Methods for forming vertically cracked thermal barrier coatings and articles including vertically cracked thermal barrier coatings

Patent metadata

Field	Value
Publication number	US-10174412-B2
Application number	US-201615368161-A
Country	US
Kind code	B2
Filing date	Dec 2, 2016
Priority date	Dec 2, 2016
Publication date	Jan 8, 2019
Grant date	Jan 8, 2019

Abstract

A method for forming a vertically cracked thermal barrier coating is disclosed including positioning an article relative to a heat source. The article includes a thermal barrier coating disposed on a first surface of a substrate, and the substrate includes a second surface distal across the substrate from the first surface. Heat is applied locally to at least one discrete portion of the second surface of the substrate. At least one vertical crack in the thermal barrier coating is formed disposed over the at least one discrete portion. An article is disclosed including a substrate and a vertically-cracked thermal barrier coating disposed on the substrate. The vertically cracked thermal barrier coating includes at least one vertical crack in the thermal barrier coating and at least one of a low density of less than 85% of a theoretical density for the thermal barrier coating and a selective crack distribution.

First claim

What is claimed is:

1. A method for forming a vertically cracked thermal barrier coating, comprising:
positioning an article relative to a heat source, the article including a thermal barrier coating disposed on a first surface of a substrate, the substrate including a second surface distal across the substrate from the first surface;
applying heat locally to at least one discrete portion of the second surface of the substrate; and
forming at least one vertical crack in the thermal barrier coating disposed over the at least one discrete portion.

2. The method of claim 1 , wherein the thermal barrier coating is a low density thermal barrier coating including a density of less than 85% of a theoretical density for the thermal barrier coating.

3. The method of claim 1 , wherein forming the vertically cracked thermal barrier coating includes forming a selective crack distribution wherein the at least one vertical crack is present in a first region of the thermal barrier coating, and a second region of the thermal barrier coating is free of vertical cracks.

4. The method of claim 1 , wherein applying heat locally includes applying a welding technique to the at least one discrete portion of the second surface of the substrate.

5. The method of claim 4 , wherein applying the welding technique to the at least one discrete portion includes forming at least one of a weld bead, a weld turbulator, and a weld repair.

6. The method of claim 4 , wherein applying the welding technique to the at least one discrete portion produces weld shrinkage at the at least one discrete portion, the weld shrinkage forming the at least one vertical crack.

7. The method of claim 1 , wherein the thermal barrier coating has a thickness, and the at least one vertical crack extends through less than the thickness of the thermal barrier coating.

8. The method of claim 1 , wherein the thermal barrier coating has a thickness, and the at least one vertical crack extends through the entire thickness of the thermal barrier coating.

9. The method of claim 1 , wherein a bond coat is disposed between the first surface of the substrate and the thermal barrier coating, and the at least one vertical crack does not extend into the bond coat.

10. The method of claim 1 , wherein the substrate includes a composition selected from the group consisting of a superalloy, a refractory alloy, a nickel-based superalloy, a cobalt-based superalloy, an iron-based superalloy, an iron-based alloy, a steel alloy, a stainless steel alloy, a cobalt-based alloy, a nickel-based alloy, a titanium-based alloy, a titanium aluminide, and combinations thereof.

11. The method of claim 1 , wherein the thermal barrier coating includes a material selected from the group consisting of rare-earth stabilized zirconia, alumina, and combinations thereof.

12. The method of claim 1 , wherein the article is selected from the group consisting of an article including sheet metal, a turbine component, a combustion liner, and combinations thereof.

13. The method of claim 12 , wherein the article is a turbine component, the turbine component being a combustion liner, the first surface is an inner surface of the combustion liner, and the second surface is an outer surface of the combustion liner.

14. The method of claim 12 , wherein applying heat locally includes welding the at least one discrete portion of the second surface of the substrate, forming a weld turbulator.

15. The method of claim 1 , wherein the method is performed without any stripping of the thermal barrier coating.

16. The method of claim 1 , wherein the at least one vertical crack in the thermal barrier coating is formed without a vacuum furnace.

17. A method for forming a vertically cracked thermal barrier coating on a turbine component, comprising:
positioning the turbine component relative to a welding device, the turbine component including a thermal barrier coating disposed on a first surface of a substrate, the substrate including a second surface distal across the substrate from the first surface;
welding at least one discrete portion of the second surface of the substrate, producing weld shrinkage at the at least one discrete portion; and
forming by the weld shrinkage at least one vertical crack in the thermal barrier coating disposed over the at least one discrete portion.

18. The method of claim 2 , wherein the density of the low density thermal barrier coating is between about 40% to about 70% of the theoretical density for the thermal barrier coating.

19. The method of claim 1 , wherein applying heat locally to the at least one discrete portion of the second surface of the substrate includes forming a molten pool on the second surface of the substrate.

20. The method of claim 19 , wherein the molten pool does not penetrate to the first surface.

Assignees

• Gen Electric

Inventors

• Lin Dechao
• Bucci David

Classifications

• F01D5/288

  Protective coatings for blades · CPC title

• C23C28/321

  with at least one metal alloy layer · CPC title

• C23C4/11

  Oxides · CPC title

• B23K31/003

  relating to controlling of welding distortion · CPC title

• B23K2103/172

  wherein at least one of the layers is non-metallic · CPC title