Friction adjustment interface between two parts made of nickel or nickel or cobalt-chromium alloy that are in relative motion against one another at high temperature

Patent metadata

Field	Value
Publication number	US-10113224-B2
Application number	US-201615294092-A
Country	US
Kind code	B2
Filing date	Oct 14, 2016
Priority date	Oct 16, 2015
Publication date	Oct 30, 2018
Grant date	Oct 30, 2018

Abstract

An adjustment interface inserted between a first part made of nickel or made of nickel alloy or made of cobalt-chromium alloy in relative motion with a second part made of nickel or made of nickel alloy or made of cobalt-chromium alloy. The interface includes a first adjustment layer on one of the two parts and has a composition that makes it possible, with the friction with the other part, to create a glaze-type layer. A second adjustment layer is deposited on the second part for cooperation with the first layer to act as a catalyst for the oxide formed by friction with the first layer. The first glaze layer of the interface improves the sliding of the parts under friction. The catalyst function provided by the second layer makes it possible to stabilize the oxide formed by friction and to thus ensure a lubrication function over an extended high-temperature range.

First claim

The invention claimed is:

1. An adjustment interface inserted between a first part made of nickel, a nickel alloy or a cobalt-chromium alloy that is in relative motion with a second part made of nickel, a nickel alloy or a cobalt-chromium alloy, wherein the adjustment interface comprises two adjustment layers comprising:
a first adjustment layer deposited on the first part of the two parts and having a composition that makes it possible, with the friction with the second part, to create a glaze-type layer;
a second adjustment layer deposited on the second part for cooperation with the first adjustment layer by acting as a catalyst for an oxide formed by friction with the first adjustment layer.

2. The adjustment interface according to claim 1 , wherein the first adjustment layer is an alloy of cobalt, chromium, molybdenum and silicon.

3. The adjustment interface as claimed in claim 1 , wherein the first adjustment layer is pre-oxidized at a minimum temperature of 525° C. and a maximum temperature of 650° C. before being subjected to friction.

4. The adjustment interface according to claim 1 , wherein the first adjustment layer has a hardness lower than that of the first part, the first adjustment layer having a microporous morphology, giving the first adjustment layer a role of adapting elasto-plastic properties via a porosity compaction mechanism.

5. The adjustment interface according to claim 1 , wherein the first adjustment layer has an overall density of micropores of between 2% and 30%.

6. The adjustment interface according to claim 1 , wherein the first adjustment layer has a thickness of between 50 μm and 200 μm after grinding.

7. The adjustment interface according to claim 1 , wherein the first adjustment layer has an elastic deformability of 80 GPa as Young's modulus.

8. The adjustment interface according to claim 1 , wherein the second adjustment layer is produced by thermochemical carbon diffusion treatment at a surface of the second part.

9. The adjustment interface according to claim 8 , wherein the treated surface is made of nickel alloy 718.

10. The adjustment interface according to claim 9 , wherein the second adjustment layer has a surface hardness of greater than 850 HV.

11. The adjustment interface according to claim 8 , wherein the second adjustment layer has a surface hardness of greater than 850 HV.

12. The adjustment interface according to claim 8 , wherein the second adjustment layer has a diffusion depth or treatment thickness of from 10 to 15 μm and a hardness of greater than 800 HV over the first 5 μm in the depth of the second adjustment layer.

13. A process for depositing the first adjustment layer on the first part made of nickel, a nickel alloy or a cobalt-chromium alloy according to claim 1 , wherein the process is a thermal spray coating deposition process comprising:
pretreating a surface of the first part to such that adhesion between the first part and the first adjustment layer withstands a tensile stress at least equal to 35 MPa;
forming the first adjustment layer from a succession of passes of sprayings of metal particles in a molten state onto the surface of the first part, the first adjustment layer being a stack of lamellae, each lamella having a minimum thickness of 15 μm.

14. The process according to claim 13 , comprising grinding the coating to obtain a final thickness.

15. The process according to claim 13 , comprising a post-spraying oxidation carried out at a temperature of 525° C. for 22 hours in an atmosphere of oxygen.

16. A process for depositing the second adjustment layer on the second part made of nickel, a nickel alloy or a cobalt-chromium alloy according to claim 1 , wherein the process comprises a thermochemical carbon diffusion treatment at a surface of the second part.

17. An articulation device comprising the adjustment interface according to claim 1 , the adjustment interface being inserted between the first part having a small kinematic length and the second part having a large kinematic length constituting the articulation device, the first adjustment layer of the adjustment interface applied to the small kinematic length and the second adjustment layer of the adjustment interface applied to the large kinematic length.

Assignees

• Airbus Operations Sas

Inventors

• Poupon Cédric

Classifications

• C22F1/10

  of nickel or cobalt or alloys based thereon · CPC title

• C23C4/123 Primary

  Spraying molten metal · CPC title

• C23C4/08

  containing only metal elements (C23C4/073 takes precedence) · CPC title

• C23C4/18

  After-treatment · CPC title

• C23C8/12

  using elemental oxygen or ozone · CPC title