Segmented environmental barrier coating systems and methods of forming the same

Patent metadata

Field	Value
Publication number	US-10934626-B2
Application number	US-201715493798-A
Country	US
Kind code	B2
Filing date	Apr 21, 2017
Priority date	Apr 21, 2017
Publication date	Mar 2, 2021
Grant date	Mar 2, 2021

Abstract

Methods for preparing an environmental barrier coating and the resulting coating are provided. The methods and products include the incorporation of a continuous ceramic inner layer and a segmented ceramic outer layer on a CMC component. The segmented ceramic outer layer may be formed by thermal spray techniques. The coating is more stable at higher temperatures and provides for a longer lifetime of the coated component.

First claim

What is claimed is:

1. A coated component comprising:
a substrate defining a surface and comprising a ceramic composite,
an inner layer defining a surface and disposed along the surface of the substrate, and
an outer layer disposed along the surface of the inner layer,
wherein the inner layer comprises ceramic material, has a porosity of less than about 40% by volume, and is continuous along the outer layer, and
wherein the outer layer comprises a plurality of growth domains defined between domain boundaries, the plurality of growth domains comprising a comparatively high density of a coating material and the domain boundaries comprising a comparatively low density of the coating material, the growth domains and domain boundaries having a plurality of pre-condensed matter particles that have been at least partially melted before impinging the surface and solidified thereon, wherein the domain boundaries comprise a density of the coating material greater than 0% and are configured to accommodate expansion and shrinkage of the growth domains.

2. The coating of claim 1 , wherein the outer layer has an intra-domain density of at least about 75%.

3. The coating of claim 2 , wherein the intra-domain density is at least about 85%.

4. The coating of claim 1 , wherein the outer layer has a substantially equiaxed grain morphology.

5. The coating of claim 1 , wherein the inner layer comprises an alkaline earth aluminosilicate.

6. The coating of claim 5 , wherein the outer layer has an intra-domain density of at least about 75%.

7. The coating of claim 5 , wherein the outer layer has a substantially equiaxed grain morphology.

8. The coating of claim 5 , wherein the coating material comprises rare earth silicate.

9. The coating of claim 5 , wherein the coating material comprises rare earth monosilicate.

10. The coating of claim 5 , wherein at least 50% or more by volume of the outer layer comprises the growth domains.

11. The coating of claim 10 , wherein the outer layer has an intra-domain density of at least about 75%,
wherein the outer layer has a substantially non-equiaxed grain morphology comprising a median aspect ratio of greater than about 4:1 to about 10:1,
wherein the coating material comprises rare earth silicate, and
wherein the coating material comprises rare earth monosilicate.

12. The coating of claim 1 , wherein the coating material comprises a rare earth silicate.

13. The coating of claim 1 , wherein the coating material comprises rare earth monosilicate.

14. The coating of claim 1 , wherein each growth domain in the plurality of growth domains has a width in a range from about 20 μm to about 100 μm.

15. The coating of claim 1 , wherein the coating comprises a spray coating.

16. The coating of claim 1 , wherein at least 50% or more by volume of the outer layer comprises the growth domains.

17. The coating of claim 1 , further comprising a bond coat disposed between the substrate and the inner layer.

18. A component of a gas turbine assembly comprising the coating system of claim 1 .

19. The coating of claim 1 , wherein less than about 50% by volume of the outer layer comprises the growth domains.

Assignees

• Gen Electric

Inventors

• Wan Julin
• Rosenzweig Larry Steven

Classifications

• C04B41/89 Primary

  for obtaining at least two superposed coatings having different compositions · CPC title

• C23D5/005

  by a method specially adapted for coating special objects · CPC title

• F01D5/282

  Selecting composite materials, e.g. blades with reinforcing filaments · CPC title

• Y02T50/60

  Efficient propulsion technologies, e.g. for aircraft · CPC title

• C04B41/009

  characterised by the material treated · CPC title