CMAS-resistant abradable coatings
View Patent ↗In one example, an article including a metallic substrate; and an abradable coating on the metallic substrate, the abradable coating including a plurality of abradable layers in an alternating arrangement with a plurality of CMAS resistant layers, wherein the plurality of CMAS resistant layers are configured to react with molten CMAS to form a stable phase.
1. An abradable system comprising:
a metallic substrate;
an abradable coating on the metallic substrate, the abradable coating comprising a plurality of abradable layers in an alternating arrangement with a plurality of CMAS resistant layers, wherein the plurality of CMAS resistant layers are configured to react with molten CMAS to form a stable phase; and
an opposing abrasive element acting on the abradable coating,
wherein the abrasive element is configured to abrade the abradable coating to a maximum penetration depth in the abradable coating, and wherein the abradable coating comprises at least one respective CMAS resistant layer of the plurality of CMAS resistant layers between the maximum penetration depth and the metallic substrate.
2. The system of claim 1 , wherein the plurality of abradable layers comprise a magnesium (Mg) spinel.
3. The system of claim 1 , wherein the plurality of CMAS resistant layers comprises at least one of gadolinium zirconate (GdZO), yttria stabilized zirconia with greater than 8 wt. % yttria, or a yttrium aluminate garnet.
4. The system of claim 1 , wherein the plurality of CMAS resistant layers comprises yttria stabilized zirconia having great than 8 wt. % yttria with a remainder being zirconia.
5. The system of claim 1 , wherein the plurality of abradable layers have a higher porosity than the plurality of CMAS resistant layers.
6. The system of claim 1 , wherein the plurality of abradable layers have a greater thickness than the plurality of CMAS resistant layers.
7. The system of claim 1 , further comprising a bond coat on the substrate, wherein the abradable coating is on the bond coat.
8. The system of claim 1 , wherein a respective layer of the plurality of CMAS resistant layers define an outermost topcoat of the abradable coating.
9. The system of claim 1 , wherein a respective layer of the plurality of abradable layers is nearest to the metallic substrate of the abradable coating.
10. A method comprising:
forming an abradable coating on a metallic substrate, the abradable coating comprising a plurality of abradable layers in an alternating arrangement with a plurality of CMAS resistant layers, wherein the plurality of CMAS resistant layers are configured to react with molten CMAS to form a stable phase; and
abrading the abradable coating with an opposing abrasive element acting on the abradable coating, wherein the abrasive element is configured to abrade the abradable coating to a maximum penetration depth in the abradable coating, and wherein the abradable coating comprises at least one respective CMAS resistant layer of the plurality of CMAS resistant layers between the maximum penetration depth and the metallic substrate.