High-temperature low-friction cobalt-free coating system for gate valves, ball valves, stems, and seats

Patent metadata

Field	Value
Publication number	US-11644106-B2
Application number	US-201917298383-A
Country	US
Kind code	B2
Filing date	Dec 18, 2019
Priority date	Dec 19, 2018
Publication date	May 9, 2023
Grant date	May 9, 2023

Abstract

A method of manufacturing a device includes thermally spraying tungsten carbine in feedstock that does not include Cobalt but that includes Nickel, Copper, or a Nickel-Copper alloy, the method improves the base coating toughness, anticorrosion, and antifouling properties for high load application in sea water and brackish water environments. Additionally, a Cobalt-free material lowers material costs and reduces the global demand of Cobalt. Providing a topcoat of a Silicon-doped DLC significantly reduces the topcoat brittleness of common DLC failures such as “egg shell” in high stress applications. Thus, high hardness, low friction applications may be tailored in high stress applications.

First claim

What is claimed is:

1. An apparatus for controlling well fluids, the apparatus comprising:
a gate valve having a body, the body having a cavity and a flow passage intersecting the cavity;
a seat ring mounted to the body at the intersection of the flow passage and the cavity, the seat ring having an engaging face formed of a steel alloy;
a gate in the cavity and having an engaging face formed of a steel alloy that slidingly engages the face of the seat ring while being moved between open and closed positions;
a hardened outer layer formed on the engaging face of the seat ring, the hardened layer formed of a Cobalt-free feedstock material and the hardened layer comprising Tungsten Carbide in a Cobalt-free matrix;
a friction-resistant coating of diamond-like carbon on the hardened outer layer, and
wherein the hardened layer exhibits two cracks or fewer per square inch, has an adhesion of 9,000 psi or greater, and has a porosity of 2 volume % or less.

2. The apparatus of claim 1 , wherein the Cobalt-free feedstock material comprises, in wt. %:
Ni: Balance
C: 0.5-2;
Cr: 10-30;
Mo: 5.81-18.2;
Nb+Ti: 2.38-10.

3. The apparatus of claim 1 , wherein the Cobalt-free feedstock material comprises, in wt. %:
Ni: Balance
C: about 0.84-about 1.56;
Cr: about 14-about 26;
Mo: about 8.4-about 15.6;
Nb: about 4.2-about 7.8; and
Ti: about 0.35-about 0.65.

4. The apparatus of claim 1 , wherein the Cobalt-free feedstock material comprises, in wt. %:
Ni: Balance
C: about 1.08-about 1.32;
Cr: about 13-about 22;
Mo: about 10.8-about 13.2; and
Nb: about 5.4-about 6.6.

5. The apparatus of claim 1 , wherein the Cobalt-free matrix of the hardened layer comprises a Nickel matrix comprising:
hard phases of 1,000 Vickers hardness or greater totaling 5 mol. % or greater;
20 wt. % or greater of a combined total of Chromium and Molybdenum;
isolated hypereutectic hard phases totaling to 50 mol. % or more of a total hard phase fraction;
a WC/Cr 3 C 2 ratio of 0.33 to 3;
an ASTM G65A abrasion loss of less than 250 mm 3 ; and
a Vickers hardness of 650 or greater.

6. The apparatus of claim 1 , wherein the hardened layer has a Vickers hardness of 750 or greater.

7. The apparatus of claim 1 , wherein the hardened layer has a porosity of 0.5 volume % or less.

8. The apparatus of claim 1 , wherein the hardened layer has a corrosion rate of 1 mpy or less in a 28% CaCl 2 ) electrolyte, pH=9.5 environment.

9. The apparatus of claim 5 , wherein the hardened layer has a corrosion rate that is less than 0.1 mpy in a 3.5% sodium chloride solution for 16 hours according to ASTM G59/ASTM G61.

10. The apparatus of claim 5 , wherein the Nickel matrix has a matrix proximity of 80% or greater as compared to a corrosion-resistant alloy defined by Ni: BAL, X>20 wt. %, wherein X represents at least one of Cu, Cr, or Mo.

11. The apparatus of claim 10 , wherein the corrosion-resistant alloy comprises an alloy having simple formula Ni30Cu.

12. The apparatus of claim 1 , wherein the hardened layer is a component of a hydraulic cylinder, tension riser, mud motor rotor, or oilfield component application.

13. The apparatus of claim 1 , wherein the Cobalt-free matrix forms a corrosion-resistant matrix, and under thermodynamic equilibrium conditions, the corrosion-resistant matrix has:
hard phases totaling 50 mol. % or greater; and
a liquidus temperature of 1550 K or lower.

14. The apparatus of claim 1 , wherein the Cobalt-free feedstock material comprises a blend of an alloy having simple formula Ni30Cu, and at least one of WC or Cr 3 C 2 .

15. The apparatus of claim 1 , wherein the Cobalt-free feedstock material is selected from the group consisting of, by wt.:
75-85% WC+15-25% Nickel-Copper alloy;
65-75% WC+25-35% Nickel-Copper alloy;
60-75% WC+25-40% Nickel-Copper alloy;
75-85% Cr 3 C 2 +15-25% Nickel-Copper alloy;
65-75% Cr 3 C 2 +25-35% Nickel-Copper alloy;
60-75% Cr 3 C 2 +25-40% Nickel-Copper alloy;
75-85% WC/Cr 3 C 2 +15-25% Nickel-Copper alloy;
65-75% WC/Cr 3 C 2 +25-35% Nickel-Copper alloy; and
60-75% WC/Cr 3 C 2 +25-40% Nickel-Copper alloy;
where the Nickel-Copper alloy is an alloy having simple formula Ni30Cu.

16. The apparatus of claim 13 , wherein a WC/Cr 3 C 2 ratio of the corrosion-resistant matrix is 0.2 to 5 by volume.

17. The apparatus of claim 1 , wherein the hardened layer comprises:
an ASTM G65A abrasion loss of less than 250 mm 3 ; and
two cracks or fewer per square inch when forming the hardened layer from a PTA or laser cladding process.

18. The apparatus of claim 17 , wherein the hardened layer comprises an impermeable HVOF coating which exhibits a corrosion rate of 1 mpy or less in a 28% CaCl 2 ) electrolyte, pH=9.5 environment.

19. The apparatus of claim 18 , wherein the hardened layer further comprises:
a Vickers hardness of 650 or greater; and
an adhesion of 9,000 psi or greater when forming the hardened layer from a HVOF thermal spray process.

20. The apparatus of claim 17 , wherein the hardened layer comprises:
a Vickers hardness of 750 or greater; and
a porosity of 0.5 volume % or less when forming the hardfacing layer from a HVOF thermal spray process.

21. The apparatus of claim 1 , wherein the coating of diamond-like carbon has a thickness of up to 30 microns.

22. A method of manufacturing the apparatus of claim 1 , the method comprising:
thermally spraying the tungsten carbide in the Cobalt-free feedstock to produce the hardened layer; and
applying the friction-resistant coating of diamond-like carbon to the hardened layer.

23. The method of claim 22 , further comprising applying a lubricant to the diamond-like layer.

24. The method of claim 22 , wherein the Cobalt-free feedstock is at least one of nickel feedstock, copper feedstock, and nickel-copper feedstock.

25. The method of claim 22 , wherein the coating of diamond-like carbon has a thickness of up to 30 microns.

Assignees

• Oerlikon Metco Us Inc

Inventors

• Williams Kevin
• Vecchio James
• Bracci Jonathon
• Cheney Justin
• Fiala Petr

Classifications

• C23C4/129

  Flame spraying · CPC title

• F16K25/005

  Particular materials for seats or closure elements · CPC title

• C22C29/08

  based on tungsten carbide · CPC title

• B22F5/10

  of articles with cavities or holes, not otherwise provided for in the preceding subgroups · CPC title

• F16K3/0263 Primary

  using particular material or covering means · CPC title