High density bond coat for ceramic or ceramic matrix composites

Patent metadata

Field	Value
Publication number	US-10858725-B2
Application number	US-201816017448-A
Country	US
Kind code	B2
Filing date	Jun 25, 2018
Priority date	Jun 26, 2017
Publication date	Dec 8, 2020
Grant date	Dec 8, 2020

Abstract

A method that includes introducing a suspension comprising a coating material and a carrier into a heated plume of a thermal spray device. The coating material may include silicon or a silicon alloy. The method further includes directing the coating material using the heated plume toward a substrate that includes a ceramic or a ceramic matrix composite and depositing the coating material to form a bond coat directly on the substrate such that the bond coat defines a porosity of less than about 3 percent by volume.

First claim

What is claimed is:

1. A method comprising:
introducing a suspension comprising a coating material and a carrier into a heated plume of a thermal spray device, wherein the coating material comprises silicon or a silicon alloy;
directing the coating material toward a substrate using the heated plume, wherein the substrate comprises a ceramic or a ceramic matrix composite; and
depositing the coating material to form a bond coat directly on a surface of the substrate, the surface of the substrate having a first surface roughness when the coating material is deposited, wherein the bond coat comprises the silicon or the silicon alloy, wherein the bond coat defines a porosity of less than about 3 percent by volume (vol. %), and wherein an average particle size of particles in the coating composition is selected such that a surface of the bond coat formed by the deposition of the coating material exhibits a second surface roughness that is less than the first surface roughness.

2. The method of claim 1 , wherein the thermal spray device comprises a plasma spray gun or a high-velocity oxy-fuel spray gun.

3. The method of claim 1 , wherein the carrier comprises a water-based or an alcohol-based fluid.

4. The method of claim 1 , wherein the coating material further comprises an additive, wherein the additive comprises at least one of a carbide, a nitride, an oxide, or a silicate.

5. The method of claim 1 , wherein the average particle size of the particles in the coating composition is between about 0.01 μm and about 25 μm.

6. The method of claim 1 , further comprising applying an inert gas shroud to the coating material during deposition of the coating material on the substrate.

7. The method of claim 1 , further comprising depositing one or more additional layers on the bond coat, wherein the one or more additional layers comprise at least one of an environmental barrier coating, a thermal barrier coating, an abradable coating, a bond coat, or a CMAS-resistant layer.

8. The method of claim 7 , wherein depositing the one or more additional layers comprises depositing the environmental barrier coating using a suspension thermal spray technique.

9. The method of claim 7 , wherein depositing the one or more additional layers comprises depositing the abradable coating using a suspension thermal spray technique.

10. The method of claim 1 , wherein the surface of the substrate has the first surface roughness without being mechanically altered to roughen the surface.

11. The method of claim 1 , wherein the surface of the substrate is not grit blasted and/or sanded prior to deposition of the coating material.

12. The method of claim 1 , further comprising, prior to depositing the coating material to form the bond coat, roughening the surface of the substrate to achieve the first surface roughness.

13. The method of claim 1 , wherein the first surface roughness is about 0.76 μm Ra to about 1.27 μm Ra.

14. The method of claim 1 , further comprising depositing a flash bond coat directly on a surface of the bond coat, wherein the flash bond coat is deposited to have at least one of a higher porosity or a higher degree of surface roughness than the bond coat.

15. The method of claim 14 , wherein depositing the flash bond coat comprises depositing the flash bond coat on the surface of the bond coat via air plasma spraying.

16. The method of claim 14 , further comprising depositing one or more additional layers on the flash bond coat, wherein the one or more additional layers comprise at least one of an environmental barrier coating, a thermal barrier coating, an abradable coating, or a CMAS-resistant layer.

17. The method of claim 14 , wherein the flash bond coat has substantially the same composition as the bond coat.

18. The method of claim 1 , wherein the average particle size of the particles in the coating composition is selected such that a surface of the bond coat formed by the deposition of the coating material exhibits the second surface roughness that is less than the first surface roughness is less than about 25 μm.

Assignees

• Rolls Royce Corp
• Rolls Royce Nam Tech Inc

Inventors

• Li Li
• Gong Stephanie
• Gold Matthew R
• Bolcavage Ann

Classifications

• Y02T50/60

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

• C23C4/129

  Flame spraying · CPC title

• F05D2300/514

  Porosity · CPC title

• C23C4/04

  characterised by the coating material · CPC title

• F01D11/122

  with erodable or abradable material (blades having cutting or grinding tips F01D5/20) · CPC title