Cryogenic cam butterfly valve

Patent metadata

Field	Value
Publication number	US-9506571-B1
Application number	US-201414463238-A
Country	US
Kind code	B1
Filing date	Aug 19, 2014
Priority date	Aug 19, 2013
Publication date	Nov 29, 2016
Grant date	Nov 29, 2016

Abstract

A cryogenic cam butterfly valve has a body that includes an axially extending fluid conduit formed there through. A disc lug is connected to a back side of a valve disc and has a circular bore that receives and is larger than a cam of a cam shaft. The valve disc is rotatable for a quarter turn within the body about a lug axis that is offset from the shaft axis. Actuating the cam shaft in the closing rotational direction first causes the camming side of the cam of the cam shaft to rotate the disc lug and the valve disc a quarter turn from the open position to the closed position. Further actuating causes the camming side of the cam shaft to translate the valve disc into sealed contact with the valve seat. Opening rotational direction of the cam shaft reverses these motions.

First claim

I claim:

1. A cam butterfly valve, comprising:
a body including an axially extending fluid conduit formed there through;
a valve seat projecting from the body annularly within the fluid conduit;
a cam shaft having a cam of circular cross section, disposed transverse to an axis of the fluid conduit, and mounted within the body to rotate about a shaft axis;
a valve disc having a seating surface that corresponds in a closed position to the valve seat of the body;
a disc lug connected to a back side of the valve disc and having a circular bore that receives and is larger than the cam of the cam shaft, the valve disc rotatable for a quarter turn within the body about a lug axis that is offset from the shaft axis; and
at least one torsion spring mounted concentrically on the cam shaft with one spring leg against the valve disc having a preload of sufficient torque to cause the valve disc to rigidly move with the cam shaft;
wherein actuating the cam shaft in the closing rotational direction first causes the camming side of the cam of the cam shaft to rotate the disc lug and the valve disc a quarter turn from the open position to the closed position and further actuating causes the camming side of the cam shaft to translate the valve disc into sealed contact with the valve seat, said valve disc being translated by the force of the valve disc against the valve seat; and
Wherein actuating the cam shaft in an opening rotational direction first causes the camming side of the cam of the cam shaft to reverse translate the valve disc to unseal from the valve seat and continued actuating causes the caroming side of the cam shaft to reverse rotate the disc lug and valve disc a quarter turn from the closed position to the open position.

2. The cam butterfly valve of claim 1 , wherein the at least one torsion spring comprises an austenitic nickel-chromium-based superalloy.

3. The cam butterfly valve of claim 1 , wherein the cam shaft has a second cam of circular cross section that moves in unison with the first cam, the cam butterfly valve further comprising a second disc lug connected to a back side of the valve disc and having a circular bore that receives and is larger than the second cam of the cam shaft, the valve disc rotatable for a quarter turn within the body about the lug axis that is offset from the shaft axis.

4. The cam butterfly valve of claim 1 , wherein the valve disc comprises a triple offset design with the cam shaft offset from a plane made from the seating surface, wherein the shaft axis is offset from a body centerline of the body, and wherein the seating surface on disc has a slanted cone shape.

5. The cam butterfly valve of claim 1 , wherein the valve seat comprises a static valve seat.

6. The cam butterfly valve of claim 5 , wherein the static valve seat comprises a conical ring attached to the valve body.

7. The cam butterfly valve of claim 1 , wherein the fluid conduit contains a cryogenic fluid, wherein further actuating of the cam shaft causes the camming side of the cam shaft to translate the valve disc a first amount into sealed contact with the valve seat at an ambient temperature and to translate the valve disc a second amount into sealed contact with the valve seat at a cryogenic temperature.

8. The cam butterfly valve of claim 1 , wherein the body, the valve disc and the cam shaft comprise stainless steel.

9. The cam butterfly valve of claim 1 , wherein actuating the cam shaft comprises a rotation of 0-90° and further actuating the cam shaft comprises an additional rotation of 90° to approximately 135° to thereby translate the valve disc towards the valve seat thereby creating a tight seal.

10. The cam butterfly valve of claim 1 , further comprising:
an actuator operably connected to the cam shaft to cause rotation; and
a reduction gearbox operatively coupled to the actuator gear reduce a rotational actuation and to assert a closing bias during cryogenic cool down.

11. The cam butterfly valve of claim 1 , further comprising:
an actuator operably connected to the cam shaft to cause rotation; and
a closing torsional biasing mechanism coupled to the actuator to assert a closing bias during cryogenic cool down.

12. A cryogenic cam butterfly valve, comprising:
a body including an axially extending fluid conduit formed there through;
a valve seat projecting from the body annularly within the fluid conduit;
a cam shaft having a cam of circular cross section, disposed transverse to an axis of the fluid conduit, and mounted within the body to rotate about a shaft axis;
a valve disc having a seating surface that corresponds in a closed position to the valve seat of the body;
a disc lug connected to a back side of the valve disc and having a circular bore that receives and is larger than the cam of the cam shaft, the valve disc rotatable for a quarter turn within the body about a lug axis that is offset from the shaft axis; and
at least one torsion spring mounted concentrically on the cam shaft with one spring leg against the valve disc having a preload of sufficient torque to cause the valve disc to rigidly move with the cam shaft;
a biasing mechanism operatively coupled to the cam shaft, wherein actuating the cam shaft in the closing rotational direction first causes the camming side of the cam of the cam shaft to rotate the disc lug and the valve disc a quarter turn from the open position to the closed position and further actuating causes the camming side of the cam shaft to translate the valve disc into sealed contact at an ambient temperature with the valve seat, said valve disc being translated by the force of the valve disc against the valve seat,
wherein the biasing mechanism asserts a closing bias rotation to the cam shaft to cause additional translation to maintain the sealed contact during cool down to a cryogenic temperature, and
wherein actuating the cam shall in an opening rotational direction first causes the camming side of the cam of the cam shaft to reverse translate the valve disc to unseal from the valve seat and continued actuating causes the camming side of the cam shaft to reverse rotate the disc lug and valve disc a quarter turn from the closed position to the open position.

13. The cryogenic cam butterfly valve of claim 12 , wherein the at least one torsion spring comprises an austenitic nickel-chromium-based superalloy.

14. The cryogenic cam butterfly valve of claim 12 , wherein the cam shaft has a second cam of circular cross section that moves in unison with the first cam, the cam butterfly valve further comprising a second disc lug connected to a back side of the valve disc and having a circular bore that receives and is larger than the second cam of the cam shaft, the valve disc rotatable for a quarter turn within the body about the lug axis that is offset from the shaft axis.

15. The cryogenic cam butterfly valve of claim 12 , wherein the valve disc comprises a triple offset design with the cam shaft offset from a plane made from the seating surface, wherein the shaft axis is offset from a body centerline of the body, and wherein the seating surface on disc has a slanted cone shape.

16. The cryogenic cam butterfly valve of claim 12 , wherein the valve seat comprises a static valve seat.

17. The cryogenic cam butterfly valve of claim 16 , wherein the static valve seat comprises a conical ring attached to the valve body.

18. The cryogenic cam butterfly valve of claim 12 , wherein the fluid conduit contains a cryogenic fluid, the wherein further actuating of causes the camming side of the cam shaft to transl

Assignees

• The Us Adminstrator Of The Nat Aeronautics And Space Administration
• Nasa

Inventors

• Mccormack Kenneth J

Classifications

• F16K31/524

  with a cam · CPC title

• F16K1/221 Primary

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

• F17C13/04

  Arrangement or mounting of valves (valves per se F16K {; snap-coupling of nipples F16L37/00}) · CPC title

• F16K1/24

  with valve members that, on opening of the valve, are initially lifted from the seat and next are turned around an axis parallel to the seat · CPC title

• F16K31/52441

  with a pivoted disc or flap · CPC title