Thrust plate for butterfly valve

Patent metadata

Field	Value
Publication number	US-9816619-B2
Application number	US-201113007850-A
Country	US
Kind code	B2
Filing date	Jan 17, 2011
Priority date	Jan 17, 2011
Publication date	Nov 14, 2017
Grant date	Nov 14, 2017

Abstract

A thrust plate for a butterfly valve includes a thrust plate body that defines a recess. The recess extends between a bottom thrust surface, side walls and an open top. A wear-resistant coating is located on the bottom thrust surface.

First claim

What is claimed is:

1. A thrust plate for a butterfly valve, the thrust plate comprising:
a thrust plate body defining a recess that extends between a bottom thrust surface, side walls and an open top; and
a wear-resistant coating located on the bottom thrust surface, the wear-resistant coating consisting essentially of 0.5-1.0 wt. % carbon, 12-18 wt. % chromium, 2.5-4.5 wt. % boron, 3.5-5.5 wt. % silicon, 3.5-5.5 wt. % iron, up to 0.2 wt. % cobalt, and a remainder of nickel, wherein the hardness of the wear-resistant coating is greater than the hardness of the thrust plate body.

2. The thrust plate as recited in claim 1 , wherein the wear-resistant coating includes chromium boride.

3. The thrust plate as recited in claim 1 , wherein the wear-resistant coating includes chromium carbide.

4. The thrust plate as recited in claim 1 , wherein the thrust plate body is a material selected from a group consisting of nickel-based alloy, cobalt-based alloy and steel.

5. The thrust plate as recited in claim 1 , wherein the thrust plate body, with the exception of the bottom thrust surface, is free of the wear-resistant coating.

6. The thrust plate as recited in claim 1 , wherein the recess defines a recess diameter (RD 1 ) and the wear-resistant coating defines an average coating thickness (CT), and ratio RD 1 /CT is between 33.2 and 56.67.

7. The thrust plate as recited in claim 1 , wherein the recess defines a recess depth (RD 2 ) and the wear-resistant coating defines an average coating thickness (CT), and a ratio RD 2 /CT is between 5 and 10.33.

8. The thrust plate as recited in claim 1 , wherein the recess defines a recess depth (RD 2 ) and the wear-resistant coating defines an average coating thickness (CT), and a ratio RD 2 /CT is between 5 and 10.33, and the recess depth is taken from a step in the recess to the bottom surface.

9. The thrust plate as recited in claim 1 , wherein the thrust plate body is stainless steel.

10. The thrust plate as recited in claim 9 , wherein a ratio of a hardness, in Rockwell C, of the wear-resistant coating to a hardness, in Rockwell C, of the stainless steel is at least 2.3.

11. The thrust plate as recited in claim 1 , wherein the recess includes a step therein.

12. The thrust plate as recited in claim 11 , wherein the step is sloped with respect to the bottom thrust surface and the side walls.

13. A butterfly valve comprising:
a valve housing defining a flow passage there through;
a shaft extending in the valve housing and including a butterfly disk mounted thereon within the flow passage;
a thrust plate including a thrust plate body defining a recess that receives an end of the shaft, and the recess extends between a bottom thrust surface, side walls and an open top; and
a wear-resistant coating located on the bottom thrust surface, wherein the recess defines a recess diameter (RD 1 ) and the wear-resistant coating defines an average coating thickness (CT), and ratio RD 1 /CT is between 33.2 and 56.67.

14. The butterfly valve as recited in claim 13 , wherein the flow passage defines a central axis, and a long axis of the shaft is non-perpendicular to the central axis.

15. The butterfly valve as recited in claim 13 , wherein the flow passage defines a diameter (D p ) in inches and the shaft contacts the wear-resistant coating over an interface area (CA) in square inches such that a ratio of D p /CA is between 8 and 12 in/in 2 .

16. The butterfly valve as recited in claim 13 , wherein the recess defines a recess depth (RD 2 ) and the wear-resistant coating defines an average coating thickness (CT) such that a ratio RD 2 /CT is between 5 and 10.33.

17. The butterfly valve as recited in claim 13 , wherein the thrust plate body is stainless steel and the wear-resistant coating is selected from a group consisting of a nickel-based alloy and a cobalt-based alloy.

18. The butterfly valve as recited in claim 13 , wherein wear-resistant coating consists essentially of 0.5-1.0 wt. % carbon, 12-18 wt. % chromium, 2.5-4.5 wt. % boron, 3.5-5.5 wt. % silicon, 3.5-5.5 wt. % iron, up to 0.2 wt. % cobalt, and a remainder of nickel.

19. The butterfly valve as recited in claim 13 , wherein an end of the shaft contacts the wear-resistant coating.

20. The butterfly valve as recited in claim 19 , wherein the flow passage defines a central axis, and a long axis of the shaft is non-perpendicular to the central axis such that the shaft is operable to produce a thrust load directed into the recess.

21. A method of installing a thrust plate on a butterfly valve, the method comprising:
securing a thrust plate to a valve housing that defines a flow passage there through such that an end of a shaft, which extends within the valve housing and includes a butterfly disk mounted thereon, is received into a recess of the thrust plate body, the recess extends between a bottom thrust surface, side walls and an open top, and the bottom thrust surface includes a wear-resistant coating thereon, the wear-resistant coating consisting essentially of 0.5-1.0 wt. % carbon, 12-18 wt. % chromium, 2.5-4.5 wt. % boron, 3.5-5.5 wt. % silicon, 3.5-5.5 wt. % iron, up to 0.2 wt. % cobalt, and a remainder of nickel.

22. The method as recited in claim 21 , including contacting the end of the shaft with the wear-resistant coating.

23. The method as recited in claim 21 , wherein the securing of the thrust plate to the valve housing includes bolting the thrust plate to the housing.

24. The method as recited in claim 21 , wherein the flow passage defines a diameter (D p ) and the shaft contacts the wear-resistant coating over an interface area (CA) such that a ratio of D p /CA is between 8 and 12.

Assignees

• Dowd Peter J
• Dehais John M
• Smith Blair A
• Boysen Timothy R
• Brooky Keith J
• Nardi Aaron T
• Rankin Kevin M
• Hamilton Sundstrand Corp

Inventors

• Dowd Peter J
• Dehais John M
• Smith Blair A
• Boysen Timothy R
• Brooky Keith J
• Nardi Aaron T
• Rankin Kevin M

Classifications

• F16K1/225 Primary

  the axis of rotation having only one bearing · CPC title

• F16K27/0218

  Butterfly valves · CPC title

• F16K1/22

  with axis of rotation crossing the valve member, e.g. butterfly valves · CPC title

• Y10T29/49412

  with assembly, disassembly or composite article making · CPC title