Inflatable members having concentrated force regions

• US 20030144683A1
• Filed: 12/11/2002
• Published: 07/31/2003
• Est. Priority Date: 12/13/2001
• Status: Abandoned Application

• Current Assignee: Avantec Vascular Corporation
• Original Assignee: Avantec Vascular Corporation
• Inventors: Dutta, Debashis, Sirhan, Motasim
• Application Number:
  US10/317,846
• Publication Number:
  US 20030144683A1
• Time in Patent Office: Days
• US Class Current: 606/194
• CPC Class Codes: A61B 17/320725 with radially expandable cutting or abrading elements A61B17/32075 takes precedence
• CPC Class Codes: A61B 2017/00526 Methods of manufacturing
• CPC Class Codes: A61B 2017/22051 with an inflatable part, e.g. balloon, for positioning, blocking, or immobilisation A61B2017/22048, A61B2017/3486 take precedence
• CPC Class Codes: A61F 2/958 Inflatable balloons for placing stents or stent-grafts
• CPC Class Codes: A61F 2002/30322 differing in surface structures
• CPC Class Codes: A61F 2250/0026 differing in surface structures
• CPC Class Codes: A61M 2025/1086 having a special balloon surface topography, e.g. pores, protuberances, spikes or grooves

Abstract

A device and a method using the same, for the treatment of stenosed areas during or prior to dilation, comprising at least one region along an expandable member which is configured to deliver a concentrated force to the diseased tissue site.

Claims

1. A device for dilating or recanalizing a vessel, comprising:

a balloon catheter comprising an expandable member having an outer surface and an inner chamber defined by an inner surface; and

at least one region along the expandable member integrally formed within the balloon and configured to deliver concentrated force to an interior of the vessel upon expansion of the expandable member in the vessel

2. A device as in claim 1 wherein the expandable member is a balloon.

3. A device as in claim 2 wherein the region extends along a longitudinal axis of the balloon.

4. A device as in claim 2 wherein the region extends along a radial axis of the balloon.

5. A device as in claim 2 wherein the region extends along a longitudinal axis and a radial axis of the balloon.

6. A device as in claim 1 wherein the region extends along a working length of the balloon disposed longitudinally between a balloon proximal end and a balloon distal end.

7. A device as in claim 1 wherein the region has a continuous dimension.

8. A device as in claim 1 wherein the region has an intermittent dimension.

9. A device as in claim 2 wherein the balloon includes at least one wing.

10. A device as in claim 9, wherein the wing is molded from the same material as the balloon.

11. A device as in claim 9 wherein the balloon includes a plurality of wings.

12. A device as in claim 9 wherein the at least one wing has a contour extending more radially outward upon the expansion of the balloon relative to the balloon.

13. A device as in claim 9 wherein the at least one wing includes portions having a relatively higher stiffness than the rest of the balloon.

14. A device as in claim 9 wherein the wing has a pocket.

15. A device as in claim 14 wherein the pocket is sealed from the interior chamber of the balloon.

16. A device as in claim 14 wherein the wing pocket includes a concentrating element disposed therein.

17. A device as in claim 16 wherein the concentrating element is a blade.

18. A device as in claim 16 wherein the concentrating element device is a wire.

19. A device as in claim 16 wherein the concentrating element is a tube.

20. A device as in claim 16 wherein the concentrating element has a continuous dimension.

21. A device as in claim 16 wherein the concentrating element has an intermittent dimension.

22. A device as in claim 17 wherein the concentrating element has a continuous dimension.

23. A device as in claim 17 wherein the concentrating element has an intermittent dimension.

24. A device as in claim 1 wherein the region includes a concentrating element.

25. A device as in claim 24 wherein the concentrating element is disposed within the interior chamber of the expandable member.

26. A device as in claim 25 wherein the concentrating element is fixedly attached to the inner surface of the expandable member.

27. A device as in claim 25 wherein the concentrating element is removably disposed within the inner chamber.

28. A device as in claim 25 wherein the concentrating element is removably attached to the inner surface.

29. A device as in claim 24 wherein a concentrating element is disposed within the wing.

30. A device as in claim 24 wherein the concentrating element is fixedly attached to an inner surface of the wing.

31. A device as in claim 24 wherein the concentrating element is removably disposed between an opposing inner surfaces of the wing.

32. A device as in claim 24 wherein the concentrating element is removably attached to an inner surface of the wing.

33. A device as in claim 24 wherein the concentrating element is configured to expand with the expandable member.

34. A device as in claim 25, wherein the region exterior surface is formed from the same material as the expandable member.

35. A device as in claim 24 wherein the concentrating element at least partially protrudes from the balloon material.