Features for mitigating thermal or mechanical stress on an environmental barrier coating

Patent metadata

Field	Value
Publication number	US-9713912-B2
Application number	US-201113521647-A
Country	US
Kind code	B2
Filing date	Jan 11, 2011
Priority date	Jan 11, 2010
Publication date	Jul 25, 2017
Grant date	Jul 25, 2017

Abstract

An article may include a substrate comprising a matrix material and a reinforcement material, a layer formed on the substrate, an array of features formed on the layer, and a coating formed on the layer and the array of features. The article may have improved thermal and/or mechanical stress tolerance compared to an article not including the array of features formed on the layer.

First claim

The invention claimed is:

1. An article comprising:
a ceramic matrix composite substrate comprising a matrix material and a reinforcement material;
a layer on the substrate, wherein the layer comprises the matrix material, and wherein the layer defines a surface and comprises an array of features in the surface;
a bond coat on the layer and the array of features; and
an abradable coating over the bond coat, wherein the abradable coating comprises a rare earth silicate and a porosity of between about 30 vol. % and about 45 vol. %.

2. The article of claim 1 , further comprising an environmental barrier coating on the bond coat, wherein the abradable coating is on the environmental barrier coating.

3. The article of claim 1 , wherein the abradable coating is on the bond coat.

4. The article of claim 1 , wherein the array of features comprises an array of at least one of grooves, depressions, ridges, or protrusions.

5. The article of claim 1 , wherein the array of features comprises a first feature and a second feature, and wherein a distance between the first feature and the second feature is less than about 1 inch.

6. The article of claim 1 , wherein the array of features comprises at least one of a groove or a depression, and wherein a depth of the groove or the depression is less than or approximately equal to a thickness of the coating.

7. The article of claim 1 , wherein the array of features comprises at least one of a ridge or a protrusion, and wherein a height of the ridge or the protrusion is less than or approximately equal to a thickness of the coating.

8. The article of claim 1 , further comprising a thermal barrier coating on the bond coat, wherein the abradable coating is on the thermal barrier coating.

9. The article of claim 1 , further comprising a calcia-magnesia-alumina-silicate resistant coating on the bond coat, wherein the abradable coating is on the calcia-magnesia-alumina-silicate resistant coating.

10. The article of claim 1 , wherein the array of features comprises a first feature and a second feature, and wherein the first feature comprises a first characteristic and the second feature comprises a second characteristic different than the first characteristic.

11. The article of claim 10 , wherein the characteristic comprises at least one of a depth, a size, or a shape.

12. The article of claim 1 , wherein the array of features comprises a first feature, a second feature, a third feature, and a fourth feature, and wherein a first pitch between the first feature and the second feature is different than a second pitch between the third feature and the fourth feature.

13. The article of claim 1 , wherein the array of features formed on the layer comprises:
a first array of features formed on the layer at a first location, wherein the first array comprises a first pattern; and
a second array of features formed on the surface of the layer at a second location, wherein the second array comprises a second pattern different than the first pattern.

14. The article of claim 13 , wherein at least one of the first array of features or the second array of features comprises a first feature and a second feature, and wherein a distance between the first feature and the second feature is between about 0.05 inches and 0.25 inches.

15. The article of claim 13 , wherein at least one of the first array of features or the second array of features comprises at least one of a groove or a depression, and wherein a depth of the groove or the depression is between about 20 percent and about 80 percent of a thickness of the coating.

16. The article of claim 13 , wherein at least one of the first array of features or the second array of features comprises at least one of a ridge or a protrusion, and wherein a height of the ridge or the protrusion is between about 20 percent and about 80 percent of a thickness of the coating.

17. The article of claim 13 , wherein at least one of the first array of features or the second array of features comprises at least one of a groove, a ridge, a depression, or a protrusion, and wherein a width of the groove, the ridge, the depression, or the protrusion is between about 0.004 inch and about 0.04 inch.

18. The article of claim 13 , wherein the first pattern comprises at least one of a depth of the features, a size of the features, a pitch between the features, or a shape of the features, and wherein the second pattern comprises at least one of a depth of the features, a size of the features, a pitch between the features, or a shape of the features.

19. The article of claim 1 , wherein the layer defines a thickness sufficient to ensure that none of the reinforcement material is exposed at a surface of the layer, and wherein the layer consists essentially of the matrix material.

20. The article of claim 1 , wherein the bond coat comprises at least one of silicon, mullite, silica, a silicide, or a rare earth silicate.

21. A method comprising:
forming a layer on a ceramic matrix composite substrate, wherein the ceramic matrix composite substrate comprises a matrix material and a reinforcement material, and wherein the layer comprises the matrix material and defines a surface;
forming an array of features in the surface of the layer;
forming a bond coat on the layer;
forming an abradable coating over the bond coat and the array of features, wherein the abradable coating comprises a rare earth silicate and a porosity of between about 30 vol. % and about 45 vol. %.

22. The method of claim 21 , further comprising forming an environmental barrier coating on the bond coat, wherein forming the abradable coating comprises forming the abradable coating on the environmental barrier coating.

23. The method of claim 22 , further comprising forming a calcia-magnesia-alumina-silicate resistant coating on the bond coat and the array of features, wherein forming the abradable coating comprises forming the abradable coating on the calcia-magnesia-alumina-silicate resistant coating.

24. The method of claim 21 , wherein forming the abradable coating comprises forming the abradable coating on the bond coat.

25. The method of claim 21 , wherein forming the array of features comprises forming an array of at least one of grooves, depressions, ridges, or protrusions.

26. The method of claim 21 , further comprising forming a thermal barrier coating on the bond coat, wherein forming the abradable coating comprises forming the abradable coating on the thermal barrier coating.

27. The method of claim 21 , wherein forming the array of features on the surface of the layer comprises:
forming a first array of features in a surface of the layer at a first location, wherein the first array of features comprises a first pattern; and
forming a second array of features in the surface of the layer at a second location, wherein the second array of features comprises a second pattern different than the first pattern.

28. The method of claim 27 , wherein the first array of features comprises an array of at least one of grooves, depressions, ridges, or protrusions, and wherein the second array of features comprises an array of at least one of grooves, depressions, ridges, or protrusions.

29. The method of claim 27 , wherein the first pattern comprises at least one of a depth of the features, a size of the features, a pitch between the features, o

Assignees

• Lee Kang N
• Rolls Royce Corp

Inventors

• Lee Kang N

Classifications

• C04B41/5031

  Alumina · CPC title

• C23C28/42

  characterized by the composition of the alternating layers · CPC title

• F01D5/288

  Protective coatings for blades · CPC title

• C04B41/5059

  Silicon carbide · CPC title

• Y10T428/24521

  with component conforming to contour of nonplanar surface · CPC title