Coating for protection against oxidation and against hot corrosion on a superalloy substrate

Patent metadata

Field	Value
Publication number	US-10745800-B2
Application number	US-201514944412-A
Country	US
Kind code	B2
Filing date	Nov 18, 2015
Priority date	Oct 14, 2010
Publication date	Aug 18, 2020
Grant date	Aug 18, 2020

Abstract

To protect a superalloy substrate from oxidation and hot corrosion, disclosed herein is coating made by a process that deposits successive layers on the substrate, a first layer of aluminium 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.

First claim

The invention claimed is:

1. A metallic superalloy substrate, comprising sulphur and a coating that protects the metallic superalloy substrate against oxidation and hot corrosion, the coating comprising
a first layer comprising aluminium and a reactive element that is capable of being alloyed with the sulphur the reactive element being selected from the group consisting of zirconium, hafnium, yttrium, cerium, lanthanum and gadolinium, the first layer forming a diffusion zone above the metallic superalloy substrate, and
a second layer disposed on the first layer, the second layer comprising a material that isolates and traps the reactive element and the sulphur in the second layer,
wherein the reactive element capable of being alloyed with sulphur has a concentration peak in an interface zone and coincides with a concentration peak of the sulphur at the interface zone, and
wherein the metallic superalloy substrate and the coating is subjected to diffusion heat treatment so that the reactive element stops progressions of the sulfur towards the external surface of the second layer and traps sulfur in the interface zone, the reactive element and the sulphur are not present on the external surface of the second layer to avoid oxidation.

2. The metallic superalloy substrate of claim 1 , wherein the first layer is formed by a diffusion zone and an additional zone, the interface zone being formed between the diffusion zone and the additional zone, the reactive element is alloyed with sulfur and has a concentration peak in the interface zone between the diffusion zone and the additional zone, wherein the concentration peak of the reactive element coincides with a concentration peak of sulphur at the interface zone.

3. The metallic superalloy substrate of claim 1 , wherein the first layer forms a diffused layer and an additional layer, said additional layer comprising the reactive element, the reactive element having a concentration peak being at the interface between the diffused layer and the additional layer.

4. The metallic superalloy substrate of claim 1 , wherein the reactive element is alloyed with sulphur and isolates the sulphur between the first and second layers.

5. A coated metallic superalloy substrate obtained by a process comprising
depositing, on the metallic superalloy substrate, a first layer of aluminium and an element capable of being alloyed with sulphur by a vapour phase aluminization process,
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, and
diffusion heat treating the metallic superalloy substrate,
wherein
the reactive element being selected from the group consisting of zirconium, hafnium, yttrium, cerium, lanthanum and gadolinium, the first layer forming a diffusion zone above the metallic superalloy substrate,
wherein the reactive element capable of being alloyed with sulphur has a concentration peak in an interface zone and coincides with a concentration peak of the sulphur at the interface zone between the first and second layers, and
after diffusion heat treatment of the metallic superalloy substrate and the coating, the reactive element stops progressions of the sulfur towards the external surface of the second layer and traps sulfur in the interface zone, the reactive element and the sulphur are not present on the external surface of the second layer to avoid oxidation.

6. The coated metallic superalloy substrate of claim 5 , further comprising a third layer disposed on the second layer, the third layer comprising platinum.

7. The coated metallic superalloy substrate of claim 6 , further comprising a ceramic layer on the third layer.

8. The metallic superalloy substrate of claim 6 , wherein the second layer comprises aluminium and platinum after the diffusion heat treatment.

9. The coated metallic superalloy substrate of claim 5 , wherein the element capable of being alloyed with sulphur is zirconium.

10. A coated metallic superalloy substrate comprising:
a substrate comprising sulfur,
a coating disposed on the substrate to protect said substrate against oxidation and hot corrosion, the coating having a surface and comprising:
a first layer comprising aluminium and a reactive element that is capable of being alloyed with the sulphur the reactive element being selected from the group consisting of zirconium, hafnium, yttrium, cerium, lanthanum and gadolinium, the first layer forming a diffusion zone above the metallic superalloy substrate, and
a second layer disposed on the first layer, the second layer comprising a material that isolates and traps the reactive element and the sulphur in the second layer,
wherein the reactive element capable of being alloyed with sulphur has a concentration peak in an interface zone and coincides with a concentration peak of the sulphur at the interface zone between the first and second layers, and
wherein after diffusion heat treatment of the metallic superalloy substrate and the coating, the reactive element stops progressions of the sulfur towards the external surface of the second layer and traps sulfur in the interface zone, the reactive element and the sulphur are not present on the external surface of the second layer to avoid oxidation.

Assignees

• Safran Aircraft Engines

Inventors

• Menuey Justine
• Hamadi Sarah
• Malie Andre Hubert Louis

Classifications

• C23C28/021 Primary

  including at least one metal alloy layer · CPC title

• Y10T428/12944

  Ni-base component · CPC title

• Y02T50/60

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

• Y10T428/12611

  Oxide-containing component · CPC title

• C23C14/16

  on metallic substrates or on substrates of boron or silicon · CPC title