Chromizing over cathodic arc coating

Patent metadata

Field	Value
Publication number	US-10844478-B2
Application number	US-201916516455-A
Country	US
Kind code	B2
Filing date	Jul 19, 2019
Priority date	Dec 10, 2013
Publication date	Nov 24, 2020
Grant date	Nov 24, 2020

Abstract

The present invention provides a Cr-rich cathodic arc coating, an article in turbine blade coated with the chromizing over cathodic arc coating, and a method to produce the coating thereof. The Cr-rich cathodic arc coating in the present invention comprises a cathodic arc coating and a diffusion coating deposited atop the cathodic arc coating to enforce hot corrosion resistance. The hardware coated with the chromizing over cathodic arc coating in the present invention is reinforced with superior-hot corrosion resistance. The present invention further provides a novel method for producing the chromizing over cathodic arc coating by re-sequencing coating deposition order. The method in the present invention is efficient and cost-reducing by eliminating some operations, e.g., DHT and peening, between the cathodic arc coating and the diffusion coating. The hot corrosion resistance in the present invention results from the high Cr content in the surface of the coating.

First claim

What is claimed is:

1. A chromium-rich cathodic arc coating comprising;
a MCrAlY cathodic arc coating on a substrate, wherein M is a metal alloy comprising nickel, cobalt, iron, or a combination thereof, and the cathodic arc coating comprises Si and 25 to 50% chromium by weight based on the weight of the MCrAl; and
a diffused chromide coating atop the MCrAlY cathodic arc coating,
wherein the diffused chromide coating has a higher content of chromium than the MCrAlY cathodic arc coating, the combined thickness of the diffused chromide coating and the MCrAlY cathodic arc coating is 2.5 to 3 mil (0.0635 to 0.0762 mm) and the chromium-rich cathodic arc coating has a chromium rich phase with a depth of 0.1 to 2.5 mils (0.00254 to 0.0635 mm).

2. The chromium-rich cathodic arc coating according to claim 1 , wherein the surface of the diffused chromide coating atop the MCrAlY has a chromium content no less than 37% by weight.

3. The chromium-rich cathodic arc coating according to claim 2 , wherein the MCrAlY has a chromium content between 25% and 35% by weight based on the weight of the MCrAlY.

4. The chromium-rich cathodic arc coating according to claim 1 , wherein the MCrAlY comprises Si in an amount of 0.15 to 0.65% by weight based on the of the MCrAlY.

5. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium rich phase has a depth of 0.2 to 1.0 mils (0.00508 to 0.0254 mm).

6. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium-rich cathodic arc coating is resistant to hot corrosion at a temperature between 1200° F. and 1600° F.

7. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium-rich cathodic arc coating is resistant to stress corrosion.

8. The chromium-rich cathodic arc coating according to claim 1 , wherein the chromium-rich cathodic arc coating is resistant to low cycle fatigue.

9. The chromium-rich cathodic arc coating according to claim 1 , wherein the substrate comprises a blade root, internal surface of turbine blade, or the external surface of a turbine blade.

10. An article comprising:
a) a substrate;
b) a MCrAlY cathodic arc coating on the substrate, wherein M is a metal alloy comprising nickel, cobalt, iron, or a combination thereof and the cathodic arc coating comprises Si and 25 to 50% chromium by weight based on the weight of the MCrAlY; and
c) a diffused chromide coating atop the MCrAlY cathodic arc coating;
wherein the diffused chromide coating atop the MCrAlY has a higher content of chromium than the MCrAlY cathodic arc coating, the combined thickness of the diffused chromide coating and the MCrAlY cathodic arc coating is 2.5 to 3 mil (0.0635 to 0.0762 mm), and the diffused chromide coating and the MCrAlY cathodic arc coating have a chromium rich phase with a depth of 0.1 to 2.5 mils (0.00254 to 0.0635).

11. The article according to claim 10 , wherein the substrate comprises a blade root, internal surface of turbine blade, or the external surface of a turbine blade.

12. The article comprising according to claim 10 , wherein the MCrAlY comprises Si in the amount of 0.15 to 0.65% by weight based on the weight of the MCrAlY.

13. The article comprising according to claim 10 , wherein chromium rich phase has a depth of 0.2 to 1.0 mils (0.00508 to 0.0254 mm).

14. A method of producing a chromium-rich cathodic arc coating comprising steps of:
a) applying a MCrAlY cathodic arc coating on a substrate, wherein M is a metal alloy comprising nickel, cobalt, iron, or a combination thereof and the cathodic arc coating comprises Si and 25 to 50% chromium by weight based on the weight of the MCrAlY; and
b) applying a diffused chromide coating atop the MCrAlY cathodic arc coating at a temperature of 1800 to 2200° F.;
wherein the diffused chromide coating has higher content of chromium than the MCrAlY cathodic arc coating and the combined thickness of the diffused chromide coating, the MCrAlY cathodic arc coating is 2.5 to 3 mil (0.0635 to 0.0762 mm) and the chromium-rich cathodic arc coating has a chromium rich phase with a depth of 0.1 to 2.5 mils (0.00254 to 0.0635 mm).

15. The method of claim 14 , wherein the surface of the diffused chromide coating has a chromium content no less than 37% by weight.

16. The method of claim 15 , wherein the MCrAlY cathodic arc coating has a chromium content of between about 25% and 35% by weight based on the weight of the MCrAlY.

17. The method of claim 14 , wherein the chromium rich phase has a thickness of 0.2 to 1.0 mils (0.00508 to 0.0254 mm).

18. The method of claim 14 , wherein the method of applying the diffused chromide coating atop the MCrAlY comprises pack chromizing, slurry chromizing, vapor diffusion coating, or gas diffusion coating.

Assignees

• United Technologies Corp
• Raytheon Tech Corp

Inventors

• Trzcinski Frank J
• Balzano Thomas
• Sinesi Prentice M
• Livings Mark A
• Task Michael N

Classifications

• F01D5/288

  Protective coatings for blades · CPC title

• F05D2300/611

  Coating · CPC title

• C23C10/20

  only one element being diffused · CPC title

• C23C10/38

  Chromising · CPC title

• C23C14/14

  Metallic material, boron or silicon · CPC title