Replacement venous valve

• US 20040193253A1
• Filed: 05/17/2004
• Published: 09/30/2004
• Est. Priority Date: 04/30/2001
• Status: Abandoned Application

• Current Assignee: Francisco J. Osse, Patricia E. Thorpe
• Original Assignee: Francisco J. Osse, Patricia E. Thorpe
• Inventors: Osse, Francisco J, Thorpe, Patricia E
• Application Number:
  US10/476,363
• Publication Number:
  US 20040193253A1
• Time in Patent Office: Days
• US Class Current: 623/1.24
• CPC Class Codes: A61F 2/2418 Scaffolds therefor, e.g. support stents
• CPC Class Codes: A61F 2/2475 Venous valves

Abstract

A replacement venous valve comprises a pair of support wings and a pair of valve wings. The valve wings are designed to deploy first from a catheter deployment device and provide stability while the support wings then deploy. The valve wings support the venous valve material and the support wings maintain patency of the vein above the valve while simultaneously anchoring the location and orientation of the valve.

Claims

1. A valve assembly, comprising:

a first valve wing coupled to a first support wing;

a second valve wing coupled to a second support wing;

a first flexible sheet fastened to the first valve wing; and

a second flexible sheet fastened to the second valve wing.

2. The valve assembly of claim 1, wherein:

the first flexible sheet and the second flexible sheet have a first position in which a trailing portion of the first flexible sheet contacts a trailing portion of the second flexible sheet for preventing blood flow therepast; and

the first flexible sheet and the second flexible sheet have a second position in which the trailing portion of the first flexible sheet and trailing portion of the second flexible sheet define an aperture for allowing blood flow through the valve.

3. The valve assembly of claim 2, wherein the first flexible sheet and the second flexible sheet are biased to assume the first position.

4. The valve assembly of claim 1, wherein the first valve wing, the second valve wing, the first support wing, and the second support wing are biased to assume an expanded shape.

5. The valve assembly of claim 1, wherein the first valve wing, the second valve wing, the first support wing, and the second support wing define a generally cylindrical surface when they assume the expanded shape.

6. The valve assembly of claim 1, wherein the first valve wing, the second valve wing, the first support wing, and the second support wing each comprise a length of wire having a U-shaped bend.

7. The valve assembly of claim 1, wherein the first valve wing, the second valve wing, the first support wing, and the second support wing are all formed from a single wire.

8. The valve assembly of claim 1, wherein a first end of the first valve wing is coupled to a first end of the first support wing by a first loop.

9. The valve assembly of claim 1, wherein a second end of the first valve wing is coupled to a second end of the second valve wing by a second loop.

10. The valve assembly of claim 1, wherein a first end of the second valve wing is coupled to a first end of the second support wing by a third loop.

11. The valve assembly of claim 1, wherein a second end of the second support wing is coupled to a second end of the first support wing by a fourth loop.

12. The valve assembly of claim 1, wherein:

a first end of the first valve wing is coupled to a first end of the first support wing by a first loop;

a second end of the first valve wing is coupled to a second end of the second valve wing by a second loop;

a first end of the second valve wing is coupled to a first end of the second support wing by a third loop;

the second support wing is coupled to a second end of the first support wing by a fourth loop;

the first loop and the third loop are interlinked; and

the second loop and the fourth loop are interlinked.

13. The valve assembly of claim 1, wherein;

a first end of the first valve wing is coupled to a first end of the first support wing by a first bend;

a second end of the first valve wing is coupled to a second end of the first support wing by a second bend;

a first end of the second valve wing is coupled to a first end of the second support wing by a third bend;

a second end of the second valve wing is coupled to a second end of the second support wing by a fourth bend; and

the first valve wing is coupled to the second valve wing by at least one coupling member.

14. The valve assembly of claim 1, wherein the first valve wing, the second valve wing, the first support wing, and the second support wing are biased to assume an expanded shape.

15. The valve assembly of claim 14, wherein the first valve wing, the second valve wing, the first support wing, and the second support wing define a generally cylindrical surface when they assume the expanded shape.

16. The valve assembly of claim 14, wherein the first valve wing and the second support wing define an first angle when the valve assembly assumes the expanded shape.

17. The valve assembly of claim 16 wherein the first angle is about a 60 degree angle.

18. The valve assembly of claim 14, wherein the second valve wing and the first support wing define a second angle when the valve assembly assumes the expanded shape.

19. The valve assembly of claim 16, wherein the second angle is about a 60 degree angle.

20. The valve assembly of claim 1, wherein the first valve wing and the second valve wing define an third angle when the valve assembly assumes the expanded shape.

21. The valve assembly of claim 18, wherein the third angle is about a 60 degree angle.

22. The valve assembly of claim 1, wherein:

the valve assembly has a length A and a radius B;

the first flexible sheet is coupled to the first valve wing at a plurality of fixing points and the location of each fixing point may be defined by a polar coordinate values including a value Z corresponding to a z-axis, value R corresponding to an r-axis, and a value theta corresponding to an angle theta;

a first fixing point of the first flexible sheet being located generally at theta=0, Z=0, and R=B;

a second fixing point of the first flexible sheet being located generally at theta=180, Z=0, and R=B; and

a third fixing point of the first flexible sheet being located generally at theta=90 degrees, Z=A, and R=B.

23. The valve assembly of claim 1, wherein:

the valve assembly has a length A and a radius B;

the second flexible sheet is coupled to the first valve wing at a plurality of fixing points and the location of each fixing point may be defined by a polar coordinate values including a value Z corresponding to a z-axis, value R corresponding to an r-axis, and a value theta corresponding to an angle theta;

a first fixing point of the second flexible sheet being located generally at theta=0, Z=0, and R=B;

a second fixing point of the second flexible sheet being located generally at theta=180, Z=0, and R=B; and

a third fixing point of the second flexible sheet being located generally at theta=270 degrees, Z=A, and R=B.

24. The valve assembly of claim 1, wherein the first flexible sheet is coupled to the first valve wing by a plurality of sutures.

25. The valve assembly of claim 1, wherein the first flexible sheet is coupled to the first valve wing by a staple.

26. The valve assembly of claim 1, wherein the first flexible sheet is coupled to the first valve wing by a hook.

27. The valve assembly of claim 1, wherein at least a portion of one of the flexible sheets includes either sclera or small intestine sub-mucosa material.

28. The valve assembly of claim 1, wherein the first valve wing, the second valve wing, the first support wing, and the second support wing comprise a resilient metallic material.

29. The valve assembly of claim 28, in which the resilient metallic material is selected from either nitinol or stainless steel.

30. The valve assembly of claim 1, wherein at least a portion of one of the flexible sheets includes mammalian tissue.

31. The valve assembly of claim 1, wherein the first valve wing and the first support wing are formed from a first wire, the second valve wing and the second support wing are formed from a second wire and the two parts are joined by a plurality of connectors.

32. The valve assembly of claim 1 where the expanded shape has a circumference larger than the circumference of the selected vascular lumen thereby inhibiting the assembly'"'"'s movement from its desired position.

33. A method of using the valve assembly comprising the following steps:

a. inserting a delivery system containing the valve assembly into the vascular system;

b. deploying at least one replacement valve assembly at a selected site within a vein with a first valve wing pair and then a second support wing pair.