Sutureless vascular anastomosis connection
A system is described for performing vascular anastomosis without the use of sutures. The system includes a connector comprised of memory material and an incision seal. The connector has one end configured to securely engage a graft vessel and another end with wings and barbs. The wings are configured to securely engage an inner wall of a main vessel and the barbs are configured to lock with the incision seal. Once locked, the incision seal and the connector apply a clamping force that secures the graft vessel with the main vessel.
1. A sutureless vascular anastomosis system, comprising:
a connector configured to attach a graft vessel to a main vessel when the connector is inserted into an incision of the main vessel, wherein the connector comprises a deployable barb that is integrally formed in the connector, the deployable barb having a barb junction integrally formed in the connector, the deployable barb configured to bend away from the connector at the barb junction in a direction towards the second vessel when deployed;
a support tube sized to fit over at least a portion of the connector, to sandwich the graft vessel between the support tube and the connector and secure the graft vessel to the main vessel, the support tube comprising:
a body configured to partially house the graft vessel and including an angled end; and
a ring disposed circumferentially around an outer surface of the body; and
an incision seal configured to fit over the support tube and couple with the connector to cover a portion of a wall of the main vessel, the incision seal comprising:
a base configured to support the wall of the main vessel;
a recess;
a first housing opening;
a second housing opening configured to receive the support tube;
a lumen connecting the first housing opening and the second housing opening and configured to receive the support tube; and
a groove disposed within the lumen and configured to couple with the ring of the support tube when the support tube is received within the lumen of the incision seal,
wherein the deployable barb of the connector is configured to puncture the wall of the main vessel and lock with the incision seal.
2. The system of claim 1 , wherein the support tube secures the graft vessel to the wall of the main vessel when the deployable barb locks with the incision seal.
3. The system of claim 1 , wherein the connector includes a tine integrally formed in the connector and configured to secure the connector to the graft vessel or the main vessel.
4. The system of claim 1 , wherein the connector comprises a memory material configured to deploy the deployable barb at a pre-determined angle when a restraining force is removed from the deployable barb.
5. The system of claim 4 , wherein the memory material is a nickel titanium alloy.
6. The system of claim 1 , wherein the connector further comprises a deployable wing integrally formed in the connector and configured to secure the connector to the main vessel.
7. The system of claim 1 , wherein connector further comprises a deployable wing integrally formed in the connector and having one or more tines configured to engage the main vessel.
8. The system of claim 1 , wherein the incision seal comprises a malleable material configured to receive and create a seal around the deployable barb.
9. The system of claim 1 , wherein the support tube is configured to couple an end of the graft vessel over a distal end of the connector.
10. The system of claim 1 , wherein the connector is secured to the second vessel using the deployable barb.
11. The system of claim 1 , wherein the connector further comprises:
a distal end; and
one or more tines integrally formed in the connector at the distal end and configured to engage an inner surface of the graft vessel when the support tube and the graft vessel are positioned over the connector.
12. The system of claim 1 , wherein the support tube further comprises a notch on the angled end of the support tube, wherein the connector further comprises a deployable wing connected to the connector by a hinge, and wherein the notch is configured to provide clearance for the hinge of the connector to deploy the deployable wing.
13. The system of claim 1 , wherein the support tube comprises Teflon tubing.