IP Library Granted Patent US 8,815,342
Granted Patent B2
US 8,815,342 · App. 13/808,708 · Granted Aug 26, 2014

Process for forming a protective coating on the surface of a metal part

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Quick Facts
Patent No.
US 8,815,342
App. No.
13/808,708
Granted
Aug 26, 2014
Kind
B2
Abstract

The present invention relates to a process for forming on the surface of a metal part a protective coating containing aluminium and zirconium, in which process said part and a cement made of an aluminium alloy are brought into contact with a gas at a treatment temperature in a treatment vessel, the gas comprising a carrier gas and an activator, the activator reacting with the cement to form a gaseous aluminium halide that decomposes on the surface of the part, depositing metallic aluminium thereon, the activator containing a zirconium salt such as ZΓO (¾ obtained from granules of a zirconium salt), disassociation reactions of said zirconium salt taking place within a disassociation temperature range with formation of a Zr metal coating on the surface of the part, the assembly comprising the part, the cement and the zirconium salt granules is progressively heated in the chamber from room temperature up to the treatment temperature, the process being characterized in that the treatment chamber is maintained at an overpressure with no carrier gas flow throughout the temperature range corresponding to the disassociation reactions of the zirconium salt.

Claims (23)

1. A process for forming a protective coating comprising aluminum and zirconium on a surface of a metal part, the process comprising:

gradually heating the metal part, a cement that comprises an aluminum alloy, and zirconium salt granules from an ambient temperature up to a treatment temperature while maintaining at an over-pressure in a treatment chamber, thereby dissociating zirconium salt granules to obtain a zirconium salt as an activator and depositing Zr metal at the surface of the metal part and

contacting the metal part and the cement with a gas comprising a carrier gas and an activator at a treatment temperature

thereby reacting the activator with the cement and generating a gaseous aluminum halide, which is capable of decomposing at the surface of the metal part and depositing metallic aluminum thereon,

wherein the gradually heating does not comprise circulating a carrier gas through the treatment chamber over a temperature interval corresponding to a dissociation reaction of the zirconium salt and wherein the carrier gas is circulated after a temperature of the treatment chamber has exceeded said temperature interval,

so that a diffused aluminization layer is formed on the surface,

so that an additional aluminization layer forms on the diffused aluminization layer, and

so that a majority of the zirconium is deposited at the interface of the diffused aluminization layer and the additional aluminization layer.

2. The process of claim 1 , wherein the gradually heating comprises a holding between 200° C. and 700° C.

3. The process of claim 2 , wherein a duration of the holding is from 5 to 30 minutes.

4. The process of claim 1 , wherein the gradually heating has a temperature rise rate of between 4° C. and 20° C. per minute.

5. The process of claim 1 , wherein the activator further comprises an ammonium halide.

6. The process of claim 1 , wherein the carrier gas is a reducing gas or a neutral gas.

7. The process of claim 6 , wherein the carrier gas is H 2 .

8. The process of claim 6 , wherein the carrier gas is argon.

9. The process of claim 1 , wherein the metal part comprises a nickel-based superalloy.

10. The process of claim 1 , wherein a zirconium element is partly replaced by hafnium or yttrium.

11. The process of claim 1 , wherein the treatment temperature is between 950° C. and 1200° C.

12. The process of claim 1 , wherein the gradually heating comprises a holding between 300° C. and 600° C.

13. The process of claim 1 , wherein the treatment temperature is approximately 1100° C.

14. The process of claim 1 , wherein the zirconium salt is ZrOCl 2 .

15. The process of claim 1 , wherein the treatment chamber is semi-sealed.

16. The process of claim 1 , wherein the aluminum alloy comprises chromium.

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 Jan 11, 2013
From: MENUEY, JUSTINE; MALIE, ANDRE HUBERT LOUIS
To: SNECMA
Reel/Frame 029610/0878 →