Instrument and method for in situ deployment of cardiac valve prostheses

• US 7,993,392 B2
• Filed: 06/27/2008
• Issued: 08/09/2011
• Est. Priority Date: 12/19/2006
• Status: Active Grant

• Current Assignee: Corcym SRL (LivaNova Plc)
• Original Assignee: Sorin Biomedica Cardio Srl (LivaNova Plc)
• Inventors: Achiluzzi, Monica, Righini, Giovanni
• Primary Examiner(s): Tyson; Melanie
• Assistant Examiner(s): DANG, PHONG SON H
• Application Number:
  US12/147,567
• Publication Number:
  US 20080262507A1
• Time in Patent Office: 1,138 Days
• Field of Search: 623/2.11, 623/1.15, 623/1.2
• US Class Current: 623/2.11
• CPC Class Codes: A61F 2/2412 with soft flexible valve members, e.g. tissue valves shaped like natural valves check valves with flexible valve members in general F16K15/14
• CPC Class Codes: A61F 2/243 Deployment by mechanical expansion
• CPC Class Codes: A61F 2/2433 using balloon catheter
• CPC Class Codes: A61F 2/2436 Deployment by retracting a sheath

Abstract

An instrument for deploying a cardiac valve prosthesis, including a plurality of radially expandable portions, at an implantation site, includes a plurality of deployment elements each independently operable to obtain the radial expansion of a radially expandable portion of the valve prosthesis. A method for deploying the cardiac valve prosthesis includes advancing the instrument to an implant site and independently actuating the radially expandable portions.

Claims

1. A device for minimally-invasive delivery of an expandable heart valve prosthesis including an annular inflow portion, an annular outflow portion, and an anchoring protrusion, which is able to protrude radially outward beyond the annular inflow portion and the annular outflow portion, disposed therebetween before and after deployment of the heart valve prosthesis at an implantation site, the device comprising:

a carrier portion for enclosing and carrying the prosthesis, the carrier portion including a first deployment element adapted to enclose the annular outflow portion and a second deployment element adapted to enclose the annular inflow portion, wherein each of the first and second deployment elements are independently operable;

a control handle coupled to the carrier portion for controlling the first and second deployment elements;

wherein the first deployment element is a cap having an internal surface including a low friction material.

2. The device of claim 1 in which the low friction material comprises ultra-high molecular weight material.

3. The device of claim 1 in which the low friction material comprises PTFE.

4. The device of claim 1 in which the low friction material comprises Teflon™

.

5. The device of claim 1 in which the low friction material is coated on the first deployment element and the second deployment element.

6. The device of claim 1 in which the first deployment element and the second deployment element are made from the low friction material.

7. The device of claim 1 wherein the cap is made from low friction material.

8. The device of claim 1 wherein the cap is coated with a low friction material.