Repair process using networked ceramic nanofibers
A repair process for an article such as an airfoil includes providing an article that has a substrate and a ceramic barrier coating disposed on the substrate, where the ceramic barrier coating has a damaged region, abrading the damaged region to provide dimple in the ceramic barrier coating, wherein a remaining region of the ceramic barrier coating adjacent the dimple remains intact, and depositing a patch of networked ceramic nanofibers in the dimple.
1. A repair process comprising:
providing an article that has a substrate and a ceramic barrier coating disposed on the substrate, wherein the ceramic barrier coating has a porous columnar microstructure that includes microstructural columns that define elongated pores there between and the ceramic barrier coating has a damaged region;
abrading the damaged region to provide a dimple in the ceramic barrier coating, wherein a remaining region of the ceramic barrier coating adjacent the dimple remains intact; and
depositing a patch of networked ceramic nanofibers in the dimple, wherein the networked ceramic nanofibers comprise filaments that are non-linear and intertwined so as to form a porous network, the filaments being bonded together at locations where the filaments contact each other, and wherein the networked ceramic nanofibers extend into the elongated pores and interlock with the elongated pores and surface roughness of the dimple such that the networked ceramic nanofibers are secured to the ceramic barrier coating.
2. The process as recited in claim 1 , wherein the abrading includes spraying the damaged region with an abrasive media.
3. The process as recited in claim 2 , wherein the abrasive media includes dry ice.
4. The process as recited in claim 1 , wherein the damaged region is a spalled or worn region.
5. The process as recited in claim 1 , wherein the depositing includes blow-spinning and sintering.
6. The process as recited in claim 5 , wherein the sintering includes heating using an energy beam.
7. The process as recited in claim 1 , further comprising polishing the patch to be flat with the remaining region of the ceramic barrier coating adjacent the patch.
8. The process as recited in claim 1 , wherein the ceramic nanofibers include zirconium oxide.
9. The process as recited in claim 8 , wherein the ceramic nanofibers are selected from the group consisting of yttria stabilized zirconia, gadolinia zirconate, rare earth stabilizer doped zirconate, and combinations thereof, and the ceramic barrier coating is selected from the group consisting of yttria stabilized zirconia, gadolinia zirconate, rare earth stabilizer doped zirconate, and combinations thereof.
10. The process as recited in claim 1 , wherein the ceramic barrier coating has a thickness t1 taken at the remaining portion adjacent the damaged region, and the patch has a thickness t2 that is less than the thickness t1.
11. The process as recited in claim 1 , wherein the filaments are flexible and act as a bumper against particle impacts.
12. The process as recited in claim 1 , wherein introducing the filaments into the elongated pores includes using blow-spinning.
13. A repair process comprising:
providing an airfoil that has a substrate and a ceramic barrier coating disposed on the substrate, wherein the ceramic barrier coating has a porous columnar microstructure that includes microstructural columns that define elongated pores there between and the ceramic barrier coating has a damaged region;
abrading the damaged region to provide a dimple in the ceramic barrier coating, wherein a remaining region of the ceramic barrier coating adjacent the dimple remains intact; and
depositing a patch of networked ceramic nanofibers in the dimple, wherein the networked ceramic nanofibers comprise filaments that are non-linear and intertwined so as to form a porous network, the filaments being bonded together at locations where the filaments contact each other, and wherein the networked ceramic nanofibers extend into the elongated pores and interlock with the elongated pores and surface roughness of the dimple such that the networked ceramic nanofibers are secured to the ceramic barrier coating.
14. The process as recited in claim 13 , wherein the abrading includes spraying the damaged region with an abrasive media.
15. The process as recited in claim 14 , wherein the abrasive media includes dry ice.
16. The process as recited in claim 13 , wherein the damaged region is a spalled or worn region.
17. The process as recited in claim 13 , wherein the depositing includes blow-spinning and sintering.
18. The process as recited in claim 17 , wherein the sintering includes heating using an energy beam.