Methods for fabricating protective coating systems for gas turbine engine applications

Patent metadata

Field	Value
Publication number	US-11623896-B2
Application number	US-201816056060-A
Country	US
Kind code	B2
Filing date	Aug 6, 2018
Priority date	Jan 16, 2014
Publication date	Apr 11, 2023
Grant date	Apr 11, 2023

Abstract

Methods for fabricating protective coating systems for gas turbine engine applications are provided. An exemplary method of applying a protective coating to a substrate includes the steps of providing a substrate formed of a ceramic matrix composite material, forming a first coating layer directly on to the substrate and comprising an oxygen barrier material, a compliance material, or a bonding material and forming a second coating layer directly on to the first coating layer and comprising a thermal barrier material. The method optionally includes forming a third coating layer partially directly on to the second coating layer and partially within at least some of the plurality of pores of the second coating layer.

First claim

What is claimed is:

1. A method of applying a protective coating to a substrate includes the steps of:
providing a substrate formed of a silicon carbide—silicon carbide (SiC—SiC) material;
forming a first coating layer directly on to the substrate and comprising an oxygen barrier material, the first coating layer comprising two or more sol-gel coating layers including a sol-gel of a silicate of zirconium with each sol-gel coating layer comprising a colloidal suspension;
forming a second coating layer directly on to the first coating layer comprising a thermal barrier material and a plurality of pores, with the second coating layer comprising a silicate of yttrium; and
forming a third coating layer partially directly on to the second coating layer and partially within at least some of the plurality of pores of the second coating layer such that the third coating layer infiltrates at least partially into the second coating layer, with the third coating layer forming an exposed surface of the protective coating.

2. The method of claim 1 , wherein forming the second layer is performed using plasma spraying, physical vapor deposition (PVD), electron beam physical vapor deposition (EB-PVD), or dipping.

3. The method of claim 1 , wherein the substrate comprises an irregular surface, and wherein the first coating layer is formed directly on to the irregular surface.

4. The method of claim 1 , wherein the first coating layer is formed with a variable thickness across the substrate of less than about 10 mils.

5. The method of claim 1 , wherein the second coating layer has a second thickness of about 10 mils to about 100 mils, which is greater than a third thickness of the third coating layer and greater than a first thickness of the first coating layer.

6. The method of claim 1 , wherein the second coating layer comprises a porosity of about 10% to about 70%.

7. The method of claim 6 , wherein the porosity has a gradient within the second coating layer.

8. The method of claim 1 , wherein an applied vacuum is used to infiltrate the third coating layer into the second coating layer and the third coating layer coats the walls of the pores but does not completely fill the pores.

9. The method of claim 8 , wherein the third coating layer infiltrates the second coating layer to a depth of about 70% or less of a total thickness of the second coating layer, thereby creating a porosity gradient in the second coating layer.

10. The method of claim 1 , wherein the third coating layer consists of a silicate of zirconium.

11. A method of applying a protective coating to a substrate includes the steps of:
providing a substrate formed of a silicon carbide—silicon carbide (SiC—SiC) material, wherein the substrate has an exterior surface exhibiting a degree of valley/hill surface irregularity comprising a plurality of hills and a plurality of valleys;
forming a first coating layer comprising two or more sol-gel coating layers including a sol-gel of a silicate of zirconium over the substrate, each of the sol-gel coating layers comprising a colloidal suspension, wherein the first coating layer is characterized as an oxygen barrier material, the first coating layer is formed directly on to the exterior surface of the substrate and conforms to the exterior surface of the substrate such that the first coating layer has a non-uniform coating thickness over the substrate, the first coating layer has a thickness within the plurality of valleys that is greater than its thickness over the plurality of hills;
forming a second, porous coating layer directly on to the exterior surface of the first coating layer and characterized as a thermal barrier material, the second coating layer further comprises a plurality of pores within the second coating layer and the second coating layer comprises a silicate of yttrium; and
forming a third coating layer partially directly on to an exterior surface of the second coating layer and partially within at least some of the plurality of pores within the second coating layer, the third coating layer forming an exposed surface of the protective coating, wherein the third coating layer coats walls of at least some of the plurality of pores but does not completely fill the at least some of the plurality of pores, the third coating layer infiltrates the second coating layer to a depth of 70% or less of a total thickness of the second coating layer and the third coating layer comprises a silicate of zirconium.

12. A method of applying a protective coating to a substrate includes the steps of:
providing substrate formed of a silicon carbide—silicon carbide (SiC—SiC) material, wherein the substrate has an exterior surface exhibiting a degree of valley/hill surface irregularity comprising a plurality of hills and a plurality of valleys;
forming a first coating layer comprising two or more sol-gel coating layers including a sol-gel consisting of a silicate of zirconium over the substrate, each of the sol-gel coating layers comprising a colloidal suspension, wherein the first coating layer is characterized as an oxygen barrier material, the first coating layer is formed directly on to the exterior surface of the substrate and conforms to the exterior surface of the substrate such that the first coating layer has a non-uniform coating thickness over the substrate, the first coating layer has a thickness within the plurality of valleys that is greater than its thickness over the plurality of hills;
forming a second, porous coating layer directly on to the exterior surface of the first coating layer and characterized as a thermal barrier material, the second coating layer further comprises a plurality of pores within the second coating layer such that the second coating layer comprises a porosity of about 10% to about 70%, the second coating layer consists of a silicate of yttrium; and
forming a third coating layer partially directly on to an exterior surface of the second coating layer and partially within at least some of the plurality of pores within the second coating layer, the third coating layer forming an exposed surface of the protective coating and the substrate has a use temperature of 3000 degrees Fahrenheit with the protective coating, the third coating layer consists of a silicate of zirconium, the third coating layer coats walls of at least some of the plurality of pores but does not completely fill the at least some of the plurality of pores, the third coating layer infiltrates the second coating layer to a depth of 70% or less of a total thickness of the second coating layer, thereby creating a porosity gradient in the second coating layer, and 30% or more of the total thickness of the second coating layer comprises pores that remain uncoated.

Assignees

• Honeywell Int Inc

Inventors

• Oboodi Reza
• Passman Eric
• Jadidian Bahram

Classifications

• Y02T50/60

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

• C04B41/009

  characterised by the material treated · CPC title

• Y10T428/26

  Web or sheet containing structurally defined element or component, the element or component having a specified physical dimension · CPC title

• C04B41/52 Primary

  Multiple coating or impregnating {multiple coating or impregnating with the same composition or with compositions only differing in the concentration of the constituents, is classified as single coating or impregnation} · CPC title

• Y10T428/24999

  Inorganic · CPC title