Duplex-phase CrAl coating for improved corrosion/oxidation protection

Patent metadata

Field	Value
Publication number	US-9689270-B2
Application number	US-201313961965-A
Country	US
Kind code	B2
Filing date	Aug 8, 2013
Priority date	Aug 8, 2012
Publication date	Jun 27, 2017
Grant date	Jun 27, 2017

Abstract

Disclosed is a coating for protecting a component against high temperatures and aggressive media, which coating has at least one subregion whose main constituent is chromium. The layer additionally comprises aluminum, the chromium content at least in the subregion in which chromium is the main constituent being greater than 30% by weight and the aluminum content being greater than or equal to 5% by weight. The invention further provides a process for producing such a coating, comprising chromizing the surface to be coated and subsequently alitizing the chromium-rich layer produced during chromizing.

First claim

What is claimed is:

1. A process for producing a coating for protecting a component against high temperatures and aggressive media, the component being formed by an alloy having one or more metallic main constituents which make up the largest proportion of the alloy, wherein the process comprises chromizing a surface to be coated and subsequently aluminizing a chromium-rich layer produced during chromizing, the chromizing being carried out with a chemical chromium activity of at least 0.4, and wherein the process affords a coating that has an outer zone and an inner zone, the outer zone comprising α-chromium phases in a matrix of a mixture of mixed crystals comprising essentially chromium, aluminum, and the one or more metallic main constituents of the alloy, and the inner zone comprising a mixed crystal zone comprising essentially chromium, aluminum, and the one or more metallic main constituents of the alloy, the proportion of chromium in a total coating being greater than 30% by weight and a proportion of aluminum in a total coating being at least 5% by weight, and wherein at least one of:
(i) a proportion of chromium in the outer zone is from 30% by weight to 95% by weight of chromium;
(ii) a proportion of chromium in the α-chromium phases is at least 70% by weight;
(iii) a proportion of aluminum in the outer zone is from 10% to 40% by weight of aluminum;
(iv) the one or more metallic main constituents in the outer zone are present in a proportion of not higher than 40% by weight;
(v) in the inner zone a proportion of chromium is not higher than 30% by weight, a proportion of aluminum is not higher than 30% by weight, and a proportion of the one or more main constituents is at least 30% by weight;
(vi) a proportion of chromium in the total coating is from greater than 30% by weight to 90% by weight;
(vii) a proportion of aluminum in the total coating is from 10% to 40% by weight;
(viii) the outer zone of the coating makes up a proportion of at least 50% of the total coating;
(ix) the coating has up to 10% by volume of pores having average diameters of from 2 μm to 20 μm;
(x) the coating comprises from 1% to 15% by weight of oxides;
(xi) the one or more metallic main constituents of the alloy are one or more of nickel, iron and cobalt;
(xii) the chromizing is carried out using a Cr-rich slip containing a liquid phase.

2. The process of claim 1 , wherein the chromizing is carried out using a Cr-rich slip containing a liquid phase.

3. The process of claim 2 , wherein the slip is applied by injection molding.

4. The process of claim 1 , wherein the chromizing is carried out at a temperature of from 1020° C. to 1180° C. for a period of from 2 to 20 hours.

5. The process of claim 1 , wherein the aluminizing is carried out at a temperature of from 1050° C. to 1150° C. for a period of from 3 to 20 hours.

6. The process of claim 1 , wherein the chemical aluminum activity during aluminizing is at least 0.3.

7. The process of claim 1 , wherein a first aluminizing is followed by a second aluminizing at a lower chemical aluminum activity at a temperature of greater than or equal to 1050° C. for a period of from 3 to 20 hours.

8. The process of claim 1 , wherein the chromizing and aluminizing are followed by a diffusion heat treatment at a temperature of greater than or equal to 1050° C. for a period of from 2 to 8 hours.

9. The process of claim 1 , wherein a surface treatment by PVD, CVD, surface coating, electrochemical deposition and/or direct application of a material, in which one or more elements from the group platinum, palladium, hafnium, zirconium, yttrium and silicon are applied, is carried out before, during or after chromizing and/or aluminizing.

10. The process of claim 1 , wherein a proportion of chromium in the outer zone is from 30% by weight to 95% by weight of chromium.

11. The process of claim 1 , wherein a proportion of chromium in the α-chromium phases is at least 70% by weight.

12. The process of claim 1 , wherein a proportion of aluminum in the outer zone is from 10% to 40% by weight of aluminum.

13. The process of claim 1 , wherein the one or more metallic main constituents in the outer zone are present in a proportion of not higher than 40% by weight.

14. The process of claim 1 , wherein in the inner zone a proportion of chromium is not higher than 30% by weight, a proportion of aluminum is not higher than 30% by weight, and a proportion of the one or more main constituents is at least 30% by weight.

15. The process of claim 1 , wherein a proportion of chromium in the total coating is from greater than 30% by weight to 90% by weight.

16. The process of claim 5 , wherein a proportion of aluminum in the total coating is from 10% to 40% by weight.

17. The process of claim 4 , wherein the outer zone of the coating makes up a proportion of at least 50% of the total coating.

18. The process of claim 3 , wherein the coating has up to 10% by volume of pores having average diameters of from 2 μm to 20 μm.

19. The process of claim 2 , wherein the coating comprises from 1% to 15% by weight of oxides.

20. The process of claim 1 , wherein the one or more metallic main constituents of the alloy are one or more of nickel, iron and cobalt.

Assignees

• MTU Aero Engines AG

Inventors

• Pillhoefer Horst
• Mueller Stefan
• Bayer Erwin
• Dautl Thomas

Classifications

• C23C10/20 Primary

  only one element being diffused · CPC title

• F01D5/288 Primary

  Protective coatings for blades · CPC title

• C23C10/60

  After-treatment · CPC title

• Y10T428/12639

  Adjacent, identical composition, components · CPC title