Ceramic matrix composite component including cooling channels in multiple plies and method of producing
A ceramic matrix composite (CMC) component and method of fabrication including one or more elongate functional features formed in multiple fiber plies of the CMC component. The CMC component includes a plurality of longitudinally extending ceramic matrix composite plies in a stacked configuration. Each of the one or more elongate functional features includes an inlet and an outlet to provide a flow of fluid from a fluid source to an exterior of the ceramic matrix composite component. The one or more elongate functional features are configured in multiple plies of the plurality of longitudinally extending ceramic matrix composite plies to form a plurality of cooling channels in multiple plies of the ceramic matrix composite component.
1. A ceramic matrix composite component, comprising:
a plurality of longitudinally extending ceramic matrix composite plies in a stacked configuration forming a densified body; and
one or more elongate functional features formed therein the densified body,
wherein each of the one or more elongate functional features includes an inlet and an outlet, the one or more elongate functional features configured to provide a flow of fluid from a fluid source to an exterior of the ceramic matrix composite component, and
wherein the one or more elongate functional features are configured in multiple plies of the plurality of longitudinally extending ceramic matrix composite plies to form a plurality of cooling channels in multiple plies of the ceramic matrix composite component, wherein a plurality of cooling channels define a z-type cooling circuit configuration.
2. The ceramic matrix composite component of claim 1 , wherein the one or more elongate functional features are enclosed within the densified body.
3. The ceramic matrix composite component of claim 1 , wherein the plurality of longitudinally extending ceramic matrix composite plies are pre-impregnated ceramic matrix composite plies.
4. The ceramic matrix composite component of claim 1 , wherein the ceramic matrix composite component is a hot gas path turbine component.
5. The ceramic matrix composite component of claim 4 , wherein the hot gas path turbine component is selected from the group consisting of a combustor liner, a blade, a shroud, a nozzle, a nozzle end wall, and a blade platform.
6. A ceramic matrix composite component, comprising:
a plurality of longitudinally extending ceramic matrix composite plies in a stacked configuration forming a densified body; and
one or more elongate functional features formed therein the densified body,
wherein each of the one or more elongate functional features includes an inlet and an outlet, the one or more elongate functional features configured to provide a flow of fluid from a fluid source to an exterior of the ceramic matrix composite component, and
wherein the one or more elongate functional features are configured in multiple plies of the plurality of longitudinally extending ceramic matrix composite plies to form a plurality of cooling channels in multiple plies of the ceramic matrix composite component,
wherein each of the one or more elongate functional features in each of the plurality of longitudinally extending ceramic matrix composite plies is in fluid communication with one or more elongate functional features in another one of the plurality of longitudinally extending ceramic matrix composite plies via one or more fluid connections.
7. The ceramic matrix composite component of claim 6 , wherein the one or more fluid connections are formed via one or more of laser drilling, electrical discharge machining, cutting or machining the ceramic matrix composite material.
8. The ceramic matrix composite component of claim 6 , wherein the one or more fluid connections comprise one or more laser drilled fluid connections.
9. The ceramic matrix composite component of claim 6 , wherein the one or more fluid connections are formed during lay-up of the plurality of longitudinally extending ceramic matrix composite plies.
10. The ceramic matrix composite component of claim 6 , wherein the plurality of longitudinally extending ceramic matrix composite plies are pre-impregnated ceramic matrix composite plies.
11. A ceramic matrix composite component, comprising:
a plurality of longitudinally extending ceramic matrix composite plies in a stacked configuration forming a densified body; and
one or more elongate functional features formed in multiple plies of the plurality of longitudinally extending ceramic matrix composite plies, each of the one or more elongate functional features in fluid communication with one or more elongate functional features in another one of the plurality of longitudinally extending ceramic matrix composite plies via one or more fluid connections,
wherein each of the one or more elongate functional features includes an inlet and an outlet, the one or more elongate functional features defining a plurality of cooling channels in multiple plies of the ceramic matrix composite component to carry a flow of fluid from a fluid source to an exterior of the ceramic matrix composite component.
12. The ceramic matrix composite component of claim 11 , wherein the one or more fluid connections are formed via one or more of laser drilling, electrical discharge machining, cutting or machining the ceramic matrix composite material.
13. The ceramic matrix composite component of claim 11 , wherein the one or more fluid connections are formed during layup of the plurality of longitudinally extending ceramic matrix composite plies.
14. The ceramic matrix composite component of claim 11 , wherein the ceramic matrix composite component is a hot gas path turbine component.
15. The ceramic matrix composite component of claim 14 , wherein the hot gas path turbine component is selected from the group consisting of a combustor liner, a blade, a shroud, a nozzle, a nozzle end wall, and a blade platform.
16. A method of forming a ceramic matrix composite (CMC) product comprising:
forming a CMC preform comprising a matrix precursor, a plurality of reinforcing fibers and a plurality of sacrificial fibers;
performing one of:
removing the plurality of sacrificial fibers such that one or more elongate functional features are formed in multiple fiber plies of the CMC preform; or
applying a fluid infiltrant to the CMC preform thereby densifying the CMC preform,
performing the other of:
removing the plurality of sacrificial fibers such that one or more elongate functional features are formed in multiple fiber plies of the CMC preform; or
applying a fluid infiltrant to the CMC preform thereby densifying the CMC preform, and
coupling the one or more functional features of the multiple fiber plies of the CMC preform in fluid communication to form a plurality of cooling channels in multiple plies of the ceramic matrix composite component.
17. The method of claim 16 , wherein coupling the one or more functional features of the multiple fiber plies is by a method selected from the group consisting of laser drilling, electrical discharge machining, cutting and machining.
18. The method of claim 16 , wherein the fluid infiltrant is silicon or a silicon alloy.
19. The method of claim 17 , wherein the ceramic matrix composite component is a hot gas path turbine component.
20. The method of claim 19 , wherein the hot gas path turbine component is selected from the group consisting of a combustor liner, a blade, a shroud, a nozzle, a nozzle end wall, and a blade platform.