System for deploying an anastomosis device and method of performing anastomosis

Information

  • Patent Grant
  • 6471713
  • Patent Number
    6,471,713
  • Date Filed
    Monday, November 13, 2000
    23 years ago
  • Date Issued
    Tuesday, October 29, 2002
    21 years ago
Abstract
A deployment system for forming an incision in a target vessel, for placement of an anastomosis device and for deployment of an anastomosis device having an inner flange formed by radial expansion of the device and an outer flange formed by axial compression of the device.
Description




BACKGROUND OF THE INVENTION




1. Field of the Invention




The invention relates to a system for deployment of an anastomosis device and a method of performing anastomosis. In a preferred embodiment, the system can be used for piercing a vessel wall as an initial step in forming a sutureless connection between a bypass graft and a blood vessel, and the subsequent deployment of an anastomosis device.




2. Brief Description of the Related Art




Vascular anastomosis is a procedure by which two blood vessels within a patient are surgically joined together. Vascular anastomosis is performed during treatment of a variety of conditions including coronary artery disease, diseases of the great and peripheral vessels, organ transplantation, and trauma. In coronary artery disease (CAD) an occlusion or stenosis in a coronary artery interferes with blood flow to the heart muscle. Treatment of CAD involves the grafting of a vessel in the form of a prosthesis or harvested artery or vein to reroute blood flow around the occlusion and restore adequate blood flow to the heart muscle. This treatment is known as coronary artery bypass grafting (CABG).




In the conventional CABG, a large incision is made in the chest and the sternum is sawed in half to allow access to the heart. In addition, a heart lung machine is used to circulate the patients blood so that the heart can be stopped and the anastomosis can be performed. During this procedure, the aorta is clamped which can lead to trauma of the aortic tissue and/or dislodge plaque emboli, both of which increase the likelihood of neurological complications. In order to minimize the trauma to the patient induced by conventional CABG, less invasive techniques have been developed in which the surgery is performed through small incisions in the patients chest with the aid of visualizing scopes. Less invasive CABG can be performed on a beating or stopped heart and thus may avoid the need for cardiopulmonary bypass.




In both conventional and less invasive CABG procedures, the surgeon has to suture one end of the graft vessel to the coronary artery and the other end of the graft vessel to a blood supplying vein or artery. The suturing process is a time consuming and difficult procedure requiring a high level of surgical skill. In order to perform the suturing of the graft to the coronary artery and the blood supplying artery the surgeon must have relatively unobstructed access to the anastomosis site within the patient. In the less invasive surgical approaches, some of the major coronary arteries including the ascending aorta cannot be easily reached by the surgeon because of their location. This makes suturing either difficult or impossible for some coronary artery sites. In addition, some target vessels, such as heavily calcified coronary vessels, vessels having very small diameter, and previously bypassed vessels may make the suturing process difficult or impossible.




An additional problem with CABG is the formation of thrombi and atherosclerotic lesions at and around the grafted artery, which can result in the reoccurrence of ischemia. The thrombi and atherosclerotic lesions may be caused by the configuration of the sutured anastomosis site. For example, an abrupt edge at the anastomosis site may cause more stenosis than a more gradual transition.




Accordingly, it would be desirable to provide a sutureless vascular anastomosis device which easily connects a graft to a target vessel and can be deployed in limited space. It would also be desirable to provide a sutureless anastomosis device which is formed of one piece and is secured to the target vessel by a one piece tool which can perform both the initial piercing of the tissue and deployment of the anastomosis device.




SUMMARY OF THE INVENTION




According to a preferred embodiment, the present invention relates to a deployment system for forming an incision in a wall of a target vessel and delivering an anastomosis device for connecting an end of a graft vessel to a target vessel at the site of the incision. The deployment system preferably includes a trocar, a tissue punch having a piercing element at a distal end thereof for being advanced through the trocar to form a puncture and for thereafter being withdrawn from the trocar, a holder tube slidably disposed within the trocar, an expander tube for cooperating with the holder tube, and a rotatable control, whereby rotation of the control causes advancing and withdrawal of the tissue punch and relative slidable movement between the trocar, the holder tube, and the expander tube for deployment of the anastomosis device. In a further aspect of the invention, the trocar is a tubular member having a passage therein through which the anastomosis device is deliverable to the incision site. Still further, the piercing element comprises a cutting blade which is movable with respect to the trocar such that the cutting blade can be moved from a cutting position at which the cutting blade is exposed to a retracted position at which the cutting blade is not exposed.




According to a further aspect of the present invention, the preferred embodiment is directed to an anastomosis device deployment system including a deployment tool having a rotatable control knob, a holder tube attached to the tool, the holder tube having a distal end configured to hold the anastomosis device with an attached graft vessel, and an expander positioned within the holder and slidable with respect to the holder to a position at which the expander is positioned within the anastomosis device and radially expands the anastomosis device. The system further preferably includes a trocar movable with respect to the holder tube to form an opening in a target vessel to receive the anastomosis device and attached graft vessel. Still further, the deployment tool includes three cam grooves, and the trocar, holder tube and expander each have a follower member engaged in one of the cam grooves to move the trocar, holder tube and expander with respect to one another upon rotation of the control knob.




In accordance with a further embodiment of the invention, a method of performing anastomosis includes providing a deployment tool having a trocar, an expander tube, a holder tube holding a one-piece tubular anastomosis device having an end of a graft vessel everted around the anastomosis device, and a rotatable control knob for moving the trocar, the expander tube and the holder tube relative to one another. The method includes rotating the control knob to puncture a target vessel with the trocar, rotating the control knob to insert the tubular anastomosis device with everted graft vessel into the puncture in the target vessel, rotating the control knob to radial expand the tubular anastomosis device with the expander tube to cause a portion of the anastomosis device to fold outward forming a first annular flange, and rotating the control knob to form a second annular flange on the anastomosis device to trap a wall of the target vessel between the first and second annular flanges and seal the graft vessel to the target vessel. According to a preferred embodiment of the method, enlargement of an internal diameter of the anastomosis device with the expander tube causes the formation of the first flange. According to a further aspect of the invention, the device is expanded by an expander in the form of an inflatable balloon. Still further, in a preferred method of the invention, the radial expansion of the anastomosis device causes a portion of the device to bend at a plurality of hinges to form the first and second annular flanges. The deployment tool may further comprise a tissue punch, wherein rotation of the control knob causes advancement of the tissue punch into the target vessel prior to advancement of the trocar.




Preferably, the target vessel is an aorta and the method is performed without occlusion (i.e., clamping) of the aorta. The end of the graft vessel and the edges of the incision in the target vessel can be captured between the first portion and the second portion so that the end of the graft vessel abuts an outside wall of the target vessel. The anastomosis device can be expandable from a first configuration to a larger second configuration where the anastomosis device is expanded with an expander to cause a portion of the anastomosis device to fold outward forming the first flange. In this regard, the first flange holds a portion of the graft vessel in contact with an inner surface of the target vessel.











BRIEF DESCRIPTION OF THE DRAWINGS




The invention will now be described in greater detail with reference to the preferred embodiments illustrated in the accompanying drawings, in which like elements bear like reference numerals, and wherein:





FIG. 1

is perspective views of a typical embodiment of an anastomosis device in a planar configuration;





FIG. 2

is a perspective view of the anastomosis device of

FIG. 1

in a configuration attached to the deployment tool of the present invention, prior to deployment;





FIG. 3A

is a perspective views of an anastomosis device deployment tool in accordance with the present invention;





FIG. 3B

is a side elevational view thereof;





FIG. 4A

is a sectional perspective view of a further embodiment of an anastomosis device deployment tool in accordance with the present invention;





FIG. 4B

is a side elevational view thereof;





FIG. 5

is a side cross sectional view of a loaded tissue punch device for use in the anastomosis device deployment tool shown in

FIG. 3

;





FIG. 5A

is an enlarged view thereof;





FIG. 6

is a side cross sectional view of the tissue punch device loaded into the anastomosis device deployment tool shown in

FIG. 3

;





FIG. 6A

is an enlarged view thereof;





FIG. 7

is a side cross sectional view of the anastomosis device deployment tool with the piercing element puncturing the target vessel;





FIG. 7A

is an enlarged view thereof;





FIG. 8

is a side cross sectional view of the anastomosis device deployment tool with the trocar moved forward for cutting an opening in the vessel wall;





FIG. 8A

is an enlarged view thereof;





FIG. 9

is a side cross-sectional view of the deployment tool when the tissue punch spring has fired;





FIG. 9A

is an enlarged view thereof;





FIG. 10

is a side cross-sectional view of the deployment tool as the tissue punch is being withdrawn through the opening in the side of the trocar;





FIG. 10A

is an enlarged view thereof;





FIG. 11

is a side cross-sectional view of the deployment tool with the tissue punch device pivoted entirely out of the trocar;





FIG. 11A

is an enlarged view thereof;





FIG. 12

is a side cross-sectional view of the deployment tool with the holder tube and expander tube moved forward for the deployment of the anastomosis device;





FIG. 12A

is an enlarged view thereof;





FIG. 13

is a side cross-sectional view of the deployment tool with the holder tube and expander tube advanced to begin deployment of the inner flange of the anastomosis device and the trocar beginning to be withdrawn;





FIG. 13A

is an enlarged view thereof;





FIG. 14

is a side cross sectional view of the deployment tool with the expander tube advanced to complete deployment of the inner flange of the anastomosis device and the trocar further withdrawn;





FIG. 14A

is an enlarged view thereof;





FIG. 15

is a side cross sectional view of the deployment tool with the trocar withdrawn and the expander withdrawn so as to seat the inner flange of the anastomosis device;





FIG. 15A

is an enlarged view thereof;





FIG. 16

is a side cross sectional view of the deployment tool with the holder tube advanced for deployment of the outer flange of the anastomosis device and disengagement of the anastomosis device therefrom;





FIG. 16A

is an enlarged view thereof;





FIG. 17

is a side cross sectional view of the deployment tool with the trocar, expander tube and holder tube withdrawn for tool removal from the target vessel; and





FIG. 17A

is an enlarged view thereof.











DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS




According to the invention it is possible to perform a variety of anastomosis procedures, including coronary artery bypass grafting. The term “target vessel” is thus used to refer to vessels within the patient which are connected to either or both of the upstream and downstream end of the graft vessel. In such procedures, a large vessel anastomotic device is used with large diameter target vessels such as the aorta or its major side branches.




In deploying a large vessel anastomotic device, the device (with one end of a graft vessel attached thereto) is inserted into an incision in a wall of the target vessel with a deformable section in a first configuration, and the deformable section is radially expanded to a second configuration to deploy a flange. The flange applies an axial force against the wall of the target vessel. Additionally, the flange can be configured to apply a radial force, substantially transverse to the device longitudinal axis, against the wall of the target vessel, to secure the device to the target vessel. For example, the device can have a plurality of deformable sections forming distal and proximal flanges. With the proximal and distal end flanges deployed, the device can be prevented from shifting proximally out of the target vessel or distally further into the interior of the target vessel.




In a coronary bypass operation in accordance with the invention, a device can be used to connect the proximal end of the graft vessel to the aorta. However, in patients with an extreme arteriosclerotic lesion in the aorta, which may result in serious complications during surgical procedures on the aorta, the surgeon may wish to avoid this region and connect the proximal end of the graft vessel to any other adjacent less diseased vessel, such as the arteries leading to the arms or head. Further, the devices can be used with venous grafts, such as a harvested saphenous vein graft, arterial grafts, such as a radial artery, or a synthetic prosthesis, as required.




Connection of the present device does not require the stoppage of blood flow in the target vessel. Moreover, through the use of the device of the present invention, anastomotic devices can be connected to the target vessel without the use of cardiopulmonary bypass, thereby avoiding many of the risks of conventional heart surgery. For example, anastomosis techniques wherein the aorta is clamped to interrupt blood flow to the area of the aortic wall to which a vein is to be anastomosed may result in liberation of plaques and tissue fragments which can lead to organ dysfunction, such as strokes, renal failure, or intestinal ischemia. Further, severely diseased aortas may not provide an area suitable for clamping due to significant calcification of the aortic wall.




According to the invention, a sutureless connection can be provided between a graft and a target vessel, while minimizing thrombosis or restenosis associated with the anastomosis. The anastomotic devices can be attached to the target vessel inside a patient remotely from outside the patient using specially designed applicators, so that the devices are particularly suitable for use in minimally invasive surgical procedures where access to the anastomosis site is limited. The devices allow the anastomosis to be performed very rapidly, with high reproducibility and reliability, without clamping, and with or without the use of cardiopulmonary bypass.




According to one preferred method of deploying the anastomosis device, the surgeon operates a deployment tool using both hands. One hand supports the tool via a handle while the other twists an actuation knob or other control member to deploy the anastomotic device. Locating the actuation knob on the tool's main axis minimizes the tendency of reaction forces to wobble the tool keeping it stable and in proper position during deployment. The twisting motion is converted to linear displacements by a set of rotating cams that engage a trocar, holder, and expander. The cams control the sequence of relative motions between the instrument's trocar and device deployment mechanisms.




During the foregoing procedure, a surgeon will place the tip of the instrument (the mechanical stop) in light contact with the site on the aorta to be anastomosed. Having located a suitable site, the surgeon then twists the actuation knob to fire the spring-loaded tissue punch and continues twisting to continue deployment of the anastomotic device. The trocar penetrates the aortic wall and maintains a substantially fluid-tight seal at the puncture site. Having entered the aortic lumen, the trocar forms a passageway for the anastomotic device and its holder tube (crown) to be advanced, thus retracting the aortic tissue and serving as an introducer for the device. Once the device has fully entered the aortic lumen the trocar begins to be withdrawn, while the anastomotic device is then expanded to its full diameter and an inner flange is deployed. The device is then drawn outwards towards the instrument where a mechanical stop is encounters, and where the inner flange is firmly seated against the intimal wall of the aorta. An outer flange is then deployed from the external side, compressing the aortic wall between the inner and outer flanges, and finally, the device is disengaged from the instrument completing the anastomosis.





FIGS. 1 and 2

illustrate an exemplary anastomosis device


600


(illustrated in planar form in

FIG. 1

for ease of description but which would be used in a tubular shape as shown in

FIG. 2

) which cooperates with a deployment tool


150


(described below) for delivering and deploying an implant


604


at a site in a living body. The anastomosis device


600


includes a frangible linkage


602


connecting the implant


604


to a discard portion


606


. As explained in greater detail below, after the device


600


is positioned at a desired location, the implant


604


can be expanded to deploy an inner flange and subsequently axially compressed to deploy an outer flange while severing the implant


604


from the discard portion


606


. The deployment tool can then be withdrawn along with the discard portion


606


which remains attached to the distal end of the deployment tool.




During radial expansion of the device, axially extending barbs


608


are pivoted outwardly by struts


610


such that the outwardly extending barbs


608


and struts


610


form the inner flange. To facilitate bending of the barbs, the barbs


608


comprise points on the ends of axially extending members


612


which have narrow sections


614


located a desired distance from the free ends of the barbs


608


. For instance, the narrow sections


614


can be located at axial positions along the device corresponding approximately to a position slightly distal of the axial midpoint of the struts


610


connecting adjacent members


612


when the device is in the preexpanded condition.




To facilitate easier bending of the struts


610


during radial expansion of the device, the distal ends of the struts can be curved at their points of attachment to the members


612


. Likewise, a curved bend can be provided at the intersection where the proximal ends of the struts are attached together. When the device is radially expanded, the members


612


move radially outward and circumferentially apart as the struts


610


move radially outward until a force on the barbs


608


by the struts


610


causes the struts to become bent at the narrow sections


614


, after which the barbs extend outwardly to form the inner flange. In this deployed condition, the barbs


608


are locked into position by an X-shaped frame formed by struts


610


and additional struts


616


. The struts


616


are similar in configuration to the struts


610


with respect to how they are shaped and attached to the members


612


. Short axially extending members


618


connect the intersection of the struts


610


to the intersection of the struts


616


.




The frangible section


602


is located at the proximal ends of axially extending members


620


which are connected to the members


612


by U-shaped links


622


. The members


620


are arranged as circumferentially spaced apart pairs which are attached together at midpoints of links


622


. During radial expansion of the device, the individual links


622


are plastically deformed from their U-shaped configuration to form segments of a circumferentially extending annular ring. As a result, the device becomes shorter in the axial direction as links


622


form the annular ring. At the same time, the proximal ends of each pair of members


620


attached to an individual link


622


move radially outward and apart in the circumferential direction.




The frangible section


602


is located between pairs of the axial members


620


and pairs of axially extending members


624


. As shown in

FIG. 1

, the members


620


are substantially parallel to each other when the device is in its unexpanded condition, i.e., prior to formation of the inner flange. However, when the device is radially expanded the distal ends of the members


620


will remain closer together than their proximal ends since the distal ends are attached to a midpoint of the links


622


. The proximal ends of pairs of the members


624


are attached at mid-points of U-shaped links


626


by a pair of thin links


627


. During expansion of the device, the U-shaped links


626


deform into a circumferentially extending ring while proximal ends of pairs of the members


624


spread apart such that a gap


628


between the pairs of members


624


becomes wider at the proximal ends of the members


624


. To aid spreading of the pairs of members


624


, the members


624


include a curved recess


629


at the distal ends thereof. The distal ends of members


624


are connected to the proximal ends of the members


620


by a frangible joint comprised of shearable connections


602


, the members


620


are connected at their proximal ends by a cross piece


630


and the members


624


are connected by a cross piece


635


which includes a projection


636


received in a recess


634


. The frangible joint is formed from a unitary piece of material such as a laser cut tube wherein the shearable connections


602


comprise thin sections of material extending between opposite sides of the projection


636


and opposing walls of the recess


634


. When the members


620


and


624


are pivoted to a sufficient extent, the shearable connections


602


are fractured allowing the implant to separate from the discard portion of the device.




Referring also to

FIG. 2

, the device


600


can be deployed by using a deployment tool


150


, described in greater detail below. Briefly, the device


600


includes a crown attached to a distal end of the deployment tool. The crown includes axially extending members


642


with tabs


643


on the proximal ends thereof, the members


642


being held in slots


151


of the tool


150


by the tabs


643


. A plastic sleeve (not shown) can be placed over the slots


151


to prevent the members


642


from coming out of the slots. When mounted on the deployment tool with an everted graft vessel thereon (not shown), the crown is flared outwardly such that the members


642


are fully radially expanded at their proximal ends. During radial expansion of the device


600


, the diamond shaped linkage of the crown


640


is expanded from an unexpanded condition like the configuration shown in

FIG. 1

to an expanded condition having deployed inner and outer flanges.




Although anastomosis device


600


is shown and described for utilization with the deployment system of the present invention, it should be clear to one skilled in the art that other embodiments of such anastomosis devices could of course also be used herewith, including but not limited to, those described for example in U.S. application Ser. Nos. 09/314,278 and 09/437,428, the entire contents of which are hereby incorporated by reference.





FIGS. 3A and 3B

illustrate the deployment system


150


of the present invention, and the sequential deployment of an anastomosis device


600


, including insertion of the anastomosis device past the aortic wall into the aortic lumen, deployment of an inner flange, seating the inner flange on the aortic intima, deployment of the outer flange, seating of the outer flange, and then fixing of the anastomosis device in place and detachment from the tool, is shown in

FIGS. 51-7A

. The deployment system


150


includes a hollow outer trocar


152


, a holder tube


154


(not shown in

FIGS. 3A-3B

) positioned inside the trocar


152


, and an expandable member or expander tube


156


(not shown in

FIGS. 3A-3B

) slidably disposed inside of the holder tube


154


. As described in detail in the above-mentioned U.S. Ser. Nos. 09/314,278 and 09/437,428, the anastomosis device may be attached to the distal end of the holder tube by inserting members


642


of the device into slots


151


which are formed around the circumference of the holder tube, or by insert-molding, or by any other attachment means. The trocar


152


, holder tube


154


and expander tube


156


are all slidable with respect to one another during operation of the device. A control member or device handle


160


, preferably a rotatable knob, is provided for moving the tubes with respect to one another through sequential movement of the cams


178


,


180


,


182


,


183


as discussed further below. The device also includes cam connectors


188


which preferably fasten together two halves (shown as a unitary body) which define the cam body


189


. The movement of the cams can be caused by mechanical, manual, or pneumatic actuation, as well as any other type of known means for obtaining relative movement. The operation thereof to deploy the anastomosis device


600


according to the present invention is sequentially shown in

FIGS. 5-17

.





FIGS. 5-5A

illustrate a tissue punch


100


in accordance with the present invention, and as more fully described in U.S. application Ser. No. 09/542,976, the entire contents of which is hereby incorporated by reference. As illustrated, the tissue punch


100


is loaded and ready for attachment to the deployment system


150


. The tissue punch


100


includes a piercing element


102


positioned within the trocar


152


. The piercing element


102


can be retracted in the trocar


152


by an elongated member


104


, such as a spring steel strap or cable which extends through an opening


153


in a side of the trocar


152


. The piercing element


102


includes a pointed distal tip


106


for penetrating the target vessel wall


32


and a narrow shaft portion


108


around which the tissue of the target vessel wall


32


contracts after piercing. The deployment system of the present invention further includes a mechanical stop


159


which is preferably compliant in nature in that it may be spring loaded and which will abut the outer wall surface of the aorta during the anastomosis procedure. The spring loading on the stop


159


is preferably in the range of approximately 0.5 to 3.0 pounds. As shown in

FIG. 5A

, the mechanical stop has been located against the wall of the aorta and will be locked in said position by the cam rotation to function as a reference point for locating the outer wall of the aorta during further operation of the deployment tool


150


.





FIGS. 6-6A

illustrate the tissue punch


100


attached to the deployment tool


150


. The deployment tool


150


preferably includes a cam body


189


having four contoured cam slots


178


,


180


,


182


,


183


corresponding to the trocar


152


, holder tube


154


, expander tube


156


, and a retraction release mechanism for the tissue punch


100


, respectively. Each of the tubes has a fitting


184


at a distal end thereof. An engagement member or pin


186


connected to each of the fittings


184


slides in a corresponding one of the cam slots


178


,


180


,


182


,


183


. Alternatively, it is within the scope of the present invention to provide the deployment tool with additional or fewer cam slots. Still further, in accordance with a further embodiment of the invention as shown in

FIGS. 4A and 4B

(prime reference numerals being used to denote similar features) the cam grooves


178


′,


180


′,


182


′,


183


′ may be formed in one or more rotatable cylinders


190


and engagement members


186


′ are provided for engagement within the grooves. A spring


196


′ is provided which, upon release during the initial rotation of the knob


160


′, results in firing of the piercing element


102


of the tissue punch


100


′. A further spring


104


′ is provided for retraction of the tissue punch upon the release thereof during subsequent rotation of the control member


160


′, as discussed further below with respect to the first embodiment of the invention. In both embodiments of the present invention, as the knob


160


is rotated, the engagement members slide in the respective cam slots or grooves to cause corresponding rotation of the cams and to cause actuation and retraction of the tissue punch and to move the trocar, holder tube and expander tube to the successive positions illustrated in

FIGS. 5-17

, and deploy the anastomosis device, as explained in detail below with respect to the first embodiment of the invention. A gear box may also be utilized to obtain the desired correspondence between rotation of the control member and the corresponding rotation of the cams. As shown in

FIG. 6

, a trigger pin


194


is engaged with a collar


192


of the tissue punch


100


so as to prevent the inadvertent firing of the piercing element prior to release. A spring


196


is also shown in its compressed state awaiting release of the trigger pin


194


.




Upon rotation of the knob


160


by the surgeon, thereby obtaining rotation of the cams as shown in

FIG. 7

, the trigger pin


194


releases the collar


192


and the compressed spring


196


. The piercing element


102


of the tissue punch


100


is thus advanced by the spring actuation into the wall of the target vessel


32


, as shown in the enlarged view of

FIG. 7A

, while the trocar


152


remains within the housing


158


. After piercing, the tissue of the target vessel wall rests around the shaft portion


108


of the piercing element


102


.




Referring to

FIGS. 8 and 8A

, the knob


160


has been further rotated as evidenced by the further rotated position of the cams


178


,


180


,


182


,


183


, and the trocar


152


and tissue punch sheath


162


have been advanced through the target vessel wall to thereby capture the piercing element


102


within the sheath


162


and punch the required opening


34


in the target vessel


32


. The tissue surrounding the shaft


108


is severed from the vessel wall and trapped within the sheath


162


for excision. As illustrated, the pin


186


is disposed at the terminal edge of cam slot


183


, just prior to release of the tissue retraction mechanism


198


.





FIGS. 9-11A

illustrate the retraction of the tissue punch


100


upon successive rotation of the knob


160


and the corresponding rotation of the cams following the release of pin


186


from cam slot


183


. In

FIG. 9A

, the retraction spring


104


has been actuated and the piercing element


102


is withdrawn such that it bottoms on a rear surface


164


of the sheath


162


. Further retraction of the tissue punch


100


, as shown in

FIG. 10A

, causes the tissue punch to rotate out of the opening


153


in the trocar


152


. As shown in

FIG. 11A

, the tissue punch


100


continues to rotate to a storage position outside of the trocar


152


within the housing


158


. When the tissue punch


100


is in the storage position, the lumen within the trocar


152


can be used to maintain the opening


34


within the blood vessel and for delivery of the anastomosis device to the puncture site in the target vessel.




Further rotation of the knob


160


brings the cams


178


,


180


,


182


to the rotated position shown in FIG.


12


. In so doing, the holder tube


154


with the anastomosis device


600


attached thereto has been shuttled forward to the puncture site along with the expander tube


156


, while the trocar


152


has begun to withdraw.




Referring to

FIGS. 13-13A

, the cams have been further rotated. Moreover, the holder tube


154


has advanced to within the target vessel with the anastomosis device


600


attached thereto. The expander tube


156


is immediately behind the holder tube


154


prior to deployment of the anastomosis device


600


, while the trocar


152


has further withdrawn within through the opening


34


. The anastomosis device


600


is now in position for deployment. More particularly, due to the variation in the thickness of the aortic wall among patients, the holder tube is advanced significantly past, approximately 0.2 inch for example, a position which would be required for the thickest possible aortic wall such that the surgeon can be certain that the anastomosis device is within the lumen of the target vessel and the inner flange will thus be deployed intramurally, as described below.





FIGS. 14-14A

show the cams further rotated by the knob


160


and the cam slot


182


has caused the expander tube


156


to be advanced through the holder tube


154


to thereby deploy the inner flange


20


of the anastomosis device. Although an expander tube is preferable for causing the deployment of the inner flange, it is within the scope of the present invention to use other mechanisms for causing the deployment thereof. The trocar


152


has also been further withdrawn from the puncture site.





FIGS. 15-15A

show that further rotation of the knob


160


causes the further pivoting of the cams


178


,


180


,


182


. As shown in

FIG. 15A

, the holder tube


154


and the expander tube


156


have been slightly withdrawn to pull the inner flange of the anastomosis device


600


against the vessel wall


32


. The trocar


152


is also now completely withdrawn into the housing


158


. Because of the variation in the thickness of the aortic wall among patients, the retraction of the inner flange is overshot beyond that which would be required for the thinnest possible aortic wall. In so doing, the present invention ensures that the inner flange will be in firm contact with the inner surface of the aortic wall. The mechanical stop


159


is released from its locked reference point during seating of the inner flange, and the compliant nature thereof allows the stop


159


to thus function as a counter-force against the withdrawal of the holder tube and expander tube and the retraction of the inner flange. An alternative embodiment to the mechanical stop may not be spring loaded, but rather, may include a larger outer diameter on the distal end thereof. As such, the mechanical stop will cause the surrounding tissue to stretch and thus provide a certain degree of resiliency which can adequately counteract the withdrawal force during the seating of the inner flange.




As shown in

FIGS. 16-16A

, the cams have been further pivoted due to the successive rotation of the knob


160


, and in so doing the holder tube


154


has moved forward again to deploy the outer flange


22


of the anastomosis device through compression of the linkages, and disengage the holder tube


154


from the anastomosis device


600


. The inner and outer radial flanges


20


,


22


trap the wall of the target vessel


32


between the flanges and thus secure the everted graft vessel


30


to the target vessel. In this instance, the mechanical stop


159


abuts the outer wall surface of the aorta during the deployment of the outer flange and prevents the unseating of the inner flange.




Final rotation of the knob


160


brings about the withdrawal of the holder tube


154


and the expander tube


156


from the puncture site, which thereby aids in removal of the deployment system


150


from the vessel, as illustrated in

FIGS. 17-17A

.




The trocars and anastomosis devices described above can be single piece or multi-piece devices which are formed by laser cutting or punching from a tube or sheet of material. The devices may be provided in varying sizes to join vessels of different sizes.




Although the invention has been principally discussed with respect to coronary bypass surgery, the trocar and/or anastomosis devices of the present invention may be used in other types of anastomosis procedures. For example, the trocar and/or anastomosis device may be used in femoral-femoral bypass, vascular shunts, subclavian-carotid bypass, organ transplants, and the like.




The trocar and/or anastomosis devices may be made of any known material which can be elastically or plastically deformed such as stainless steel, nickel titanium alloys, polymer materials, and the like.




While the invention has been described in detail with reference to the preferred embodiments thereof, it will be apparent to one skilled in the art that various changes and modifications can be made and equivalents employed, without departing from the present invention.



Claims
  • 1. A deployment system for forming an incision in a wall of a target vessel and delivering an anastomosis device for connecting an end of a graft vessel to a target vessel at the site of the incision, the deployment system comprising:a holder tube; a deployment tube for cooperating with the holder tube; and a rotatable control, whereby rotation of the control causes relative slidable movement between the holder tube and and the deployment tube.
  • 2. The deployment system of claim 1, further comprising a trocar, the holder tube being slidably disposed within the trocar.
  • 3. The deployment system of claim 2, wherein the trocar comprises a tubular member having a passage therein through which the anastomosis device is deliverable to the incision site.
  • 4. The deployment system of claim 2, further comprising a tissue punch having a piercing element at a distal end thereof for forming a puncture, wherein the piercing element comprises a cutting blade which is movable with respect to the trocar such that the cutting blade can be moved from a cutting position at which the cutting blade is exposed to a retracted position at which the cutting blade is not exposed.
  • 5. The deployment system of claim 4, wherein the piercing element includes a vessel wall piercing portion and a trimming portion, the piercing portion forming the incision upon insertion of the distal end of the member into the vessel wall and the trimming portion removing tissue around the incision upon retraction of the member.
  • 6. An anastomosis device deployment system comprising:a tool having a rotatable control member; a holder tube attached to the tool, the holder tube having a distal end configured to hold the anastomosis device with an attached graft vessel; and an deployment member positioned within the holder and slidable with respect to the holder to a position at which the deployment member is positioned within the anastomosis device and thereby deploys the anastomosis device.
  • 7. The system of claim 6, further comprising a trocar movable with respect to the holder tube to form an opening in a target vessel to receive the anastomosis device and attached graft vessel.
  • 8. The system of claim 7, wherein the tool includes three cam grooves, and the trocar, holder tube and deployment member each have a follower member engaged in one of the cam grooves to move the trocar, holder tube and deployment member with respect to one another upon rotation of the control member.
  • 9. The system of claim 8, wherein the tool includes at least one rotatable cylinder, said cam grooves being disposed on the at least one cylinder.
  • 10. The system of claim 6, further comprising a tissue punch having a piercing element for establishing an initial puncture of a vessel wall.
  • 11. The system of claim 6, further comprising a compliant mechanical stop.
  • 12. A method of performing anastomosis comprising:providing a deployment tool having a trocar, an expander, a holder tube holding a one-piece tubular anastomosis device having an end of a graft vessel everted around the anastomosis device, and a rotatable control knob for moving the trocar, the expander tube and the holder tube relative to one another; rotating the control knob to puncture a target vessel with the trocar; rotating the control knob to insert the tubular anastomosis device with everted graft vessel into the puncture in the target vessel; rotating the control knob to radial expanding the tubular anastomosis device with the expander to cause a portion of the anastomosis device to fold outward forming a first annular flange; and rotating the control knob to form a second annular flange on the anastomosis device to trap a wall of the target vessel between the first and second annular flanges and seal the graft vessel to the target vessel.
  • 13. The method of claim 12, wherein enlargement of an internal diameter of the anastomosis device with the expander tube causes the formation of the first flange.
  • 14. The method of claim 12, wherein the anastomosis device is expanded by advancing the expander with an outer diameter greater than an inner diameter of the anastomosis device into the anastomosis device.
  • 15. The method of claim 12, wherein the device is expanded by the expander in the form of an inflatable balloon.
  • 16. The method of claim 12, wherein the radial expansion of the anastomosis device causes a portion of the device to bend at a plurality of hinges to form the first annular flange.
  • 17. The method of claim 12, wherein the first and second annular flanges each form an angle between about 45 and 100 degrees with an axis of the device.
  • 18. The method of claim 12, wherein the deployment tool further comprises a tissue punch, wherein rotation of the control knob causes advancement of the tissue punch into the target vessel prior to puncturing thereof by the trocar.
US Referenced Citations (194)
Number Name Date Kind
2370776 Carlson Mar 1945 A
3254650 Collito Jun 1966 A
3254651 Collito Jun 1966 A
3519187 Kapitanov et al. Jul 1970 A
3774615 Lim et al. Nov 1973 A
4118806 Porier et al. Oct 1978 A
4214587 Sakura, Jr. Jul 1980 A
4217664 Faso Aug 1980 A
4350160 Kolesov et al. Sep 1982 A
4352358 Angelchik Oct 1982 A
4366819 Kaster Jan 1983 A
4368736 Kaster Jan 1983 A
4503568 Madras Mar 1985 A
4523592 Daniel Jun 1985 A
4534761 Raible Aug 1985 A
4553542 Schenck et al. Nov 1985 A
4577631 Kreamer Mar 1986 A
4589416 Green May 1986 A
4593693 Schenck Jun 1986 A
4603693 Conta et al. Aug 1986 A
4607637 Berggren et al. Aug 1986 A
4624255 Schenck et al. Nov 1986 A
4624257 Berggren et al. Nov 1986 A
4657019 Walsh et al. Apr 1987 A
4665906 Jervis May 1987 A
4721109 Healey Jan 1988 A
4747407 Liu et al. May 1988 A
4752024 Green et al. Jun 1988 A
4773420 Green Sep 1988 A
4861330 Voss Aug 1989 A
4875815 Phillips, II Oct 1989 A
4883453 Berry et al. Nov 1989 A
4892098 Sauer Jan 1990 A
4907591 Vasconcellos et al. Mar 1990 A
4917087 Walsh et al. Apr 1990 A
4917090 Berggren et al. Apr 1990 A
4917091 Berggren et al. Apr 1990 A
4930674 Barak Jun 1990 A
5005749 Aranyi Apr 1991 A
5015238 Solomon et al. May 1991 A
5062842 Tiffany Nov 1991 A
5089006 Stiles Feb 1992 A
5104025 Main et al. Apr 1992 A
5119983 Green et al. Jun 1992 A
5129913 Ruppert Jul 1992 A
5156613 Sawyer Oct 1992 A
5156619 Ehrenfeld Oct 1992 A
5171262 MacGregor Dec 1992 A
5178634 Ramos Martinez Jan 1993 A
5187796 Wang et al. Feb 1993 A
5192289 Jessen Mar 1993 A
5193731 Aranyi Mar 1993 A
5205459 Brinkerhoff et al. Apr 1993 A
5211683 Maginot May 1993 A
5217474 Zacca et al. Jun 1993 A
5221281 Klicek Jun 1993 A
5222963 Brinkerhoff et al. Jun 1993 A
5234447 Kaster et al. Aug 1993 A
5250058 Miller et al. Oct 1993 A
5250060 Carbo et al. Oct 1993 A
5271544 Fox et al. Dec 1993 A
5275322 Brinkerhoff et al. Jan 1994 A
5285945 Brinkerhoff et al. Feb 1994 A
5290298 Rebuffat et al. Mar 1994 A
5292053 Bilotti et al. Mar 1994 A
5304220 Maginot Apr 1994 A
5314435 Green et al. May 1994 A
5314468 Ramos Martinez May 1994 A
5326205 Anspach, Jr. et al. Jul 1994 A
5333773 Main et al. Aug 1994 A
5336233 Chen Aug 1994 A
5350104 Main et al. Sep 1994 A
5354302 Ko Oct 1994 A
5364389 Anderson Nov 1994 A
5366462 Kaster et al. Nov 1994 A
5392979 Green et al. Feb 1995 A
5395030 Kuramoto et al. Mar 1995 A
5395311 Andrews Mar 1995 A
5401131 Yoshino Mar 1995 A
5443497 Venbrux Aug 1995 A
5447514 Gerry et al. Sep 1995 A
5454825 Van Leeuwen Oct 1995 A
5456712 Maginot Oct 1995 A
5456714 Owen Oct 1995 A
5464449 Ryan et al. Nov 1995 A
5465895 Knodel et al. Nov 1995 A
5478354 Tovey et al. Dec 1995 A
5503635 Sauer et al. Apr 1996 A
5515478 Wang May 1996 A
5522834 Fonger et al. Jun 1996 A
5524180 Wang et al. Jun 1996 A
5533661 Main et al. Jul 1996 A
5540677 Sinofsky Jul 1996 A
5553198 Wang et al. Sep 1996 A
5556405 Lary Sep 1996 A
5558667 Yarborough et al. Sep 1996 A
5571167 Maginot Nov 1996 A
5643340 Nunokawa Jul 1997 A
5645520 Nakamura et al. Jul 1997 A
5657429 Wang et al. Aug 1997 A
5669918 Balazs et al. Sep 1997 A
5669934 Sawyer Sep 1997 A
5676670 Kim Oct 1997 A
5693088 Lazarus Dec 1997 A
5695504 Gifford, III et al. Dec 1997 A
5702412 Popov et al. Dec 1997 A
5707362 Yoon Jan 1998 A
5707380 Hinchliffe et al. Jan 1998 A
5709335 Heck Jan 1998 A
5709693 Taylor Jan 1998 A
5725544 Rygaard Mar 1998 A
5725553 Moenning Mar 1998 A
5732872 Bolduc et al. Mar 1998 A
5754741 Wang et al. May 1998 A
5755778 Kleshinski May 1998 A
5762458 Wang et al. Jun 1998 A
5779718 Green et al. Jul 1998 A
5792135 Madhani et al. Aug 1998 A
5797900 Madhani et al. Aug 1998 A
5797920 Kim Aug 1998 A
5799661 Boyd et al. Sep 1998 A
5799857 Robertson et al. Sep 1998 A
5807377 Madhani et al. Sep 1998 A
5814073 Bonutti Sep 1998 A
5815640 Wang et al. Sep 1998 A
5817113 Gifford, III et al. Oct 1998 A
5827316 Young et al. Oct 1998 A
5833698 Hinchliffe et al. Nov 1998 A
5841950 Wang et al. Nov 1998 A
5855583 Wang et al. Jan 1999 A
5868763 Spence et al. Feb 1999 A
5875782 Ferrari et al. Mar 1999 A
5878193 Wang et al. Mar 1999 A
5879371 Gardiner et al. Mar 1999 A
5881943 Heck et al. Mar 1999 A
5893369 LeMole Apr 1999 A
5904697 Gifford, III et al. May 1999 A
5907664 Wang et al. May 1999 A
5911036 Wright et al. Jun 1999 A
5915616 Viola et al. Jun 1999 A
5921995 Kleshinski Jul 1999 A
5944730 Nobles et al. Aug 1999 A
5947363 Bolduc et al. Sep 1999 A
5957363 Heck Sep 1999 A
5968089 Krajicek Oct 1999 A
5976159 Bolduc et al. Nov 1999 A
6001124 Bachinski Dec 1999 A
6007544 Kim Dec 1999 A
6013190 Berg et al. Jan 2000 A
6015416 Stefanchik et al. Jan 2000 A
6022367 Sherts Feb 2000 A
6024748 Manzo et al. Feb 2000 A
6030370 Kupka et al. Feb 2000 A
6030395 Nash et al. Feb 2000 A
6036699 Andreas et al. Mar 2000 A
6036700 Stefanchik et al. Mar 2000 A
6036702 Bachinkski et al. Mar 2000 A
6036703 Evans et al. Mar 2000 A
6036704 Yoon Mar 2000 A
6036705 Nash et al. Mar 2000 A
6050472 Shibata Apr 2000 A
6053390 Green et al. Apr 2000 A
6056762 Nash et al. May 2000 A
6066144 Wolf et al. May 2000 A
6066148 Rygaard May 2000 A
6068637 Popov et al. May 2000 A
6074416 Berg et al. Jun 2000 A
6080167 Lyell Jun 2000 A
6080173 Williamson, IV et al. Jun 2000 A
6083234 Nicholas et al. Jul 2000 A
6110188 Narciso, Jr. Aug 2000 A
6113612 Swanson et al. Sep 2000 A
6117148 Ravo et al. Sep 2000 A
6120432 Sullivan et al. Sep 2000 A
6146393 Wakabayashi Nov 2000 A
6149681 Houser et al. Nov 2000 A
6152937 Peterson et al. Nov 2000 A
6152945 Bachinski et al. Nov 2000 A
6165185 Shennib et al. Dec 2000 A
6167889 Benetti Jan 2001 B1
6171319 Nobles et al. Jan 2001 B1
6171321 Gifford, III et al. Jan 2001 B1
6176413 Heck et al. Jan 2001 B1
6176864 Chapman Jan 2001 B1
6186942 Sullivan et al. Feb 2001 B1
6187019 Stefanchik et al. Feb 2001 B1
6187020 Zegdi et al. Feb 2001 B1
6190396 Whitin et al. Feb 2001 B1
6190397 Spence et al. Feb 2001 B1
6190590 Randall et al. Feb 2001 B1
6193129 Bittner et al. Feb 2001 B1
6193734 Bolduc et al. Feb 2001 B1
6206912 Goldsteen et al. Mar 2001 B1
6206913 Yencho et al. Mar 2001 B1
Foreign Referenced Citations (87)
Number Date Country
29713335.7 Nov 1997 DE
19732234 Jan 1999 DE
0517252 Dec 1992 EP
0 701 800 Mar 1996 EP
0 885 595 Dec 1998 EP
0 938 870 Sep 1999 EP
0 820 724 Jan 2000 EP
0 820 725 Jan 2000 EP
0 913 125 Jul 2000 EP
0 990 420 Dec 2000 EP
2316910 Apr 1977 FR
9208513 May 1992 WO
96-25886 Aug 1996 WO
9725002 Jul 1997 WO
9727898 Aug 1997 WO
9731575 Sep 1997 WO
9747261 Dec 1997 WO
9807399 Feb 1998 WO
9819608 May 1998 WO
9819618 May 1998 WO
9819625 May 1998 WO
9819629 May 1998 WO
9819630 May 1998 WO
9819631 May 1998 WO
9819632 May 1998 WO
9819634 May 1998 WO
9819636 May 1998 WO
9830153 Jul 1998 WO
9837814 Sep 1998 WO
9840036 Sep 1998 WO
9842262 Oct 1998 WO
9847430 Oct 1998 WO
9855027 Dec 1998 WO
9908603 Feb 1999 WO
9911178 Mar 1999 WO
9917665 Apr 1999 WO
9918887 Apr 1999 WO
9921491 May 1999 WO
9937218 Jul 1999 WO
9938441 Aug 1999 WO
9938454 Aug 1999 WO
9940851 Aug 1999 WO
9940868 Aug 1999 WO
9945848 Sep 1999 WO
9952481 Oct 1999 WO
9962406 Dec 1999 WO
9962409 Dec 1999 WO
9962415 Dec 1999 WO
9963910 Dec 1999 WO
9965409 Dec 1999 WO
0009040 Feb 2000 WO
0010486 Mar 2000 WO
0012013 Mar 2000 WO
0015144 Mar 2000 WO
0015146 Mar 2000 WO
0015147 Mar 2000 WO
0015148 Mar 2000 WO
0015149 Mar 2000 WO
0027310 May 2000 WO
0027311 May 2000 WO
0027312 May 2000 WO
0027313 May 2000 WO
0033745 Jun 2000 WO
0041633 Jul 2000 WO
0053104 Sep 2000 WO
0056223 Sep 2000 WO
0056226 Sep 2000 WO
0056227 Sep 2000 WO
0056228 Sep 2000 WO
0059380 Oct 2000 WO
0066007 Nov 2000 WO
0066009 Nov 2000 WO
0069343 Nov 2000 WO
0069346 Nov 2000 WO
0069349 Nov 2000 WO
0069364 Nov 2000 WO
0072764 Dec 2000 WO
0074579 Dec 2000 WO
0076405 Dec 2000 WO
0108601 Feb 2001 WO
0112074 Feb 2001 WO
0115607 Mar 2001 WO
0117440 Mar 2001 WO
0119257 Mar 2001 WO
0119259 Mar 2001 WO
0119284 Mar 2001 WO
0134037 May 2001 WO