IP Library Granted Patent US 7,984,892
Granted Patent B2
US 7,984,892 · App. 11/276,265 · Granted Jul 26, 2011

Low friction butterfly ring

Assignee: GE Aviation Systems, LLC
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Quick Facts
Patent No.
US 7,984,892
App. No.
11/276,265
Granted
Jul 26, 2011
Kind
B2
Abstract

A butterfly valve for controlling the flow of fluid within a bore, including a butterfly and at least one ring extending at least one of substantially and completely around a perimeter of the butterfly and adapted to develop an expansion force in the radial direction when the at least one ring is in a contracted state with respect to the radial direction, wherein the at least one ring is secured to the butterfly in the contracted state and radial expansion due to the developed expansion force of the at least one ring is effectively restrained, wherein the butterfly valve is adapted to operate, when placed in a bore, without friction or substantially without friction between the at least one ring and the bore when the butterfly valve is placed in a closed position within the bore.

Claims (27)

1. A butterfly valve for controlling the flow of fluid within a bore, comprising:

a butterfly; and

at least one ring extending at least one of substantially and completely around a perimeter of the butterfly and adapted to develop an expansion force in the radial direction when the at least one ring is in a contracted state with respect to the radial direction,

wherein the at least one ring is secured to the butterfly in the contracted state and radial expansion due to the developed expansion force of the at least one ring is effectively restrained by the butterfly, wherein the butterfly valve is adapted to operate, when placed in a bore, without friction or substantially without friction between the at least one ring and the bore when the butterfly valve is placed in a closed position within the bore.

2. A butterfly valve according to claim 1 , further comprising a ring retainer, wherein the ring retainer is adapted to secure the at least one ring to the butterfly so that radial expansion of the at least one ring is restrained.

3. A butterfly valve according to claim 2 , wherein the ring retainer is adapted to clamp the at least one ring between the ring retainer and the butterfly so that radial expansion of the at least one ring is restrained.

4. A butterfly valve according to claim 2 , wherein the ring retainer is attached to the butterfly by an attachment device.

5. A butterfly valve according to claim 1 , wherein the radial expansion of the at least one ring is restrained so that radial expansion of the at least one ring is effectively prevented when the butterfly valve is moved from the closed position to an open position.

6. A butterfly valve assembly for controlling the flow of fluid within a bore, comprising:

a housing with a bore; and

the butterfly valve according to claim 1 .

7. A butterfly valve assembly according to claim 6 , further comprising a ring retainer, wherein the ring retainer is adapted to secure the at least one ring to the butterfly so that radial expansion of the at least one ring is restrained.

8. A butterfly valve assembly according to claim 7 , wherein the ring retainer is adapted to clamp the at least one ring between the ring retainer and the butterfly.

9. A butterfly valve assembly according to claim 7 , wherein the ring retainer is attached to the butterfly by an attachment device.

10. A butterfly valve assembly according to claim 6 , wherein the radial expansion of the at least one ring is restrained so that radial expansion of the at least one ring is prevented or substantially prevented when the butterfly valve is in an open position.

11. The butterfly valve according to claim 6 , wherein the butterfly valve is adapted to operate, when placed in a bore, in at least one of the following manners over an expected lifetime of the butterfly valve:

(i) the at least one ring experiences an interference fit with the housing bore at closing of the butterfly valve during a limited number of initial actuation cycles as compared to the expected lifetime of the butterfly valve, and experiences a slip fit with the housing bore thereafter; and

(ii) the at least one ring experiences a slip fit with the housing bore over the expected lifetime of the butterfly valve.

12. The butterfly valve according to claim 1 , wherein the butterfly valve is adapted to operate, when placed in a bore, in at least one of the following manners over an expected lifetime of the butterfly valve:

(i) the at least one ring experiences an interference fit with the housing bore at closing of the butterfly valve during a limited number of initial actuation cycles as compared to the expected lifetime of the butterfly valve, and experiences a slip fit with the housing bore thereafter; and

(ii) the at least one ring experiences a slip fit with the housing bore over the expected lifetime of the butterfly valve.

13. A butterfly valve for controlling the flow of fluid within a bore, comprising a butterfly; and

at least one ring extending at least one of substantially and completely around a perimeter of the butterfly and adapted to develop an expansion force in the radial direction when the at least one ring is in a contracted state with respect to the radial direction,

wherein the at least one ring is secured to the butterfly in the contracted state and radial expansion due to the developed expansion force of the at least one ring is effectively restrained by the butterfly, wherein the butterfly valve is adapted to operate, when placed in a bore, in such a manner that, during opening of the valve, an outer diameter of the at least one ring expands only by an amount that is equal to or less than the amount of compression caused by the bore when the butterfly valve is placed in a closed position within the bore.

14. A butterfly valve assembly for controlling the flow of fluid within a bore, comprising:

a housing with a bore; and

the butterfly valve according to claim 13 .

Assignments (2)
CHANGE OF NAME Recorded Jan 25, 2011
From: SMITHS AEROSPACE LLC
To: GE AVIATION SYSTEMS LLC
Reel/Frame 025689/0540 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 9, 2006
From: SHENK, DAVID R.
To: SMITHS AEROSPACE LLC.
Reel/Frame 017600/0885 →
Continuity (1)
Related Publication 20070194265A1 · Aug 23, 2007