Process for manufacturing a part provided with a lubricating surface coating, part provided with such a coating and turbomachine

Patent metadata

Field	Value
Publication number	US-10266782-B2
Application number	US-201414787087-A
Country	US
Kind code	B2
Filing date	Apr 23, 2014
Priority date	Apr 26, 2013
Publication date	Apr 23, 2019
Grant date	Apr 23, 2019

Abstract

A process for manufacturing a part provided with a lubricating surface coating ( 10 ), in which: a composition is prepared that includes at least one precursor having at least one organic group, the composition is deposited on the part, a heat treatment is carried out, wherein the heat treatment of the coating is carried out at a temperature above 220° C., so as to form a lubricating surface coating ( 10 ) formed of an at least partially inorganic solid network incorporating solid carbon in at least one lubricating allotropic form in the dispersed state and trapped within the solid network. A part, such as a foil of a foil bearing ( 1 ) obtained by the process, a turbomachine, such as a turbomachine for a fuel cell, including such a part, and an aircraft cabin air-conditioning system including at least one such turbomachine are also described.

First claim

The invention claimed is:

1. A process for manufacturing a part provided with a lubricating surface coating, said part being chosen from a turbomachine foil bearing foil and a turbomachine axial thrust bearing foil wherein:
a composition comprising at least one precursor of said lubricating surface coating having at least one organic group is prepared,
said composition is deposited on at least a portion of a surface of said part, said portion of a surface of the part being formed of at least one metallic material,
after said composition has been deposited on the surface of said part, at least one heat treatment is carried out at a temperature greater than 220° C. so as to form a lubricating surface coating,
wherein said composition comprises at least one precursor of said lubricating surface coating chosen from the group formed of the alkoxides of the following general formula (I):
X(O—R 1 ) n′−a (R 2 ) a   (I)

wherein:
X is chosen from silicon (Si) and the metallic elements,
R 1 is chosen from the hydrocarbyl groups,
n′ is a natural integer representing the valence of the element X,
a is a natural integer of the interval [1; n′],
R 2 is chosen from the organic groups bonded to X by a carbon atom,

so as to form, at the end of said heat treatment, a lubricating surface coating formed of an inorganic solid network incorporating solid carbon in at least one lubricating allotropic form in a dispersed state and trapped within said solid network, said solid carbon lubricating allotropic form being at least graphene, said lubricating surface coating being free of organic groups and polymeric material and composed solely of a solid ceramic network incorporating said solid carbon, and said lubricating surface coating having a thickness of from 0.2 μm to 5 μm.

2. The process as claimed in claim 1 , wherein at least one organic group of at least one precursor of said lubricating surface coating is chosen from the hydrocarbyl groups, and wherein the heat treatment is carried out so as to form within said solid network at least one solid lubricating compound of carbon chosen from the group formed of graphene, graphite, amorphous carbon and mixtures thereof.

3. The process as claimed in claim 1 , wherein said composition comprises at least one precursor chosen from the group formed of the alkoxysilanes of the following general formula (II):
Si (O—R 1 ) 4−a (R 2 ) a   (II)

wherein:
R 1 is chosen from the hydrocarbyl groups,
a is a natural integer of the interval [1; 3],
R 2 is chosen from the organic groups bonded to silicon by a carbon atom.

4. The process as claimed in claim 1 , wherein said composition comprises at least one precursor chosen from the group formed of the metal alkoxides of the following general formula (III):
M(O—R 3 ) m   (III)

wherein:
M is a metallic element chosen from aluminium, titanium, zirconium and vanadium,
R 3 is a hydrocarbyl group of the formula [C n H 2n+1 ], n being an integer greater than or equal to 1,
m is a natural integer representing the valence of the metallic element M.

5. The process as claimed in claim 1 ,
wherein said heat treatment is carried out in an oxidizing atmosphere at a temperature of from 220° C. to 450° C.

6. The process as claimed in claim 1 , wherein said heat treatment is carried out in a non-oxidizing atmosphere at a temperature of from 300° C. to 800° C.

7. The process as claimed in claim 1 , wherein said composition is deposited on at least a portion of a surface of said part by a deposition technique chosen from dip coating, spray coating, centrifugation and screen printing.

8. The process as claimed in claim 1 , wherein, after said heat treatment, the part is deformed by bending.

9. A part provided with a lubricating surface coating, wherein said lubricating surface coating is formed of an inorganic solid network incorporating solid carbon in at least one lubricating allotropic form in a dispersed state and trapped within said solid network, said solid carbon being graphene, said lubricating surface coating being free of organic groups and polymeric material and composed solely of a solid ceramic network incorporating said solid carbon,
said part being formed of at least one metallic material and being chosen from a turbomachine foil bearing foil and a turbomachine axial thrust bearing foil and said lubricating surface coating having a thickness of from 0.2 μm to 5 μm, and
said coating being formed by at least one heat treatment carried out at a temperature greater than 220° C., after deposition of a composition comprising at least one precursor of said lubricating surface coating chosen from the group formed of the alkoxides of the following general formula (I):
X(O—R 1 ) n′−a (R 2 ) a   (I)

wherein:
X is chosen from silicon (Si) and the metallic elements,
R 1 is chosen from the hydrocarbyl groups,
n′ is a natural integer representing the valence of the element X,
a is a natural integer of the interval [1; n′],
R 2 is chosen from the organic groups bonded to X by a carbon atom.

10. The part as claimed in claim 9 , wherein said inorganic solid network is chosen from the group formed of metallic oxide networks, silicon oxide networks and mixtures thereof.

11. A turbomachine, especially a compressor, a turbine or a turbocompressor, comprising at least one part according to claim 9 .

12. An aircraft cabin air conditioning system comprising at least one turbomachine as claimed in claim 11 .

13. A fuel cell system comprising at least one turbomachine as claimed in claim 11 .

14. The process as claimed in claim 2 , wherein said composition comprises at least one precursor chosen from the group formed of the alkoxysilanes of the following general formula (II):
Si (O—R 1 ) 4−a (R 2 ) a   (II)

wherein:
R 1 is chosen from the hydrocarbyl groups,
a is a natural integer of the interval [1 ; 3],
R 2 is chosen from the organic groups bonded to silicon by a carbon atom.

Assignees

• Liebherr Aerospace Toulouse Sas
• Centre Nat Rech Scient
• Univ Toulouse 3 Paul Sabatier

Inventors

• Rahoui Souphiane
• Bonino Jean-Pierre
• Turq-Perrussel Viviane
• Rocchi Jerome

Classifications

• C23C18/122

  Inorganic polymers, e.g. silanes, polysilazanes, polysiloxanes · CPC title

• C23C18/04

  Pretreatment of the material to be coated (C23C18/06 takes precedence) · CPC title

• C23C18/1216

  Metal oxides (C23C18/1212 takes precedence) · CPC title

• Y02T50/6765

  Cross-Sectional Technologies · mapped topic

• C10M103/02 Primary

  Carbon; Graphite · CPC title