This application relates to a unique connector link for a butterfly valve.
Butterfly valves are known and are utilized in a number of applications. In general, a butterfly valve sits within a fluid flow duct and pivots between a blocking position and a flow allowing position. An actuator includes a piston which moves a link to pivot a connecting link. The connecting link then moves an arm to, in turn, pivot the butterfly valve within the duct between the restrictive and flow allowing positions.
In the prior art, the connecting link has had some deficiencies.
A connector link for use in an actuation system for a butterfly valve has a central web extending between two generally cylindrical ends. There are bores formed in each of two generally cylindrical ends and bushings extend axially upwardly from a nominal face at each of the ends. One of the ends has a bore formed at a radius defined as a first distance. A distance between center points of the bores in the first and second ends is defined as a second distance. The ratio of the second distance to the first distance is greater than or equal to 19.2772 and less than or equal to 19.4125. A valve and method are also disclosed.
These and other features may be best understood from the following drawings and specification.
A butterfly valve and actuation assembly 20 is illustrated in
As shown in
As shown in
In embodiments, a ratio of d2 to d1 is between 19.2772 and 19.4125.
One material utilized to form the connector link 30 is 17-7PH stainless steel. The bushings 31 are formed of Stellite 6B®. Stellite 6B® is a cobalt alloy, and is a registered trademark of Kennametal, Inc.
In the prior connecting link, the d1 dimension was 1.568 inches (3.982 centimeters) +/−0.0004 inch (0.0010 centimeter) and the d2 dimension was 3.070 inches (7.797 centimeters) +/−0.003 inch (0.008 cm).
Although an embodiment of this invention has been disclosed, a worker of ordinary skill in this art would recognize that certain modifications would come within the scope of this invention. For that reason, the following claims should be studied to determine the true scope and content of this invention.
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Number | Date | Country |
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WO 2014127793 | Aug 2014 | WO |
Number | Date | Country | |
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20160131262 A1 | May 2016 | US |