Method for producing a hydrostatic fluid bearing with cells

Patent metadata

Field	Value
Publication number	US-10995796-B2
Application number	US-201515519009-A
Country	US
Kind code	B2
Filing date	Oct 12, 2015
Priority date	Oct 14, 2014
Publication date	May 4, 2021
Grant date	May 4, 2021

Abstract

The method comprises depositing a coating of metal material on the inside surface of the body ( 4 ) of the stator ( 36 ), impregnating said coating with a self-lubricating composite material ( 20 ), machining internal cells ( 28 ) in the thickness of the coating ( 10 ), and machining orifices ( 34 ) leading into the cells.

First claim

The invention claimed is:

1. A method of fabricating a hydrostatic fluid bearing comprising a stator having a right circular cylindrical inside surface of a body of the stator that includes cells, the method comprising the following successive steps:
depositing a coating of metal material on the right circular cylindrical inside surface of the body of the stator;
impregnating said coating with a self-lubricating composite material;
machining the cells in a direction of a thickness of the coating so that a periphery of each of the cells is surrounded by the right circular cylindrical inside surface of the stator, and machining orifices leading into the cells, wherein the thickness of the coating is in the range 0.8 mm to 2 mm, and the cells have a depth in the direction of the thickness of the coating in the range 0.3 mm to 0.6 mm.

2. A method according to claim 1 , wherein the metal material comprises bronze.

3. A method according to claim 1 , wherein the self-lubricating composite material comprises polytetrafluoroethylene.

4. A method according to claim 1 , wherein after impregnating the coating, the coated right circular cylindrical inside surface is subjected to re-boring.

5. A method according to claim 1 , wherein the coating is deposited by thermally spraying particles of the metal material against the right circular cylindrical inside surface of the stator.

6. A method according to claim 1 , wherein the coating is deposited in an environment that is less oxidizing than air.

7. A method according to claim 1 , wherein the coating is deposited by making at least one internal layer of coating against the right circular cylindrical inside surface and making at least one top layer of coating against said internal layer, the top layer presenting porosity that is greater than the porosity of the internal layer.

8. A method according to claim 1 , wherein deposition of the coating is followed by heat treatment, that precedes impregnating the coating.

9. A method according to claim 1 , wherein the coating is impregnated by applying the composite material to the coating and pressing it against the coating.

10. A method according to claim 1 , wherein the coating is impregnated by applying the self-lubricating composite material to the coating in the form of a paste.

11. A method according to claim 1 , wherein, while machining the internal cells, the coated right circular cylindrical inside surface is subjected to the re-boring.

12. A method according to claim 1 , wherein the coating is deposited in a closed enclosure in which there is an inert gas.

13. A method according to claim 1 , wherein machining the cells in the thickness of the coating comprises machining at least three internal cells.

14. A method of fabricating a hydrostatic fluid bearing comprising a stator having a right circular cylindrical inside surface of a body of the stator that includes cells, the method comprising the following successive steps:
depositing a coating of metal material on the right circular cylindrical inside surface of the body of the stator;
impregnating said coating with a self-lubricating composite material;
machining the cells by removing a partial thickness of the coating in a radial direction of the body of the stator so that a periphery of each of the cells is surrounded by the right circular cylindrical inside surface of the stator, and machining orifices leading into the cells, wherein the thickness of the coating in the radial direction is in the range 0.8 mm to 2 mm, and the cells have a depth in the radial direction in the range 0.3 mm to 0.6 mm.

15. A method according to claim 14 , wherein machining the cells in the thickness of the coating comprises machining at least three internal cells.

Assignees

• Safran Aircraft Engines

Inventors

• Geffroy Christian
• Le Foulon John-Fitzgerald
• Ridelaire Pascal

Classifications

• F16C33/14

  Special methods of manufacture; Running-in · CPC title

• F16C33/12

  Structural composition; Use of special materials or surface treatments, e.g. for rust-proofing · CPC title

• F16C32/06 Primary

  with moving member supported by a fluid cushion formed, at least to a large extent, otherwise than by movement of the shaft, e.g. hydrostatic air-cushion bearings · CPC title

• F02K9/48

  driven by a gas turbine fed by propellant combustion gases {or fed by vaporized propellants or other gases} · CPC title

• F16C2202/10

  Porosity · CPC title