Ceramic matrix composite component having low density core and method of making
Disclosed is a ceramic matrix component having a fibrous core and a ceramic matrix composite shell surrounding at least a portion of the fibrous core. The ceramic matrix composite shell comprises a fibrous preform. The fibrous core has a greater porosity than the fibrous preform. A method of making the ceramic matrix component is also disclosed.
1. A ceramic matrix component comprising a fibrous core and a ceramic matrix composite shell surrounding at least a portion of the fibrous core, wherein the ceramic matrix composite shell comprises a fibrous preform and the fibrous core has a greater porosity than the fibrous preform; and
wherein the fibrous core further comprises ceramic foam, and wherein the ceramic foam is positioned at a leading edge of the fibrous core.
2. The ceramic matrix component of claim 1 , wherein the fibrous core porosity is 2-3 times greater than the porosity of the fibrous preform.
3. The ceramic matrix component of claim 1 , wherein the ceramic foam is positioned at a trailing edge of the fibrous core.
4. The ceramic matrix component of claim 1 , wherein the fibrous core comprises cooling passages.
5. The ceramic matrix component of claim 4 , wherein cooling passages are located at a leading edge of the ceramic matrix component.
6. The ceramic matrix component of claim 4 , wherein cooling passages are located at the trailing edge of the ceramic matrix component.
7. The ceramic matrix component of claim 1 , wherein the ceramic matrix composite shell has a thickness greater than or equal to 0.03 inch.
8. The ceramic matrix component of claim 1 , wherein the fibrous core comprises braided or woven fibers.
9. The ceramic matrix component of claim 1 , wherein the fibrous core employs the same type of fibers as the fibrous preform.
10. A method of making a ceramic matrix component comprising forming a fibrous core having a first porosity, forming a fibrous preform on the fibrous core wherein the fibrous preform has a porosity less than the first porosity, and forming a ceramic matrix on the fibrous preform using chemical vapor infiltration; and
wherein the fibrous core comprises ceramic foam, and wherein the ceramic foam is positioned at a leading edge of the fibrous core.
11. The method of claim 10 , wherein the ceramic foam is positioned at a trailing edge of the fibrous core.
12. The method of claim 10 , wherein the fibrous core comprises sacrificial fibers.
13. The method of claim 12 , wherein the sacrificial fibers are located at a leading edge of the fibrous core.
14. The method of claim 12 , wherein the sacrificial fibers are located at a trailing edge of the fibrous core.
15. The method of claim 10 , wherein the fibrous core comprises braided or woven fibers.
16. The method of claim 10 , wherein the fibrous core employs the same type of fibers as the fibrous preform.