 AlN 3 and Ti 4 SiC 3 .
5. The ceramic matrix composite of claim 1 , wherein the silicon carbide is present in the ceramic matrix at a concentration of no more than about 60 wt. %.
6. The ceramic matrix composite of claim 5 , wherein the concentration of the silicon carbide is from about 1 wt. % to about 40 wt. %.
7. The ceramic matrix composite of claim 1 , wherein the ceramic matrix further comprises a silicide.
8. The ceramic matrix composite of claim 7 , wherein the silicide is selected from the group consisting of titanium silicide, vanadium silicide, chromium silicide, scandium silicide, zirconium silicide, niobium silicide, molybdenum silicide, hafnium silicide and tantalum silicide.
9. The ceramic matrix composite of claim 1 , wherein the ceramic matrix comprises no more than about 5 wt. % unreacted silicon.
10. A ceramic matrix composite (CMC) part comprising at least one component comprising the ceramic matrix composite of claim 1 .
11. The CMC part of claim 10 , wherein the component is selected from the group consisting of: blade seal segments, blades, vanes, and combustion liners.
12. A method of making a ceramic matrix composite, the method comprising:
infiltrating a porous fiber preform comprising coated silicon carbide fibers with a slurry comprising solid particulate matter, the solid particulate matter including silicon carbide particles and at least one MAX phase precursor, thereby forming an impregnated fiber preform;
infiltrating the impregnated fiber preform with a melt comprising silicon; and
forming a ceramic matrix composite comprising silicon carbide fibers in a ceramic matrix, wherein the ceramic matrix comprises silicon carbide and a MAX phase compound having a chemical composition M n+1 AX n , where M is a transition metal selected from the group consisting of: Ti, V, Cr, Sc, Zr, Nb, Mo, Hf, and Ta; A is a group-A element selected from the group consisting of: Al, Si, P, S, Ga, Ge, As, Cd, In, Sn, Tl and Pb, and X is carbon or nitrogen, with n being an integer from 1 to 3.
13. The method of claim 12 , wherein the melt comprises a silicon alloy.
14. The method of claim 13 , wherein the melt further comprises the transition metal.
15. The method of claim 14 , wherein the melt further comprises the group-A element.
16. The method of claim 13 , wherein the melt comprises the silicon alloy at a eutectic composition thereof.
17. The method of claim 13 , wherein the melt is at a temperature less than a melting temperature of silicon.
18. The method of claim 12 , wherein the at least one MAX phase precursor comprises a carbide, nitride or hydride comprising the transition metal.
19. The method of claim 12 , wherein the at least one MAX phase precursor comprises a carbide, nitride or hydride comprising the group-A element.
20. A ceramic matrix composite comprising:
a ceramic matrix including silicon carbide, a silicide, and a MAX phase compound having a chemical composition M n+1 AX n , where
M is selected from the group consisting of: Ti, V, Cr, Sc, Zr, Nb, Mo, Hf, and Ta,
A is selected from the group consisting of: Al, Si, P, S, Ga, Ge, As, Cd, In, Sn, Tl and Pb,
X is carbon or nitrogen, and
n is an integer from 1 to 3; and
continuous silicon carbide fibers in the ceramic matrix.
21. The ceramic matrix composite of claim 20 , wherein the silicide is selected from the group consisting of titanium silicide, vanadium silicide, chromium silicide, scandium silicide, zirconium silicide, niobium silicide, molybdenum silicide, hafnium silicide and tantalum silicide.