Sutureless vascular anastomosis connection
Techniques for sutureless vascular anastomosis are described, including a sutureless vascular anastomosis connector configured to couple a graft vessel to a main vessel, including a connector body configured to engage a main vessel when inserted into an opening in a wall of the main vessel, and a wing coupled to the connector body and formed using a memory material, the wing being configured to rotate about a transverse axis of the connector when a restraining force is removed from an exterior surface of the wing.
1. A sutureless vascular anastomosis system, comprising:
a vascular anastomosis connector, comprising:
a connector tip configured to engage a graft vessel, the connector tip being formed in a substantially wave-shaped pattern and configured to shrink in response to an applied force;
a connector body including a body tine formed using a memory material and configured to be deployed from the connector body and engage an interior surface of the graft vessel;
a connector base, wherein the connector tip, the connector body, and the connector base are one continuous structure, the connector base being configured to engage a main vessel when inserted into an opening in a wall of the main vessel, wherein a dividing line between the connector body and the connector base defines a diagonal plane, the diagonal plane representing an angle in which the connector body is configured to be coupled with the main vessel, and wherein the connector base comprises;
a front wing including a front tine;
a rear wing including a rear tine, wherein the front and rear wings are configured to deploy to predetermined angles, such that the front and rear wings are substantially parallel with the diagonal plane when deployed, and wherein the front and rear tines are separately deployable from the front and rear wings by swinging away from the wings at tine junctions; and
two side wings, wherein each of the side wings comprises a first barb with a first unfixed barb end comprising a first sharp end and a first protrusion extending from the first sharp end, and a second barb with a second unfixed barb end comprising a second sharp end and a second protrusion extending from the second sharp end, the first protrusion and the second protrusion being configured to pierce the wall of the main vessel from within the main vessel, wherein the front wing, the front tine, the rear wing, the rear tine, and the two side wings all comprise a shape memory material; and
an incision seal configured to lock with the connector by insertion of the first protrusion of the first barb of one of the side wings into a first slot disposed on a side wall of the incision seal and by insertion of the second protrusion of the second barb of said one of the side wings into a second slot disposed on the side wall of the incision seal, wherein the first protrusion of the first barb of said one of the side wings and the second protrusion of the second barb of said one of the side wings, once received in the first slot and the second slot, respectively, are configured to prevent the incision seal from separating from the connector body.
2. The system of claim 1 , wherein the shape memory material is an alloy comprising at least nickel and titanium.
3. The system of claim 1 , wherein the shape memory material is Nitinol.
4. The system of claim 1 , wherein the connector base is formed using the shape memory material with the front wing, the front tine, the rear wing, the rear tine, and the two side wings in a fully deployed state, wherein the front wing, the front tine, the rear wing, the rear tine, and the two side wings are configured to be restrained in a retracted state.
5. The system of claim 1 , wherein the front wing, the front tine, the rear wing, the rear tine, and the two side wings are configured to deploy when a restraining force is removed from an exterior surface of the connector base.