Butterfly valve with vibration resistant mount

Patent metadata

Field	Value
Publication number	US-11313473-B2
Application number	US-202017012666-A
Country	US
Kind code	B2
Filing date	Sep 4, 2020
Priority date	Sep 4, 2020
Publication date	Apr 26, 2022
Grant date	Apr 26, 2022

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.

First claim

The invention claimed is:

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;
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, said spring bias being provided by a pair of springs, with one of said springs being associated with each of said inner races, and said spring bias being in an outward direction such that said each of said springs biases its inner race in an opposed direction relative to the other; and
wherein said roller pin having channels associated with each of two axial ends, there being two of said channels, and both of said channels being positioned between said bearings and receiving one of said spring members to apply said spring bias to each said inner race.

2. The butterfly valve as set forth in claim 1 , wherein said spring members are wave springs.

3. The butterfly valve as set forth in claim 2 , wherein a shim is positioned between each said wave spring and said inner race.

4. The butterfly valve as set forth in claim 1 , wherein a shim is positioned between said spring member and each said inner race.

5. The butterfly valve as set forth in claim 4 , wherein said roller pin moves within a slot in a connecting portion of said piston connecting said opposed piston heads.

6. The butterfly valve as set forth in claim 5 , 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.

7. The butterfly valve as set forth in claim 6 , wherein said nut is welded to said remote end of said bolt.

8. 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.

9. 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;
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, said spring bias being provided by a pair of springs, with one of said springs being associated with each of said inner races, and said spring bias being in an outward direction such that said each of said springs biases its inner race in an opposed direction relative to the other; and
wherein said roller pin having cavities associated with each of two axial ends, there being two of said channels, and both of said channels being positioned between said bearings and receiving one of said spring members to apply said spring bias to each said inner race.

10. The gas turbine engine anti-ice system as set forth in claim 9 , wherein said spring members are wave springs.

11. The gas turbine engine anti-ice system as set forth in claim 10 , wherein a shim is positioned between said wave spring and said inner race.

12. The gas turbine engine anti-ice system as set forth in claim 9 , wherein a shim is positioned between said spring member and said inner race.

13. The gas turbine engine anti-ice system as set forth in claim 12 , wherein said roller pin moves within a slot in a connecting portion of said piston connecting said opposed piston heads of said piston.

14. The gas turbine engine anti-ice system as set forth in claim 13 , 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.

15. The gas turbine engine anti-ice system as set forth in claim 14 , wherein said nut is welded to said remote end of said bolt.

16. The gas turbine engine anti-ice system as set forth in claim 9 , 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.

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 9 , wherein said butterfly valve is mounted on a gas turbine engine.

Assignees

• Hamilton Sundstrand Corp

Inventors

• Simpson Scott W
• Parent Calvin R
• Zawilinski David J

Classifications

• F16C11/045

  with at least a pair of arms pivoting relatively to at least one other arm, all arms being mounted on one pin (crank-pins F16C11/02) · CPC title

• F16K31/1635 Primary

  for rotating valves · CPC title

• F16K31/5282

  comprising a pivoted disc or flap · CPC title

• F16K1/221

  specially adapted operating means therefor (operating means per se F16K31/00) · CPC title

• F16K47/00

  Means in valves for absorbing fluid energy (for pipes F16L55/00) · CPC title