US2017343113A1PendingUtilityA1
Thrust plate for butterfly valve
Est. expiryJan 17, 2031(~4.5 yrs left)· nominal 20-yr term from priority
Inventors:Peter J. DowdJohn M. DehaisBlair A. SmithTimothy R. BoysenKeith J. BrookyAaron T. NardiKevin M. Rankin
F16K 1/22F16K 1/225Y10T29/49412F16K 27/0218
53
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Claims
Abstract
A thrust plate for a butterfly valve includes a thrust plate body that defines a recess that extends between a bottom thrust surface, side walls, and an open top. There is a nickel-based or cobalt-based wear-resistant coating located on the bottom thrust surface. The wear-resistant coating is harder than the thrust plate body.
Claims
exact text as granted — not AI-modifiedWhat 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 nickel-based or cobalt-based wear-resistant coating located on the bottom thrust surface, the wear-resistant coating being harder than the thrust plate body.
2 . The thrust plate as recited in claim 1 , wherein the wear-resistant coating is a nickel-based alloy.
3 . The thrust plate as recited in claim 1 , wherein the wear-resistant coating includes chromium boride.
4 . The thrust plate as recited in claim 1 , wherein the wear-resistant coating includes chromium carbide.
5 . The thrust plate as recited in claim 1 , wherein the thrust plate body is stainless steel.
6 . The thrust plate as recited in claim 5 , wherein a ratio of a hardness of the wear-resistant coating to a hardness of the stainless steel is at least 2.3.
7 . The thrust plate as recited in claim 6 , 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.
8 . The thrust plate as recited in claim 7 , 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.
9 . The thrust plate as recited in claim 8 , wherein the thrust plate body, with the exception of the bottom thrust surface, is free of the wear-resistant coating.
10 . 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, and the wear-resistant coating is a nickel-based alloy.
11 . 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.
12 . The butterfly valve as recited in claim 11 , wherein the 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
13 . The butterfly valve as recited in claim 11 , wherein the thrust plate body is stainless steel.
14 . The butterfly valve as recited in claim 13 , wherein a ratio of a hardness of the wear-resistant coating to a hardness of the stainless steel is at least 2.3.
15 . The butterfly valve as recited in claim 14 , 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.
16 . The butterfly valve as recited in claim 15 , 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.
17 . The butterfly valve as recited in claim 16 , wherein the thrust plate body, with the exception of the bottom thrust surface, is free of the wear-resistant coating.
18 . The butterfly valve as recited in claim 11 , wherein the flow passage defines a central axis, and a long axis of the shaft is non-perpendicular to the central axis.
19 . The butterfly valve as recited in claim 11 , wherein the recess defines a recess diameter (RD 1 ) and a recess depth (RD 2 ) and the wear-resistant coating defines an average coating thickness (CT) such that a ratio RD 1 /CT is between 33.2 and 56.67 and a ratio RD 2 /CT is between 5 and 10.33.
20 . 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.Cited by (0)
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