Components with thermal barrier coatings having solid films thereon and methods of coating the same
AssigneeHoneywell International Inc.
InventorsJason Van Sluytman, Vladimir Tolpygo
Life of this patent
Estimating the term…
Loading patent…
AssigneeHoneywell International Inc.
InventorsJason Van Sluytman, Vladimir Tolpygo
Estimating the term…
Components and methods for coating the components are provided. The methods include depositing a coating composition on a substrate that includes about 350 wt. % rare-earth oxides, 45-96.5 wt. % zirconia, and 0.5-4 wt. % alumina, heat treating the coating composition to form a CMAS-resistant thermal barrier coating (TBC) that includes a columnar microstructure with voids in open communication with a surface thereof, wherein the alumina is homogeneously distributed throughout the TBC, contacting the TBC with a film precursor, transporting the film precursor along interior wall surfaces of the voids to form a thin film thereon, wherein the thin film has a thickness on the interior wall surfaces of 10-150 nm, and forming a solid film on the interior wall surfaces of the voids from the film precursor that includes aluminum phosphate and that does not fill the voids that have diameters of 50 nm or greater.
A method, comprising:
A component of a gas turbine engine, comprising:
Dependencies are inferred from the claim text.