IP Library Granted Patent US 9,228,264
Granted Patent B2
US 9,228,264 · App. 13/270,466 · Granted Jan 5, 2016

Process for depositing a coating for protection against oxidation and against hot corrosion on a superalloy substrate

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Quick Facts
Patent No.
US 9,228,264
App. No.
13/270,466
Granted
Jan 5, 2016
Kind
B2
Abstract

To protect a superalloy substrate from oxidation and hot corrosion, disclosed herein is a process that deposits successive layers on the substrate, a first layer of aluminum and of at least one element capable of being alloyed with sulphur, and a second layer of a material that isolates the at least one element capable of being alloyed with sulphur.

Claims (20)

1. A process for protecting a metallic superalloy substrate against oxidation and hot corrosion, the process comprising

depositing, on the metallic superalloy substrate, a first layer of aluminium and at least one element capable of being alloyed with sulphur by a vapour phase aluminization process, and

depositing by chemical vapour deposition a second layer of a material that isolates said element capable of being alloyed with sulphur on the first layer,

wherein the first layer forms a diffusion zone between the metallic superalloy substrate and the second layer with an interface zone between the first and second layers; and

the vapour phase aluminization process is conducted so that the at least one element is alloyed with sulphur and has a concentration peak in the interface zone and coincides with a concentration peak of the sulphur at the interface zone.

2. The process according to claim 1 , further comprising providing a third layer comprising platinum on the second layer.

3. The process according to claim 2 , further comprising applying a diffusion heat treatment to enrich the first layer, the second layer or both with platinum from the third layer.

4. The process according to claim 2 , wherein the third layer further comprises at least 35 wt % of nickel.

5. The process according to claim 4 , wherein the third layer is formed by depositing a layer of platinum followed by depositing a layer of nickel.

6. The method according to claim 2 , further comprising depositing a ceramic layer on the third layer.

7. The process according to claim 1 , wherein the element capable of being alloyed with sulphur is a reactive element or a rare earth element.

8. The process according to claim 1 , wherein the material in the second layer that isolates said element capable of being alloyed with sulphur is aluminium.

9. The process according to claim 1 , wherein the element capable of being alloyed with sulphur is zirconium, hafnium, yttrium, silicon, cerium or lanthanum or gadolinium.

10. The process according to claim 1 , wherein the element capable of being alloyed with sulphur is zirconium.

11. The process according to claim 1 , wherein the depositing of the first layer of aluminium and at least one element capable of being alloyed with sulphur by a vapour phase aluminization process comprises contacting the substrate and an aluminium alloy with a gas in a treatment chamber, the gas comprising a carrier gas and an activator and the activator reacts with the aluminium alloy to form a gaseous aluminium halide that decomposes at the surface of the substrate to deposit aluminium and the element capable of being alloyed with sulphur.

12. The process according to claim 11 , wherein the contacting in the treatment chamber is conducted at a temperature of from 950 to 1200° C.

13. The process according to claim 11 , wherein the element capable of being alloyed with sulphur is zirconium.

14. The process according to claim 13 , wherein the activator is a zirconium salt.

15. The process according to claim 11 , wherein the temperature in the treatment chamber is raised from ambient temperature at a rate of 4 to 20° C. per minute.

16. The process according to claim 11 , wherein the gas is circulated through the chamber when the temperature of the treatment chamber is above 700° C.

Assignments (3)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Oct 11, 2011
From: MENUEY, JUSTINE; HAMADI, SARAH; MALIE, ANDRE HUBERT LOUIS
To: SNECMA
Reel/Frame 027043/0739 →