1. Field of the Invention
The invention relates to an implantable medical device such as an anastomosis device and a deployment system for implanting the device. In a preferred embodiment, the device can be used for forming a sutureless connection between a bypass graft and a blood vessel.
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. It would also be desirable to provide a sutureless anastomosis device which is formed of one piece and is secured to the target vessel in a single step.
According to a preferred embodiment, the present invention relates to an anastomosis device for connecting an end of a graft vessel to a target vessel wherein the device cooperates with a deployment tool for connecting an end of the graft vessel to the target vessel. The anastomosis device comprises a first linkage deformable by the deployment tool to form a first flange (e.g., an inner flange which connects the graft vessel to an inner surface of the target vessel), an optional connecting portion extending from the first linkage, and a second linkage deformable by the deployment tool to form a second flange (e.g., an outer flange which connects the graft vessel to an outer surface of the target vessel), the second linkage including deformable links which cooperate with a distal end of the deployment tool to form the second flange. The anastomosis device is preferably sized to fit through an incision in the target vessel such that the first flange comprises an inner flange which presses a portion of the graft vessel into intimate contact with an inner surface of the target vessel and the second flange comprises an outer flange which presses another portion of the graft vessel into intimate contact with an outer surface of the target vessel.
The anastomosis device can include various features. For instance, a connecting portion can be provided between the first and second linkages and the first and second linkages can include axial members having weakened areas which cause the axial members to bend simultaneously during formation of the inner and/or outer flange. The deployment tool can include an expander which forms the first flange and a holder tube surrounding the expander, the holder tube engaging the deformable links and bending the deformable links outwardly to form the second flange.
The deployment tool can incorporate various features. For example, a deforming crown tool can include first members and the deformable links can include second members which remain connected to the first members during formation of the first flange and disconnect from the first members during formation of the second flange, the deformable members bending the deformable links outwardly during formation of the second flange and returning to a non-bent configuration after formation of the second flange. The first members can comprise tabs and the second members can comprise slots which engage the tabs and openings which disengage the tabs, the slots extending from the openings towards a proximal end of the anastomosis device. A deforming crown deployment tool can include deformable members at the distal end thereof, the deformable members being plastically deformed after bending the deformable links outwardly to form the second flange. In a third embodiment, the deployment tool breaks off part of the anastomosis device during formation of the outer flange. For example, the anastomosis device can include a deployed portion (implant) and a severable portion (discard) wherein the first and second flanges are formed on the deployed portion and the severable portion is severed from the deployed portion when the second flange is formed. The deployed portion can be connected to the severable portion by shearable connectors and the shearable connectors can be located at pivot connections between the deployed portion and the severable portion. The severable portion and the deployed portion are preferably machined from a single piece of metal and the pivot connections can comprise thin sections of the metal extending between the deployed portion and the severable portion.
The anastomosis device can incorporate various structural features. For instance, the first linkage can include a plurality of struts arranged in a configuration such that an axial dimension of the first linkage changes upon radial expansion of the first linkage. Further, the first linkage can include a plurality of piercing members which penetrate the graft vessel. The second linkage can include a plurality of axial members and struts arranged in a configuration such that radial expansion of the second linkage does not cause formation of the second flange. The second linkage can also include pairs of axial members which are closer together at a distal end thereof than at a proximal end thereof, the proximal ends of the axial members being joined by circumferentially extending severable links to a linkage supported by the tool, the severable links being severed when the second flange is formed.
An anastomosis device deployment system according to the invention can include a handle and a holder tube attached to the handle, 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 tube and slidable with respect to the holder tube to a position at which the expander is positioned within the anastomosis device and radially expands the anastomosis device. The system can further include 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. The trocar can be a split trocar which is slidable over the holder tube and the expanded anastomosis device. The handle can include cam grooves which cooperate with followers of the holder tube and expander to move the holder tube and expander with respect to one another upon activation of a trigger of the handle. The distal end of the holder tube can include a plurality of slits, loops and/or flexible fingers for engaging tabs of the anastomosis device during formation of the inner and outer flanges.
According to another embodiment of the invention, the frangible linkage can be used to release an implant portion of a medical device at a target site in a living body. According to this embodiment, the medical device cooperates with a deployment tool for delivering and deploying the medical device to the site. The medical device includes first and second sections connected together by a frangible linkage, the frangible linkage being deformable by the deployment tool such that frangible elements of the frangible linkage are broken and the first section is separated from the second section. The frangible elements can include weakened areas which cause the frangible elements to bend when the frangible linkage is deformed by the deployment tool. For instance, the medical device can comprise an anastomosis device and the first section can include hinged axial members which bend outwardly and form first and second flanges. The deployment tool can include an expander which forms the first flange and a holder tube surrounding the expander, the holder tube engaging the second section and forming the second flange while separating the first section from the second section.
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:
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 or a small vessel anastomotic device is used for a target vessel which has a small diameter such as a coronary artery.
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.
The large vessel devices can be configured to connect to target vessels of various sizes having a wall thickness of at least about 0.5 mm, and typically about 0.5 mm to about 5 mm. In a preferred embodiment of the invention, the large vessel anastomotic device is configured to longitudinally collapse as the deformable section is radially expanded. The surgeon can control the longitudinal collapse to thereby position the distal end flange at a desired location at least partially within the incision in the target vessel wall. The surgeon can also control the position of the proximal end flange by longitudinally collapsing the device to a greater or lesser degree, to thereby position the proximal end flange at a desired location in contact with the target vessel. Thus, regardless of the thickness of the target vessel wall, the device can be longitudinally collapsed to position the flanges against the target vessel wall and effectively connect the device thereto. This feature is significant because the device must be connected to target vessels which have a wide range of wall thickness. For example, the aortic wall thickness is typically about 1.4 mm to about 4.0 mm and the aorta diameter can range from about 25 to about 65 mm in diameter. Therefore, regardless of the thickness of the target vessel wall, the degree of deployment of the proximal end flange, and thus the longitudinal collapse of the device, can be controlled by the physician to thereby effectively connect the device to the target vessel. For example, the surgeon may choose between partially deploying the proximal end flange so that it is positioned against an outer surface of the target vessel wall, or fully deploying the flange to position it in contact with the media of the target vessel wall within the incision in the target vessel wall.
In deploying a small vessel anastomotic device, the device can be used on small target vessels having a wall thickness of less than about 1.0 mm, and typically about 0.1 mm to about 1 mm in the case of coronary arteries. Despite the small size of the target vessels, the small vessel devices provide sutureless connection without significantly occluding the small inner lumen of the target vessel or impeding the blood flow therethrough. For example, the small vessel devices can include an outer flange (with the graft vessel connected thereto) loosely connected to an inner flange before insertion into the patient with the space between the loosely connected inner and outer flanges being at least as great as the wall thickness of the target vessel so that the inner flange can be inserted through an incision in the target vessel and into the target vessel lumen, with the outer flange outside the target vessel. With the outer and inner flanges in place on either side of a wall of the target vessel, tightening the flanges together compresses a surface of the graft vessel against the outer surface of the target vessel. This configuration forms a continuous channel between the graft vessel and the target vessel, without the need to suture the graft vessel to the target vessel wall and preferably without the use of hooks or barbs which puncture the target vessel.
In a coronary bypass operation in accordance with the invention, a large vessel device can be used to connect the proximal end of the graft vessel to the aorta, and a small vessel device can be used to connect the distal end of the graft vessel to an occluded coronary artery. 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 dissected mammary artery, or a synthetic prosthesis, as required.
Connection of the large vessel device does not require the stoppage of blood flow in the target vessel. Moreover, the anastomotic devices can be connected to the target vessel without the use of cardiopulmonary bypass. In contrast, 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. However, severely diseased aortas may not provide an area suitable for clamping due to significant calcification of the aortic wall. In the anastomosis technique according to the invention, the surgeon does not need significant room inside the patient to connect the anastomotic devices to the target vessel. For example, unlike sutured anastomoses which require significant access to the aorta for the surgeon to suture the graft vessel thereto, the anastomotic devices allow the proximal end of the graft vessel to be connected to any part of the aorta. All parts of the aorta are accessible to the large vessel anastomosis devices, even when minimally invasive procedures are used. Consequently, the graft vessel may be connected to the descending aorta, so that the graft vessel would not be threatened by damage during a conventional sternotomy if a second operation is required at a later time.
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 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 trocar and continues twisting to deploy the anastomotic device. The trocar penetrates the aortic wall at a high rate of speed to minimize any unintended deformation of the aorta and maintains a substantially fluid-tight seal at the puncture site. Having entered the aortic lumen, the trocar dilates as the anastomotic device and its holder tube (crown) are advanced through it, thus retracting the aortic tissue and serving as an introducer for the device. Once the device has fully entered the aortic lumen the trocar is withdrawn. 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 (mechanical stop) to seat the inner flange firmly 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 the device is disengaged from the instrument completing the anastomosis.
In use, a graft vessel 30 is inserted through a center of the tubular anastomosis device 10 and is everted over the first linkage 16 at the first end of the device. The first end of the device may puncture part way or all the way through the graft vessel wall to hold the graft vessel 30 on the device. An opening 34 is formed in the target vessel 32 to receive the graft vessel 30 and anastomosis device 10. Once the anastomosis device 10 with everted graft vessel 30 are inserted through the opening 34 in the target vessel 32, the inner and outer flanges 20, 22 are formed as shown in
The inner and outer flanges 20, 22 are formed by radial expansion of the anastomosis device 10 as follows. The first and second linkages 16, 18 are each made up of a plurality of axial members 12 and struts 14. The struts 14 are arranged in a plurality of diamond shapes with adjacent diamond shapes connected to each other to form a continuous ring of diamond shapes around the device. One axial member 12 extends through a center of each of the diamond shapes formed by the struts 14. A reduced thickness section 26 or hinge in each of the axial members 12 provides a location for concentration of bending of the axial members. When an expansion member of a deployment tool such as a rod or balloon is inserted into the tubular anastomosis device 10 and used to radially expand the device, each of the diamond shaped linkages of struts 14 are elongated in a circumferential direction causing a top and bottom of each of the diamond shapes to move closer together. As the top and bottom of the diamond shapes move closer together, the axial members 12 bend along the reduced thickness sections 26 folding the ends of the device outward to form the inner and outer flanges 20, 22 with the result that the wall of the target vessel 32 is trapped between the flanges and the everted graft vessel 30 is secured to the target vessel.
In the anastomosis device 10 shown in
As shown in
As shown in
One alternative embodiment of the holder tube 154 employs a plurality of flexible fingers which receive the pull tabs 130 of the anastomosis device 120. According to this embodiment each pull tab 130 is received by an independent finger of the holder tube 154. To deploy the second or outer flange of the anastomosis device 120, the flexible fingers flex outward bending the pull tabs 130 outward. For instance, the flexible fingers can be designed to flex when the pull tabs and fingers are put under axial compression in which case the fingers and tabs buckle outwards together to deploy the outer flange and release the anastomosis device from the holder tube.
The handle 160 is shown in
The handle 160 also includes a first channel 188 and a second channel 190 in the grip 170 through which the graft vessel (not shown) may be guided. The grip 170 also includes a cavity 192 for protecting an opposite end of the graft vessel from the attachment end.
According to one embodiment of the invention, the anastomosis device includes a frangible linkage which allows an implant to separate from the remainder of the device upon formation of the outer flange. According to a preferred linkage design, the frangible linkage can be radially expanded and axially compressed to fracture the frangible linkage. The inner flange can be formed during radial expansion of the device and the implant can be severed while forming the outer flange.
To facilitate easier bending of the struts 210 during radial expansion of the device, the distal ends of the struts can be curved at their points of attachment to the members 212. 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 212 move radially outward and circumferentially apart as the struts 210 move radially outward until a force on the barbs 208 by the struts 210 causes the struts to become bent at the narrow sections 214, after which the barbs extend outwardly to form the inner flange. In this deployed condition, the barbs 208 are locked into position by an X-shaped frame formed by struts 210 and additional struts 216. The struts 216 are similar in configuration to the struts 210 with respect to how they are shaped and attached to the members 212. Short axially extending members 218 connect the intersection of the struts 210 to the intersection of the struts 216.
The frangible section 202 is located at the proximal ends of axially extending members 220 which are connected to the members 212 by U-shaped links 222. The members 220 are arranged in pairs which are attached together at only their distal ends. In particular, the distal ends of the links 222 are attached to proximal ends of the members 212 and the midpoint of each link 222 is attached to the distal ends of a respective pair of members 220. As shown in
The frangible link shown in
The device 200 can be deployed using deployment tool 300 as follows. As shown in
In the embodiment shown in
In the foregoing embodiment, the device is deployed by radial expansion and axial compression. The axial compression can be accomplished by pushing the holder tube while the expander tube is held in a fixed position or vice versa According to a further embodiment, the axial compression can be accomplished by rotation of the device. For instance,
According to the next embodiment, the device can be designed so as to be released from the tool without use of fracture elements. For example, the tool can include a deforming crown which mechanically disengages with the device after forming the outer flange. The device and tool can incorporate any suitable release mechanism which, for example, connects the crown to the deployment tool when a tensile force is applied to the connection but which disconnects when a compressive force is applied to the connection, e.g., hooks, tabs, spring clips, etc.
During radial expansion of the device, axially extending barbs 408 are pivoted outwardly by struts 410 such that the outwardly extending barbs 408 and struts 410 form the inner flange. To facilitate bending of the barbs, the barbs 408 comprise points on the ends of axially extending members 412 which have narrow sections 414 located a desired distance from the free ends of the barbs 408. For instance, the narrow sections 414 can be located at axial positions along the device corresponding approximately to the axial midpoint of the struts 410 connecting adjacent members 412 when the device is in the pre-expanded condition.
To facilitate easier bending of the struts 410 during radial expansion of the device, the distal ends of the struts can be curved at their points of attachment to the members 412. 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 412 move radially outward and circumferentially apart as the struts 410 move radially outward until a force on the barbs 408 by the struts 410 causes the struts to become bent at the narrow sections 414, after which the barbs extend outwardly to form the inner flange. In this deployed condition, the barbs 408 are locked into position by an X-shaped frame formed by struts 410 and additional struts 416. The struts 416 are similar in configuration to the struts 410 with respect to how they are shaped and attached to the members 412. Short axially extending members 418 connect the intersection of the struts 410 to the intersection of the struts 416.
The frangible section 402 is located at the proximal ends of axially extending members 420 which are connected to the members 412 by U-shaped links 422. The members 420 are arranged in pairs which are attached together at midpoints of links 422. During radial expansion of the device, the individual links 422 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 422 form the annular ring and the distal ends of the pairs of members 420 attached to an individual link 422 move radially outward but not apart in the circumferential direction. At the same time, the proximal ends of the members 420 move radially outward and circumferentially apart.
The frangible section 402 is located between axial members 420 and axially extending members 424. As shown in
The device 400 can be deployed in the same manner that the device 200 is deployed using deployment tool 300. That is, the device 400 includes a crown attached to a distal end of the deployment tool. The crown includes axially extending members 442 with tabs 443 on the proximal ends thereof, the members 442 being held in slots 304 of the tool 300 by the tabs 443. A plastic sleeve (not shown) can be placed over the slots 304 to prevent the members 442 from coming out of the slots. When mounted on the deployment tool, the crown is flared outwardly such that the members 442 are fully radially expanded at their proximal ends. During radial expansion of the device 400, the diamond shaped linkage of the crown 440 is expanded from an unexpanded condition like the configuration shown in
During radial expansion of the device, axially extending barbs 508 are pivoted outwardly by struts 510 such that the outwardly extending barbs 508 and struts 510 form the inner flange. To facilitate bending of the barbs, the barbs 508 comprise points on the ends of axially extending members 512 which have narrow sections 514 located a desired distance from the free ends of the barbs 508. For instance, the narrow sections 514 can be located at axial positions along the device corresponding approximately to the axial midpoint of the struts 510 connecting adjacent members 512 when the device is in the pre-expanded condition.
To facilitate easier bending of the struts 510 during radial expansion of the device, the distal ends of the struts can be curved at their points of attachment to the members 512. 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 512 move radially outward and circumferentially apart as the struts 510 move radially outward until a force on the barbs 508 by the struts 510 causes the struts to become bent at the narrow sections 514, after which the barbs extend outwardly to form the inner flange. In this deployed condition, the barbs 508 are locked into position by an X-shaped frame formed by struts 510 and additional struts 516. The struts 516 are similar in configuration to the struts 510 with respect to how they are shaped and attached to the members 512. Short axially extending members 518 connect the intersection of the struts 510 to the intersection of the struts 516.
The frangible section 502 is located at the proximal ends of axially extending members 520 which are connected to the members 512 by U-shaped links 522. The members 520 are arranged in pairs which are attached together at only their distal ends. In particular, the distal ends of the links 522 are attached to proximal ends of the members 512 and the midpoint of each link 522 is attached to the distal ends of a respective pair of members 520. During radial expansion of the device, the individual links 522 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 522 form the annular ring and the distal ends of the members 520 move radially outward but not apart in the circumferential direction. At the same time, the proximal ends of the members 520 move radially outward and circumferentially apart.
The frangible section 502 is located between pairs of the axial members 520 and pairs of axially extending members 524. As shown in
The device 500 can be deployed in the same manner that the device 200 is deployed using deployment tool 300. That is, the device 500 includes a crown attached to a distal end of the deployment tool. The crown includes axially extending members 542 with tabs 543 on the proximal ends thereof, the members 542 being held in slots 304 of the tool 300 by the tabs 543. A plastic sleeve (not shown) can be placed over the slots 304 to prevent the members 542 from coming out of the slots. When mounted on the deployment tool, the crown is flared outwardly such that the members 542 are fully radially expanded at their proximal ends. During radial expansion of the device 500, the diamond shaped linkage of the crown 540 is expanded from an unexpanded condition like the configuration shown in
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 pre-expanded 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
The device 600 can be deployed in the same manner that the device 200 is deployed using deployment tool 300. That is, 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 304 of the tool 300 by the tabs 643. A plastic sleeve (not shown) can be placed over the slots 304 to prevent the members 642 from coming out of the slots. When mounted on the deployment tool, 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
During radial expansion of the device, axially extending barbs 708 are pivoted outwardly by struts 710 such that the outwardly extending barbs 708 and struts 710 form the inner flange. To facilitate bending of the barbs, the barbs 708 comprise points on the ends of axially extending members 712 which have narrow sections 714 located a desired distance from the free ends of the barbs 708. For instance, the narrow sections 714 can be located at axial positions along the device corresponding approximately to the axial midpoint of the struts 710 connecting adjacent members 712 when the device is in the pre-expanded condition.
To facilitate easier bending of the struts 710 during radial expansion of the device, the distal ends of the struts can be curved at their points of attachment to the members 712. 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 712 move radially outward and circumferentially apart as the struts 710 move radially outward until a force on the barbs 708 by the struts 710 causes the struts to become bent at the narrow sections 714, after which the barbs extend outwardly to form the inner flange. In this deployed condition, the barbs 708 are locked into position by an X-shaped frame formed by struts 710 and additional struts 716. The struts 716 are similar in configuration to the struts 710 with respect to how they are shaped and attached to the members 712. Short axially extending members 718 connect the intersection of the struts 710 to the intersection of the struts 716.
The frangible section 702 is located at the proximal ends of axially extending members 720 which are connected to the members 712 by U-shaped links 722 and U-shaped links 723. The members 720 are arranged in pairs which are attached at their distal ends to proximal ends of the links 723 and the midpoints of the links 723 are attached to midpoints of the links 722. The ends of the links 722 are attached to the proximal ends of adjacent members 718. During radial expansion of the device, the individual links 722, 723 are plastically deformed from their U-shaped configuration to form segments of two circumferentially extending annular rings. As a result, the device becomes shorter in the axial direction as links 722, 723 form the annular rings and the distal ends of each pair of the members 720 attached to an individual link 723 move radially outward but not apart in the circumferential direction. At the same time, the proximal ends of pairs of the members 720 move radially outward and circumferentially apart.
The frangible section 702 is located between pairs of the axial members 720 and pairs of axially extending members 724. As shown in
The device 700 can be deployed in the same manner that the device 200 is deployed using deployment tool 300. That is, the device 700 includes a crown attached to a distal end of the deployment tool. The crown includes axially extending members 742 with tabs 743 on the proximal ends thereof, the members 742 being held in slots 304 of the tool 300 by the tabs 743. A plastic sleeve (not shown) can be placed over the slots 304 to prevent the members 742 from coming out of the slots. When mounted on the deployment tool, the crown is flared outwardly such that the members 742 are fully radially expanded at their proximal ends. During radial expansion of the device 700, the diamond shaped linkage of the crown 740 is expanded from an unexpanded condition like the configuration shown in
A preferred method of loading an expander 156 in a holder tube 154 and placing a graft vessel over the anastomosis device is explained with reference to
In order to deploy the device 820, the inner flange can be expanded by pushing the expander 156 a set distance while maintaining the holder tube 154 in a fixed position. As a result, the linkage of the inner flange rotates the barbed ends 824 about the hinged connections 828 such that the barbed ends 824 from an angle of 40 to 140° with the central axis. Then, the holder tube 154 is pushed a set distance while holding the expander 156 in a fixed position to deploy the outer flange. As a result, the linkage of the outer flange and the discard portion of the anastomosis device is axially compressed such that the linkage fractures as the outer flange is rotated outwardly and towards the already deployed inner flange.
Each of the anastomosis devices described above are preferably single 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 such as arteries, veins, bile ducts, etc., of different sizes. Although various linkage arrangements have been shown wherein the devices include struts which extend between two circumferentially spaced apart locations and axial members which extend between two axially spaced apart locations, the linkages which form the flanges could also be formed by V-shaped links arranged in diamond like patterns. For example,
The mesh 830 can be joined to another mesh with the same or different linkage arrangement with or without a connecting linkage therebetween. If the same linkage arrangement is used, in order to obtain deployment of one flange prior to deployment of the other flange, one of the linkages can be made with wider and/or thicker links. For example, by using a distal linkage of thin links and a proximal linkage of thick links, it is possible to deploy the inner flange prior to deployment of the outer flange. In other words, axial compression of the tubular mesh can cause the weaker distal linkage to deploy first and form the inner flange after which the outer flange can be formed by axial compression of the stronger proximal linkage.
Although the invention has been principally discussed with respect to coronary bypass surgery, the anastomosis devices of the present invention may be used in other types of anastomosis procedures. For example, the anastomosis device may be used in femoral-femoral bypass, vascular shunts, subclavian-carotid bypass, organ transplants, and the like.
The anastomosis devices may be made of any known material which can be bent and will retain the bent shape such as stainless steel, nickel titanium alloys, and the like. The hinges or pivot joints which have been discussed above in the various embodiments of the present invention may be designed to concentrate the bending at a desired location.
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.
This is a continuation of application Ser. No. 10/003,406, filed Dec. 6, 2001, now U.S. Pat. No. 6,537,288.
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 |
3995619 | Glatzer | Dec 1976 | A |
4018228 | Goosen | Apr 1977 | 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 |
4625727 | Leiboff | Dec 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 |
4929240 | Kirsch et al. | May 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 |
5100423 | Fearnot | Mar 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 |
5221259 | Weldon 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 |
5403338 | Milo | Apr 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 |
5470320 | Tiefenbrun et al. | Nov 1995 | A |
5478353 | Yoon | Dec 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 |
5603721 | Lau et al. | Feb 1997 | A |
5643340 | Nunokawa | Jul 1997 | A |
5645520 | Nakamura et al. | Jul 1997 | A |
5657429 | Wang et al. | Aug 1997 | A |
5667513 | Torrie et al. | Sep 1997 | A |
5667520 | Bonutti | Sep 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 | Hinchcliffe 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 | Hinchcliffe et al. | Nov 1998 | A |
5841950 | Wang et al. | Nov 1998 | A |
5855583 | Wang et al. | Jan 1999 | A |
5868761 | Nicholas et al. | Feb 1999 | A |
5868763 | Spence et al. | Feb 1999 | A |
5871495 | Mueller | 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 |
5910153 | Mayenberger | Jun 1999 | A |
5911036 | Wright et al. | Jun 1999 | A |
5915616 | Viola et al. | Jun 1999 | A |
5921995 | Kleshinski | Jul 1999 | A |
5931842 | Goldsteen et al. | Aug 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 |
5972014 | Nevins | Oct 1999 | A |
5976159 | Bolduc et al. | Nov 1999 | A |
5976178 | Goldsteen et al. | Nov 1999 | A |
5989278 | Mueller | 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 | Bachinski 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 |
6132439 | Kontos | Oct 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 |
6235054 | Berg et al. | May 2001 | B1 |
6302905 | Goldsteen et al. | Oct 2001 | B1 |
6309416 | Swanson et al. | Oct 2001 | B1 |
6371964 | Vargas et al. | Apr 2002 | B1 |
6391036 | Berg et al. | May 2002 | B1 |
6402764 | Hendricksen et al. | Jun 2002 | B1 |
6428550 | Vargas et al. | Aug 2002 | B1 |
6461320 | Yencho et al. | Oct 2002 | B1 |
6485496 | Suyker et al. | Nov 2002 | B1 |
6524322 | Berreklouw | Feb 2003 | B1 |
6605098 | Nobis et al. | Aug 2003 | B1 |
6695859 | Golden et al. | Feb 2004 | B1 |
20010047180 | Grudem et al. | Nov 2001 | A1 |
20020058955 | Blatter et al. | May 2002 | A1 |
20020082614 | Logan et al. | Jun 2002 | A1 |
20030065342 | Nobis | Apr 2003 | A1 |
Number | Date | Country |
---|---|---|
29713335 | Nov 1997 | DE |
19732234 | Jan 1999 | DE |
0 701 800 | Mar 1996 | EP |
0 517 252 | Dec 1996 | EP |
0 885 595 | Dec 1998 | EP |
0 820 724 | Jan 2000 | EP |
0 820 725 | Jan 2000 | EP |
0 913 125 | Jul 2000 | EP |
0 938 870 | Sep 2000 | EP |
0 990 420 | Dec 2000 | EP |
2316910 | Jul 1976 | FR |
9840036 | Sep 1988 | WO |
9208513 | May 1992 | WO |
9625886 | 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 |
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 |
Number | Date | Country | |
---|---|---|---|
20030109893 A1 | Jun 2003 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 10003406 | Dec 2001 | US |
Child | 10273910 | US |