Process for producing a thermal barrier in a multilayer system for protecting a metal part and part equipped with such a protective system

Patent metadata

Field	Value
Publication number	US-10851667-B2
Application number	US-201816189712-A
Country	US
Kind code	B2
Filing date	Nov 13, 2018
Priority date	Mar 7, 2011
Publication date	Dec 1, 2020
Grant date	Dec 1, 2020

Abstract

A first ceramic (2a), referred to as the inner ceramic, is designed to have a substantially higher expansion coefficient. The outer ceramic (2b) is designed to have at least lower thermal conductivity, and a sintering temperature and/or maximum operating temperature that is substantially higher. The thermal barrier (23) has a composition and porosity gradient (3) from the metal sub-layer (21) to the outer ceramic (2b).

First claim

The invention claimed is:

1. A metal part made of superalloy, equipped with a thermal barrier being formed by a flash sintering operation in an SPS machine enclosure,
wherein the metal part comprises
a substrate, and
a thermal barrier comprising at least two ceramic layers consisting of zirconium-based refractory ceramic, at least one layer is an inner ceramic layer of zirconium-based refractory ceramic, and at least one layer is an outer ceramic layer of zirconium-based refractory ceramic having an outer face and being disposed over the inner ceramic layer,

wherein the thermal barrier has a porosity gradient, with porosity increasing from the outer ceramic layer to the inner ceramic layer with regard to the metal part,
wherein
(i) the outer ceramic layer has at least one physicochemical resistance property to calcium-magnesium-aluminum-silicate oxide pollutants which is higher than that of the inner ceramic layer, or
(ii) the outer ceramic layer has a higher thermal resistance property than that of the inner ceramic layer

wherein the thermal barrier formed by the flash sintering operation is a monolayer having a gradient of properties from the metal part to the outer face of the outer ceramic layer corresponding to the gradient of initial properties of the inner ceramic layer and the outer ceramic layer, and
wherein the inner ceramic layer has a higher thermal expansion coefficient than the outer ceramic layer.

2. The metal part according to claim 1 , wherein the substrate comprises a nickel-based superalloy.

3. The metal part according to claim 1 , wherein the metal part comprises a metal sub-layer.

4. The metal part according to claim 3 , wherein the metal sub layer has a platinum enriched beta-(Ni,Pt)Al phase, and an alpha-NiPtAl phase, or both, and a TGO oxide layer formed by thermal growth during flash sintering.

5. The metal part according to claim 3 , wherein the inner ceramic layer is chemically and thermally compatible with the sub-layer.

6. The metal part according to claim 1 , wherein the physicochemical resistance property of the outer ceramic layer is at least one selected from the group consisting of sintering, corrosion, erosion and aerodynamics, wherein the property is implemented by a selection of ceramics that is at least one selected from the group consisting of thermal conductivity, porosity, hardness, and roughness that is reinforced by the flash sintering so that the outer ceramic layer has, relative to the inner ceramic layer, at least one of the properties selected from the group consisting of lower thermal expansion, greater hardness, lower thermal conductivity, higher sintering temperature, lower open porosity and less roughness.

7. The metal part according to claim 6 , wherein the outer ceramic layer has lower thermal conductivity than that of the inner ceramic layer, and a natural sintering temperature, a maximum operating temperature, or both, that is substantially higher than that of the inner layer.

8. The metal part according to claim 6 , wherein the thermal barrier has a composition and porosity gradient from the metal sub-layer to the outer face, and functions for anchoring to the metal sub-layer, and for protecting, the outer face, smoothing the outer face, or both.

9. The metal part according to claim 1 , wherein the inner ceramic layer is selected from the group consisting of a YSZ compound of zirconia partially stabilized with yttria, a GYSZ compound of YSZ doped with gadolinium oxide, a LZ compound of lanthanum zirconate and a LZC compound of partially ceriated lanthanum zirconates.

10. The metal part according to claim 9 , wherein the inner and outer ceramic layers are selected from the group consisting of xYSZ/LZ, xYSZ/LZC and xYSZ/GYSZ, wherein x is a percentage by mass of yttria greater than or equal to 7% by mass.

11. The metal part according to claim 9 , wherein the LZC compounds are LZyC(1-y), wherein y=70%, y and 1-y are additional percentages of zirconium and partially ceriated zirconate cerium, and the doped YSZ compounds are tGvYSZ, wherein a percentage t by mass of gadolinium oxide is equal to 2% and a percentage v by mass of YSZ is equal to 8% by mass.

12. The metal part according to claim 10 , wherein x=7% by mass.

13. The metal part according to claim 10 , wherein x=8% by mass.

14. The metal part according to claim 1 , wherein the porosity of the thermal barrier is between 15% and 25%.

15. The metal part according to claim 1 , wherein the porosity of the outer ceramic layer is less than 15%.

16. The metal part according to claim 1 , wherein the roughness of the outer ceramic layer is less than 10 micrometers.

17. A metal part made of superalloy and comprising an assembly of layers of material comprising:
a substrate comprising a nickel-based superalloy,
a metal sub-layer, and
a thermal barrier, said thermal barrier comprising at least one inner ceramic layer consisting of zirconium-based refractory ceramic and at least one outer ceramic layer consisting of zirconium-based refractory ceramic having an outer face, said outer ceramic layer of zirconium-based refractory ceramic being disposed over the inner ceramic layer,
wherein (i) the outer ceramic layer has at least one physicochemical resistance property to calcium-magnesium-aluminum-silicate oxide pollutants which is higher than that of the inner ceramic layer, (ii) the outer ceramic layer has a higher thermal resistance property than that of the inner ceramic layer, or (iii) both (i) and (ii),
the thermal barrier being a continuous structure having a porosity gradient with porosity increasing from the outer face of the outer ceramic layer to the oxide layer formed on the metal part, and
wherein the inner ceramic layer has a higher thermal expansion coefficient than the outer ceramic layer.

18. The metal part according to claim 17 , wherein the assembly has undergone a flash sintering operation.

19. The metal part according to claim 18 , wherein the metal part comprises an oxide layer formed thereon during the flash sintering operation.

Assignees

• Safran Aircraft Engines
• Centre Nat Rech Scient
• Inst Nat Polytechnique Toulouse
• Univ Paul Sabatier De Toulouse

Inventors

• Hugot Juliette
• Boidot Mathieu
• Monceau Daniel
• Oquab Djar
• Estournes Claude

Classifications

• C23C24/082 Primary

  without intermediate formation of a liquid in the layer · CPC title

• C23C28/00 Primary

  Coating for obtaining at least two superposed coatings either by methods not provided for in a single one of groups C23C2/00 - C23C26/00 or by combinations of methods provided for in subclasses C23C and C25C or C25D · CPC title

• F01D5/288

  Protective coatings for blades · CPC title

• C23C28/3455

  with a refractory ceramic layer, e.g. refractory metal oxide, ZrO2, rare earth oxides or a thermal barrier system comprising at least one refractory oxide layer · CPC title

• C23C24/08

  by application of heat or pressure and heat (C23C24/04 takes precedence) · CPC title