Butterfly valve with vibration resistant mount

Abstract

A valve member is mounted on a shaft to pivot within a fluid passage. A control selectively moves a piston in a linear direction to control a position of the valve member in the fluid passage. The piston causes a roller pin to move as the piston moves linearly. The roller pin is mounted in crank collars of a crank shaft such that movement of the roller pin causes the crank collars to rotate crank shaft rotating position, and the valve shaft. The roller pin is mounted within the crank collars by bearings. The bearings each have an outer race associated with a crank collar, an inner race associated with the roller pin, and bearing members separate the inner and outer race. There is a spring bias resisting movement of the inner races relative to said roller pin. An anti-ice system is also disclosed.

1 . A butterfly valve comprising:
 a valve member mounted on a shaft to pivot within a fluid passage;   an actuator including a piston having opposed piston heads associated with fluid chambers, and a control to move the piston in a linear direction to control a position of said valve member in said fluid passage, said piston causing a roller pin to move as said piston moves linearly, said roller pin mounted in crank collars of a crank shaft such that movement of said roller pin causes said crank shaft to rotate said valve shaft; and   said roller pin being mounted within said crank collars by bearings, said bearings each having an outer race associated with one of said crank collars, an inner race associated with said roller pin, and bearing members separating said inner and outer race, there being a spring bias resisting movement of said inner races relative to said roller pin.   
     
     
         2 . The butterfly valve as set forth in  claim 1 , wherein said roller pin having cavities associated with each of two axial ends, and receiving a spring member to apply said spring bias to each said inner race. 
     
     
         3 . The butterfly valve as set forth in  claim 2 , wherein said spring members are wave springs. 
     
     
         4 . The butterfly valve as set forth in  claim 3 , wherein a shim is positioned between each said wave spring and said inner race. 
     
     
         5 . The butterfly valve as set forth in  claim 2 , wherein a shim is positioned between said spring member and each said inner race. 
     
     
         6 . The butterfly valve as set forth in  claim 5 , wherein said roller pin moves within a slot in a connecting portion of said piston connecting said opposed piston heads. 
     
     
         7 . The butterfly valve as set forth in  claim 6 , wherein said roller pin has an internal bore and a bearing retention bolt extends through said inner bore and receives a nut at a remote end to secure said roller pin within said crank collars. 
     
     
         8 . The butterfly valve as set forth in  claim 7 , wherein said nut is welded to said remote end of said bolt. 
     
     
         9 . The butterfly valve as set forth in  claim 1 , wherein said roller pin moves within a slot in a connecting portion of said piston connecting said opposed piston heads, wherein said roller pin has an internal bore and a bearing retention bolt extends through said inner bore and receives a nut at a remote end to secure said roller pin within said crank collars, wherein said nut is welded to said remote end of said bolt. 
     
     
         10 . A gas turbine engine anti-ice system comprising:
 a source of hot air to provide deicing;   a destination to receive the hot air for deicing a location on an aircraft associated with a gas turbine engine; and   a butterfly valve controlling flow from said source to said destination, the butterfly valve including:
 a valve member mounted on a shaft to pivot within a fluid passage; 
 an actuator including a piston having opposed piston heads associated with fluid chambers, and a control to move the piston in a linear direction to control a position of said valve member in said fluid passage, said piston causing a roller pin to move as said piston moves linearly, said roller pin mounted in crank collars of a crank shaft such that movement of said roller pin causes said crank shaft to rotate said valve shaft; and 
 said roller pin being mounted within said crank collars by bearings, said bearings each having an outer race associated with one of said crank collars, an inner race associated with said roller pin, and bearing members separating said inner and outer races, there being a spring bias resisting movement of said inner races relative to said roller pin. 
   
     
     
         11 . The gas turbine engine anti-ice system as set forth in  claim 10 , wherein said roller pin having cavities associated with each of two axial ends, and receiving a spring member to apply said spring bias to each said inner race. 
     
     
         12 . The gas turbine engine anti-ice system as set forth in  claim 11 , wherein said spring members are wave springs. 
     
     
         13 . The gas turbine engine anti-ice system as set forth in  claim 12 , wherein a shim positioned between said wave spring and said inner race. 
     
     
         14 . The gas turbine engine anti-ice system as set forth in  claim 11 , wherein a shim is positioned between said spring member and said inner race. 
     
     
         15 . The gas turbine engine anti-ice system as set forth in  claim 14 , wherein said roller pin moves within a slot in a connecting portion of said piston connecting said opposed piston heads of said piston. 
     
     
         16 . The gas turbine engine anti-ice system as set forth in  claim 15 , wherein said roller pin has an internal bore and a bearing retention bolt extends through said inner bore and receives a nut at a remote end to secure said roller pin within said crank collars. 
     
     
         17 . The gas turbine engine anti-ice system as set forth in  claim 16 , wherein said nut is welded to said remote end of said bolt. 
     
     
         18 . The gas turbine engine anti-ice system as set forth in  claim 10 , wherein said roller pin moves within a slot in a connecting portion of said piston connecting said opposed piston heads of said piston, wherein said roller pin has an internal bore and a bearing retention bolt extends through said inner bore and receives a nut at a remote end to secure said roller pin within said crank collars. 
     
     
         19 . The gas turbine engine anti-ice system as set forth in  claim 18 , wherein said nut is welded to said remote end of said bolt. 
     
     
         20 . The gas turbine engine anti-ice system as set forth in  claim 10 , wherein said butterfly valve is mounted on a gas turbine engine.