Pressure lamination method for forming composite ePTFE/textile and ePTFE/stent/textile prostheses

• US 7,560,006 B2
• Filed: 12/19/2003
• Issued: 07/14/2009
• Est. Priority Date: 06/11/2001
• Status: Expired due to Fees

• Current Assignee: Lifeshield Sciences LLC (Acacia Research Corporation)
• Original Assignee: Boston Scientific Scimed (Boston Scientific Corporation)
• Inventors: Sowinski, Krzysztof, Rakos, Ronald
• Primary Examiner(s): Fischer; Justin
• Application Number:
  US10/741,209
• Publication Number:
  US 20040182511A1
• Time in Patent Office: 2,034 Days
• Field of Search: 156/285, 156/293, 156/294, 156/295
• US Class Current: 156/293
• CPC Class Codes: A61F 2/06 Blood vessels
• CPC Class Codes: A61F 2/07 Stent-grafts
• CPC Class Codes: A61F 2/89 the wire-like elements comprising two or more adjacent rings flexibly connected by separate members
• CPC Class Codes: A61F 2002/072 Encapsulated stents, e.g. wire or whole stent embedded in lining
• CPC Class Codes: A61L 27/16 obtained by reactions only involving carbon-to-carbon unsaturated bonds
• CPC Class Codes: A61L 27/48 with macromolecular fillers
• CPC Class Codes: A61L 27/507 for artificial blood vessels apparatus for applying cells on a blood vessel prosthesis A61F2/062
• CPC Class Codes: A61L 31/048 obtained by reactions only involving carbon-to-carbon unsaturated bonds A61L31/041 takes precedence
• CPC Class Codes: A61L 31/129 containing macromolecular fillers
• CPC Class Codes: C08L 27/18 Homopolymers or copolymers or tetrafluoroethene

Abstract

A method of forming a composite textile and ePTFE implantable device includes the steps of (a) providing an ePTFE layer having opposed surfaces comprising a microporous structure of nodes interconnected by fibrils; (b) providing a textile layer having opposed surfaces; (c) applying a coating of an elastomeric bonding agent to one of the opposed surfaces of the ePTFE layer or the textile layer; (d) providing a hollow member having an open end and an opposed closed end defining a fluid passageway therebetween and having a wall portion with at least one hole extending therethrough, the hole being in fluid communication with the fluid passageway; (e) concentrically placing the ePTFE layer and the textile layer onto the hollow member and over the at least one hole of the hollow member to provide an interior composite layer and an exterior composite layer, thereby defining a composite assembly, wherein the interior composite layer is one of the ePTFE layer or the textile layer and the exterior composite layer is the other of the ePTFE layer or the textile layer; (f) placing the hollow member with the composite assembly within a pressure chamber; (g) applying a pressure differential so that the pressure within the chamber is greater than a pressure within the fluid passageway of the hollow member; and (h) applying heat to the bonding agent to adhesively bond the textile layer and the ePTFE layer to provide a laminated composite assembly.

Claims

1. A method of forming a composite textile and ePTFE implantable device comprising the steps of:

(a) providing an ePTFE layer having opposed surfaces comprising a microporous structure of nodes interconnected by fibrils;

(b) providing a textile layer having opposed surfaces;

(c) applying a coating of an elastomeric bonding agent to one of said opposed surfaces of said ePTFE layer or said textile layer;

(d) providing a hollow member having an open end and an opposed closed end defining a fluid passageway therebetween and having a wall portion with at least one hole extending therethrough, the hole being in fluid communication with said fluid passageway;

(e) concentrically placing said ePTFE layer and said textile layer onto said hollow member and over said at least one hole of said hollow member to provide an interior composite layer and an exterior composite layer, thereby defining a composite assembly, wherein said interior composite layer is one of said ePTFE layer or said textile layer and said exterior composite layer is the other of said ePTFE layer or said textile layer;

(f) expanding an elastic silicone barrier member;

(g) disposing the expanded elastic silicone barrier member over an exterior surface of said exterior composite layer;

(h) placing said hollow member with said composite assembly within a pressure chamber;

(i) applying a positive pressure to said chamber so that the positive pressure within said chamber is higher than a pressure outside of said chamber;

(j) applying a pressure differential so that the pressure within said chamber is greater than a pressure within said fluid passageway of said hollow member;

(k) applying heat to said bonding agent to adhesively bond said textile layer and said ePTFE layer to provide a laminated composite assembly; and

(l) removing said elastic silicone barrier member from said laminated composite assembly, to provide a composite textile and ePTFE implantable device having an improved bond peel strength of at least 32 g/mm and a variation of said bond peel strength of less than about 4.

2. The method of claim 1, wherein said applying step includes:

applying a solution of said bonding agent.

3. The method of claim 2, wherein said applying step further includes:

spray coating said surface of said ePTFE layer with said solution.

4. The method of claim 1, wherein said textile layer is a hollow tubular textile layer having an inner and outer textile surface and said ePTFE layer is applied to said inner textile surface.

5. The method of claim 4,wherein said ePTFE layer is a hollow tubular structure.

6. The method of claim 4,wherein said implantable device is a vascular prosthesis.

7. The method of claim 4, further including the steps of:

providing a distensible stent; and

placing said distensible stent between said textile layer and said ePTFE layer prior to the step of placing said hollow member within said pressure chamber.

8. The method of claim 7, further including the step of providing a second layer of ePTFE between said stent and said textile layer prior to the step of placing said hollow member within said pressure chamber.

9. The method of claim 4, further including the steps of:

providing a distensible stent; and

placing said distensible stent onto said hollow member prior to the step of placing said ePTFE layer and said textile layer onto said hollow member.

10. The method of claim 1, wherein said textile layer is a hollow tubular textile layer having an inner and outer textile surface and said ePTFE layer is applied to said outer textile surface.

11. The method of claim 10, wherein said implantable device is a vascular prosthesis.

12. The method of claim 1, wherein said elastic silicone barrier is adjacently disposed over said exterior surface of said exterior composite layer.

13. The method of claim 1, wherein said elastic silicone barrier is adjacently disposed over said exterior surface of said exterior composite layer without applying a flowable mass particulate therebetween.

14. The method of claim 1, where said applied pressure differential is from about 1 psia to about 50 psia.

15. The method of claim 1, wherein the step of applying heat to said bonding agent includes heating said bonding agent from about 325°

F. to about 450°

F.

16. The method of claim 1, wherein the step of applying said coating of said elastomeric bonding agent includes applying said coating to one of said opposed surfaces of said ePTFE layer with said bonding agent being disposed within said microporous structure.

17. The method of claim 1, wherein said bonding agent is selected from the group consisting of urethanes, styrene/isobutylene/styrene block copolymers, silicones, and combinations thereof.

18. The method of claim 1, wherein said bonding agent is a polycarbonate urethane.

19. The method of claim 1, wherein said textile layer is knitted textile layer, a woven textile layer, a stretch-knit textile layer, a braided textile layer, and combinations thereof.

20. The method of claim 1,wherein said textile layer and said ePTFE layer are substantially planar.

21. The method of claim 20, wherein said composite device is a vascular patch.

22. The method of claim 1, wherein said elastic silicone barrier member has a thickness of about 0.5 mm to about 1.25 mm.

23. The method of claim 1, wherein said composite textile and ePTFE implantable device has a bond shear strength of at least 5.5 g/mm² and a variation of said bond shear strength of less than about 2.

24. A method of forming a composite textile and ePTFE implantable device comprising the steps of:

(a) providing an ePTFE layer having opposed surfaces comprising a microporous structure of nodes interconnected by fibrils;

(b) providing a textile layer having opposed surfaces;

(c) providing a self-expanding, radially distensible and metallic stent;

(c) applying a coating of an elastomeric bonding agent to one of said opposed surfaces of said ePTFE layer or said textile layer;

(e) providing a hollow member having an open end and an opposed closed end defining a fluid passageway therebetween and having a wall portion with at least one hole extending therethrough, the hole being in fluid communication with said fluid passageway;

(f) concentrically placing said ePTFE layer, said textile layer and said distensible stent onto said hollow member and over said at least one hole of said hollow member to provide an interior composite layer and an exterior composite layer, wherein said distensible stent is placed between said textile layer and said ePTFE layer, thereby defining a composite assembly, wherein said interior composite layer is one of said ePTFE layer or said textile layer and said exterior composite layer is the other of said ePTFE layer or said textile layer;

(g) placing said hollow member with said composite assembly within a pressure chamber;

(h) applying a positive pressure to said chamber so that the positive pressure within said chamber is higher than a pressure outside of said chamber;

(i) applying a pressure differential so that the pressure within said chamber is greater than a pressure within said fluid passageway of said hollow member; and

(j) applying heat to said bonding agent to adhesively bond said textile layer and said ePTFE layer to provide a laminated composite assembly having a bond shear strength of at least 5.5 g/mm2 and a variation of said bond shear strength of less than about 2.

25. The method of claim 24, wherein said textile layer is a hollow tubular textile layer having an inner and outer textile surface and said ePTFE layer is applied to said inner textile surface.

26. The method of claim 24, further including the step of providing a second layer of ePTFE between said stent and said textile layer prior to the step of placing said hollow member within said pressure chamber.

30. The method of claim 24, wherein said laminated composite assembly has a bond peel strength of at of at least 32 g/mm and a variation of said bond peel strength of less than about 4.

27. A method of forming a composite textile and ePTFE implantable device comprising the steps of:

providing an ePTFE layer having opposed surfaces comprising a microporous structure of nodes interconnected by fibrils;

providing a textile layer having opposed surfaces;

applying a coating of an elastomeric bonding agent to one of said opposed surfaces of said ePTFE layer or said textile layer;

providing a hollow member having an open end and an opposed closed end defining a fluid passageway therebetween and having a wall portion with at least one hole extending therethrough, the hole being in fluid communication with said fluid passageway;

providing a pressure controller at the open end of said hollow member;

concentrically placing said ePTFE layer and said textile layer onto said hollow member and over said at least one hole of said hollow member to provide an interior composite layer and an exterior composite layer, thereby defining a composite assembly, wherein said interior composite layer is one of said ePTFE layer or said textile layer and said exterior composite layer is the other of said ePTFE layer or said textile layer;

providing an elastic silicone barrier member;

expanding the elastic silicone member to a diameter greater that that of said hollow tubular member;

disposing the expanded silicone member over an exterior surface of said exterior composite layer;

reducing the diameter of the expanded silicone member to cover said aligned ePTFE layer and said aligned textile layer over said hollow member;

placing said hollow member with said composite assembly within a pressure chamber;

applying a positive pressure to said chamber so that the positive pressure within said chamber is higher than a pressure outside of said chamber;

applying a pressure differential so that the pressure within said chamber is greater than a pressure within said fluid passageway of said hollow member;

controlling said positive pressure and said pressure differential by said pressure controller;

applying heat to said bonding agent to adhesively bond said textile layer and said ePTFE layer to provide a laminated composite assembly; and

removing said elastic silicone barrier member from said laminated composite assembly.

31. The method of claim 27, wherein said laminated composite assembly has a bond shear strength of at least 5.5 g/mm² and a variation of said bond shear strength of less than about 2 and a bond peel strength of at of at least 32 g/mm and a variation of said bond peel strength of less than about 4.

28. A method of forming a composite textile and ePTFE implantable device comprising the steps of:

providing an ePTFE layer having opposed surfaces comprising a microporous structure of nodes interconnected by fibrils;

providing a textile layer having opposed surfaces;

applying a coating of an elastomeric bonding agent to one of said opposed surfaces of said ePTFE layer or said textile layer;

providing a hollow member having an open end and an opposed closed end defining a fluid passageway therebetween and having a wall portion with at least one hole extending therethrough, the hole being in fluid communication with said fluid passageway;

concentrically placing said ePTFE layer and said textile layer onto said hollow member and over said at least one hole of said hollow member to provide an interior composite layer and an exterior composite layer, thereby defining a composite assembly, wherein said interior composite layer is one of said ePTFE layer or said textile layer and said exterior composite layer is the other of said ePTFE layer or said textile layer;

providing an elastic silicone barrier member;

expanding the elastic silicone barrier member to a diameter greater that that of said hollow tubular member;

disposing the expanded silicone barrier member over an exterior surface of said exterior composite layer;

reducing the diameter of the expanded silicone barrier member to cover said aligned ePTFE layer and said aligned textile layer over said hollow member;

placing said hollow member with said composite assembly within a pressure chamber;

applying a positive pressure to said chamber so that the positive pressure within said chamber is higher than a pressure outside of said chamber;

applying a pressure differential so that the pressure within said chamber is greater than a pressure within said fluid passageway of said hollow member;

applying heat to said bonding agent to adhesively bond said textile layer and said ePTFE layer to provide a laminated composite assembly; and

removing said elastic silicone barrier member from said laminated composite assembly.

32. The method of claim 28, wherein said laminated composite assembly has a bond shear strength of at least 5.5 g/mm² and a variation of said bond shear strength of less than about 2 and a bond peel strength of at of at least 32 g/mm and a variation of said bond peel strength of less than about 4.

29. A method of forming a composite textile and ePTFE implantable device comprising the steps of:

providing an ePTFE layer having opposed surfaces comprising a microporous structure of nodes interconnected by fibrils;

providing a textile layer having opposed surfaces;

applying a coating of an elastomeric bonding agent to one of said opposed surfaces of said ePTFE layer or said textile layer;

providing a hollow member having an open end and an opposed closed end defining a fluid passageway therebetween and having a wall portion with at least one hole extending therethrough, the hole being in fluid communication with said fluid passageway;

providing a pressure controller at the open end of said hollow member;

concentrically placing said ePTFE layer and said textile layer onto said hollow member and over said at least one hole of said hollow member to provide an interior composite layer

and an exterior composite layer, thereby defining a composite assembly, wherein said interior composite layer is one of said ePTFE layer or said textile layer and said exterior composite layer is the other of said ePTFE layer or said textile layer;

providing a thin elastic silicone barrier member having a thickness of about 0.5 mm to about 1.25 mm;

expanding the thin elastic silicone barrier to a diameter greater that that of said hollow tubular member;

disposing the expanded thin elastic silicone barrier over an exterior surface of said exterior composite layer;

reducing the diameter of the expanded thin elastic silicone barrier to cover said aligned ePTFE layer and said aligned textile layer over said hollow member;

placing said hollow member with said composite assembly within a pressure chamber;

applying a positive pressure to said chamber so that the positive pressure within said chamber is higher than a pressure outside of said chamber;

applying a pressure differential so that the pressure within said chamber is greater than a pressure within said fluid passageway of said hollow member;

applying heat to said bonding agent to adhesively bond said textile layer and said ePTFE layer to provide a laminated composite assembly; and

removing said thin elastic silicone barrier member from said laminated composite assembly;

wherein a force exerted by the thin elastic silicone barrier on said aligned ePTFE layer and said aligned textile layer is less than said pressure differential.

33. The method of claim 29, wherein said laminated composite assembly has a bond shear strength of at least 5.5 g/mm² and a variation of said bond shear strength of less than about 2 and a bond peel strength of at of at least 32 g/mm and a variation of said bond peel strength of less than about 4.