Systems and methods for attaching a prosthesis with a body lumen or hollow organ

Abstract
Systems and methods introduce and deploy prosthesis into a blood vessel or hollow body organ by intra-vascular access. The prosthesis is secured in place by fasteners which are implanted by an applier that is also deployed by intra-vascular access. The applier is configured to permit controlled, selective release of the fastener in a step that is independent of the step of implantation.
Description
FIELD OF THE INVENTION

The invention relates generally to prostheses, and in particular, the attachment of prostheses used in the repair of diseased and/or damaged sections of a hollow body organ and/or a blood vessel.


BACKGROUND OF THE INVENTION

The weakening of a vessel wall from damage or disease can lead to vessel dilatation and the formation of an aneurysm. Left untreated, an aneurysm can grow in size and may eventually rupture.


For example, aneurysms of the aorta primarily occur in abdominal region, usually in the infrarenal area between the renal arteries and the aortic bifurcation. Aneurysms can also occur in the thoracic region between the aortic arch and renal arteries. The rupture of an aortic aneurysm results in massive hemorrhaging and has a high rate of mortality.


Open surgical replacement of a diseased or damaged section of vessel can eliminate the risk of vessel rupture. In this procedure, the diseased or damaged section of vessel is removed and a prosthetic graft, made either in a straight of bifurcated configuration, is installed and then permanently attached and sealed to the ends of the native vessel by suture. The prosthetic grafts for these procedures are usually unsupported woven tubes and are typically made from polyester, ePTFE or other suitable materials. The grafts are longitudinally unsupported so they can accommodate changes in the morphology of the aneurysm and native vessel. However, these procedures require a large surgical incision and have a high rate of morbidity and mortality. In addition, many patients are unsuitable for this type of major surgery due to other co-morbidities.


Endovascular aneurysm repair has been introduced to overcome the problems associated with open surgical repair. The aneurysm is bridged with a vascular prosthesis, which is placed intraluminally. Typically these prosthetic grafts for aortic aneurysms are delivered collapsed on a catheter through the femoral artery. These grafts are usually designed with a fabric material attached to a metallic scaffolding (stent) structure, which expands or is expanded to contact the internal diameter of the vessel. Unlike open surgical aneurysm repair, intraluminally deployed grafts are not sutured to the native vessel, but rely on either barbs extending from the stent, which penetrate into the native vessel during deployment, or the radial expansion force of the stent itself is utilized to hold the graft in position. These graft attachment means do not provide the same level of attachment when compared to suture and can damage the native vessel upon deployment.


SUMMARY OF THE INVENTION

The invention provides apparatus, tools, systems, and methods for repairing diseased and/or damaged sections of a hollow body organ and/or a blood vessel. The apparatus, tools, systems, and methods find use, e.g., in the introduction and deployment of a prosthesis into a blood vessel or hollow body organ, which desirably is achieved by intra-vascular access. The prosthesis is secured in place by fasteners, which are implanted by the apparatus, tools, systems, and methods that embody one or more features of the invention, which are also desirably deployed by intra-vascular access.


According to one aspect of the invention, the applier is configured to permit controlled, selective release of the fastener in a step that is independent of the step of implantation. According to one embodiment of this aspect of the invention, the applier includes a driven member that is carried on a tool body. The tool body can include, e.g., a tube, such as a catheter, to permit intra-vascular deployment of the driven member. The driven member is operable to apply an implantation force to the fastener. A drive actuator operates the driven member. The applier also includes a fastener-engaging mechanism on the driven member. The mechanism is operable in a first condition to couple the fastener to the driven member to transfer the implantation force from the driven member to the fastener. Implantation of the fastener can thereby be achieved. The mechanism is also operable in a second condition to release the fastener from the driven member. According to this aspect of the invention, the mechanism includes a second actuator, which places the mechanism in the second condition, to release the fastener. The second actuator is operable independent of the drive actuator. There can thus be a definite, stepwise separation between implanting the fastener in tissue using the implantation tool and releasing the fastener from the implantation tool after implantation is satisfactorily achieved.


Another aspect of the invention provides a tool that can be used to apply an implantation force to a fastener, which is sized and configured for implantation in tissue in response to an implantation force applied according to prescribed conditions. The tool is coupled to a controller, which interrupts implantation before it is completed, and interjects a “go”/“no go” decision-making step before proceeding further. The tool includes a driven member carried on a tool body. The tool body can comprise, e.g., a tube, such as a catheter. The driven member is operable to apply the implantation force. A mechanism on the driven member couples the fastener to the driven member to transfer the implantation force from the driven member to the fastener. According to this aspect of the invention, a controller is coupled to the driven member. The controller executes differing operational phases during the implantation process. During an initial phase the driven member is operated to apply the implantation force under conditions that do not achieve the prescribed conditions, so that only partial implantation of the fastener occurs. A lull phase commences at the end of the initial phase. The lull phase interrupts operation of the driven member. There is a final phase, which operates the driven member under conditions that supplement the conditions of the initial phase to achieve the prescribed conditions, and thus achieve complete implantation. However, the controller requires, after the initial phase, a prescribed command to advance from the lull phase to the final phase. The lull phase requires a decision be made before implantation of the fastener is finalized. If implantation during the initial phase is deemed not to be satisfactory, implantation can be aborted, and the fastener (now only partially implanted) can be withdrawn. The decision can comprise a conscious decision by the operator and/or a decision based, at least in part, upon physuical or operational conditions sensed during the initial phase.


Another aspect of the invention provides a tool for applying an implantation force to a fastener that is sized and configured for implantation in tissue in response to an implantation force. The tool comprises a driven member carried on a tool body that is operable to apply the implantation force. According to this aspect of the invention, an element is included that tethers the fastener to the tool body. The tethering element safeguards against inadvertent loss of the fastener prior to implantation. The tethering element includes a frangible portion, so that, once the fastener is satisfactorily implanted, the tethering element can be parted from the fastener and the tool body removed.


The invention also provides various systems and methods for using the above-described devices to implant tissue in a vessel or hollow body organ.


Other features and advantages of the invention shall be apparent based upon the accompanying description, drawings, and claims.





BRIEF DESCRIPTION OF THE DRAWINGS

The invention will be understood from the following detailed description of preferred embodiments, taken in conjunction with the accompanying drawings, wherein:



FIG. 1 is a perspective view of a prosthesis having a fastening region that accommodates the introduction of one or more fasteners.



FIG. 2 is a perspective view of the prosthesis shown in FIG. 1, showing the attachment of fasteners in the fastening region.



FIG. 3 is a perspective view of the prosthesis shown in FIG. 1 positioned within an abdominal aortic aneurysm.



FIG. 4 is a perspective view of the prosthesis shown in FIG. 3 as it is being deployed by an intra-vascular catheter.



FIG. 5 is a perspective view of the prosthesis shown in FIG. 3 after it been deployed and as fasteners are being implanted by an intra-vascular fastener applier.



FIG. 6. is a side view, partly broken away and in section, of an intra-vascular fastener applier that can be used to implant fasteners in the prosthesis shown in FIGS. 1 and 2, in the manner shown in FIG. 5.



FIG. 7 is a perspective view of a type of helical fastener that can be implanted using the intra-vascular fastener applier shown in FIG. 6.


FIG. 8A(1) is an enlarged view of a carrier for implanting a fastener of the type shown in FIG. 7, the carrier being located at the distal end of an intra-vascular fastener applier of the type shown in FIG. 8A(2), the carrier being shown in a condition to receive a fastener prior to implantation.


FIG. 8A(2) is a side view, partly broken away and in section, of a fastener applier that includes, at its distal end, a carrier as shown in FIG. 8A(1), the carrier being shown after receipt of a fastener and as the carrier is being rotated to implant the fastener in a prosthesis/tissue wall.


FIG. 8B(1) is an enlarged view of the carrier shown in FIG. 8A(1), the carrier being shown in a condition to release a fastener after implantation.


FIG. 8B(2) is a side view, partly broken away and in section, of the fastener applier that includes, at its distal end, the carrier shown in FIG. 8B(1), the carrier being shown releasing a fastener following its implantation in a prosthesis/tissue wall.



FIG. 8C is a side view, partly broken away and in section, of the fastener applier shown in FIG. 8A(2), the carrier being shown withdrawing or retrieving a fastener from a prosthesis/tissue wall.


FIG. 9A(1) is an enlarged view of another embodiment of a carrier for implanting a fastener of the type shown in FIG. 7, the carrier being located at the distal end of an intra-vascular fastener applier of the type shown in FIG. 9A(2), the carrier being shown in a condition to receive a fastener prior to implantation.


FIG. 9A(2) is a side view, partly broken away and in section, of a fastener applier that includes, at its distal end, a carrier as shown in FIG. 9A(1), the carrier being shown after receipt of a fastener and as the carrier is being rotated to implant the fastener in a prosthesis/tissue wall.


FIG. 9B(1) is an enlarged view of the carrier shown in FIG. 9A(1), the carrier being shown in a condition to release a fastener after implantation.


FIG. 9B(2) is a side view, partly broken away and in section, of the fastener applier that includes, at its distal end, the carrier shown in FIG. 9B(1), the carrier being shown releasing a fastener following its implantation in a prosthesis/tissue wall.


FIG. 10A(1) is an enlarged view of a carrier for implanting a fastener of the type shown in FIG. 7, the carrier being located at the distal end of an intra-vascular fastener applier of the type shown in FIG. 10A(2), the carrier being shown in a condition to receive a fastener prior to implantation.


FIG. 10A(2) is a side view, partly broken away and in section, of a fastener applier that includes, at its distal end, a carrier as shown in FIG. 10A(1), the carrier being shown after receipt of a fastener and as the carrier is being rotated to implant the fastener in a prosthesis/tissue wall.


FIG. 10B(1) is an enlarged view of the carrier shown in FIG. 10A(1), the carrier being shown in a condition to release a fastener after implantation.


FIG. 10B(2) is a side view, partly broken away and in section, of the fastener applier that includes, at its distal end, the carrier shown in FIG. 10B(1), the carrier being shown releasing a fastener following its implantation in a prosthesis/tissue wall.



FIG. 11 is an enlarged view of a carrier for implanting a fastener of the type shown in FIG. 7, the carrier being located at the distal end of an intra-vascular fastener applier of the type shown in FIGS. 10A(2) and 10B(2), the carrier being shown in a condition to receive a fastener prior to implantation.



FIGS. 12A and 12B are perspective views of a fastener assembly comprising a helical fastener and a cap, FIG. 12A showing an exploded view of the assembly and FIG. 12B showing an assembled view of the assembly.



FIGS. 13A and 13B are side views showing in interior of a carrier for implanting a fastener assembly of the type shown in FIG. 12B, the carrier being located at the distal end of an intra-vascular fastener applier of the type shown in FIG. 15A, the carrier in FIG. 13A being shown in a condition to receive the fastener assembly prior to implantation, the carrier in FIG. 13B being shown in a condition to release the fastener assembly after implantation.



FIGS. 14A and 14B are side views showing the mounting of the fastener assembly shown in FIG. 12B to the carrier shown in FIG. 13A.



FIG. 15A is a side view, partly broken away and in section, of a fastener applier that includes, at its distal end, a carrier as shown in FIG. 13A, the carrier being shown after receipt of a fastener assembly as shown in FIG. 14B and as the carrier is being rotated to implant the fastener assembly in a prosthesis/tissue wall.



FIG. 15B is a side view, partly broken away and in section, of a fastener applier shown in FIG. 15A, the carrier being shown releasing the fastener assembly after its implantation in a prosthesis/tissue wall.



FIG. 15C is a side view, partly broken away and in section, of a fastener applier shown in FIG. 15A, the carrier being shown withdrawing or retrieving the fastener assembly from a prosthesis/tissue wall.


FIG. 16A(1) is an enlarged view of a carrier for implanting a fastener of the type shown in FIG. 7, the carrier being located at the distal end of an intra-vascular fastener applier of the type shown in FIG. 16A(2), the carrier being shown holding a fastener prior to implantation.


FIG. 16A(2) is a side view, partly broken away and in section, of a fastener applier that includes, at its distal end, a carrier as shown in FIG. 16A(1), the carrier being rotated to implant the fastener in a prosthesis/tissue wall.



FIG. 16B is a side view, partly broken away and in section, of the fastener applier shown in FIG. 16A(2), the carrier being shown at the end of a first operating phase, during which the fastener has been partially implanted in a prosthesis/tissue wall and in which the fastener remains secured to the carrier.



FIG. 16C is a side view, partly broken away and in section, of the fastener applier shown in FIG. 16A(2), the carrier being shown following the first operating phase and at the end of a second operating phase, during which the fastener has been fully implanted and released from the carrier into a prosthesis/tissue wall.



FIG. 16D is a side view, partly broken away and in section, of the fastener applier shown in FIG. 16A(2), the carrier being shown following the first operating phase and during another operating phase, during which the fastener is being withdrawn or retrieved from a prosthesis/tissue wall while still secured to the carrier.



FIGS. 17A and 17B are side views of a fastener applier of the type shown in any of the preceding Figures, the fastener applier including an element releasably tethering a fastener to the fastener applier, FIG. 17A showing the tethering element holding on to the fastener following its implantation in a prosthesis/tissue wall, and FIG. 17B showing the tethering element after having been parted from the fastener.



FIGS. 18A and 18B show an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secure to a frangible portion of the fastener, FIG. 18A showing the tethering element holding on to the fastener following its implantation in a prosthesis/tissue wall, and FIG. 18B showing the tethering element after having been parted from the fastener.



FIG. 19A shows an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured to a frangible joint that is broken by rotating the tethering element relative to the fastener.



FIG. 19B shows an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured to a frangible joint that is broken by pulling the tethering element from the fastener.



FIGS. 20A and 20B show an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured to a screw joint (FIG. 20A) that is parted by rotating the tethering element relative to the fastener (FIG. 20B).



FIGS. 21A and 21B show an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured to a ball joint (FIG. 21A) that is parted by pulling the tethering element away from the fastener (FIG. 21B).



FIGS. 22A and 22B show an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured to a slip joint (FIG. 22A) that is parted by pulling the tethering element away from the fastener (FIG. 22B).



FIGS. 23A and 23B show an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured to a knotted joint (FIG. 23A) that is parted by pulling the tethering element away from the fastener (FIG. 23B).



FIGS. 24A and 24B show an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured to a frangible tube joint (FIG. 24A) that is parted by pulling a rip cord (FIG. 24B).



FIGS. 25A and 25B show an embodiment of a tethering element of the type shown in FIGS. 17A and 17B, the tethering element being secured by an interlocking joint (FIG. 25A) that is released by pulling away a slidable sleeve (FIG. 25B).





DETAILED DESCRIPTION OF THE INVENTION

I. Prosthesis


A. Structure



FIG. 1 shows a prosthesis 10. The prosthesis 10 serves to repair or reinforce a region of a vessel wall or hollow body organ which has been weakened by disease or damage.


In the illustrated embodiment (see FIG. 1), the prosthesis 10 comprises a tubular trunk 12. The trunk 12 is sized and configured to fit within a targeted region of a hollow body organ and/or a blood vessel. The targeted region is selected on the basis of certain anatomic characteristics. These characteristics include a weakened conditioned caused, e.g., by disease or damage.


The trunk 12 forms a generally cylindrical structure with an open interior lumen 18. In the illustrated embodiment, the trunk 12 includes a prosthetic material 14 supported by a scaffold 16. The prosthetic material 14 is selected on the basis of its biocompatibility, durability, and flexible mechanical properties. The material 14 can comprise, e.g., woven polyester or ePTFE.


The scaffold 16 is desirable sized and configured to permit non-invasive deployment of the prosthesis 10 by an intra-vascular catheter. With this criteria in mind, the scaffold 16 is sized and configured to assume a compressed or collapsed, low profile condition, to permit its intra-vascular introduction into the hollow body organ and/or blood vessel by a catheter, as will be described in greater detail later.


Also with this criteria in mind, the scaffold 16 is sized and configured for expansion in situ from its collapsed condition into an expanded condition in contact with tissue in the targeted region, as will also be described in greater detail later.


In this respect, the scaffold 16 can comprise, e.g., a malleable plastic or metal material that expands in the presence of an applied force. In this arrangement, the deployment catheter can include, e.g., an expandable body, such as a balloon, to apply the expansion force to the scaffold 16 in situ.


Alternatively, the scaffold 16 can comprise a self-expanding plastic or metal material that can be compressed in the presence of a force, but self-expands upon removal of the compressive force. In this arrangement, the deployment catheter can include, e.g., a sleeve that can be manipulated to enclosed the scaffold 16 in a collapsed condition, thereby applying the compressive force, and to release the scaffold 16 when desired to allow the scaffold 16 to self-expand in situ.


For self-expansion, the scaffold 16 can include individual self-expanding, zigzag type main scent rings 22. The main stent rings 22 can be made, e.g., from Nitinol® wire. Still, other materials, manufacturing methods and designs can be used.


The main stent rings 22 need not be attached to one another throughout the prosthesis material 14, as FIG. 1 shows. The individual main stent rings 22 allow for longitudinal compliance while maintaining radial support of the open interior lumen 18. This technical feature allows the prosthesis 10 to more readily accommodate changes in morphology in the targeted region. Still, it may be desirable in certain locations within the prosthesis structure to have attachments between the individual main stent rings 22 to provide enhanced stability and/or additional radial support.


Each of the main stent rings 22 can be, e.g., sewn onto prosthetic material 14. In the illustrated embodiment, in which the prosthetic material 14 is woven polyester, the attachment of the main scent rings 22 can be made, e.g., with polyester suture.


However, it is also contemplated that other attachment means could be utilized to secure the main stent rings 22 to the prosthetic material 14. These means include bonding; capturing the main stent rings 22 between two layers of prosthetic material 14; and incorporating the main stent rings 22 directly into the prosthetic material 14.


In certain locations it is desired to have the main stent rings 22 attached to the outer diameter of the prosthetic material 14. Still, it is also contemplated that the main stent rings 22 could be attached to the inner diameter of the prosthetic material 22.


At least, one end of the trunk 12 desirably also includes one or more end stent rings 24. The principal purpose of an end stent ring 24 is to provide a seal between the trunk 12 and adjoining tissue. This sealing function is particularly desirable when the prosthesis 10 is deployed in a blood vessel or other body organ, where body fluids are intended to reside or pass through the prosthesis 10. The end sent rings 24 can also serve, with the main stent rings 22, to help maintain the position of the prosthesis 10 in the targeted region.


The trunk 12 (material 14 and/or scaffold 16) can carry radiopaque markers 46 to help fluoroscopically position the prosthesis 10. The markers 46 can take the form, e.g. of marker bands, tight wound coils, or wire made from radiopaque materials such as platinum, platinum/iridium, or gold.


The trunk 12 also desirably includes at least one fastening region 26 that accommodates the introduction of one or more fasteners 28 to anchor the prosthesis 10 in place (see FIG. 2). It is desirable that this region 26 of the trunk 12 be specially sized and configured for the receipt and retention of fasteners 28. For example, the size and spacing of ring stent patterns can be configured in the region 26 to specially accommodate the placement of fasteners; and/or woven fibers with an “X-pattern” or a “sinusoidal pattern” can be used in the region 26 to specially accommodate placement of fasteners; and/or the prosthetic material 14 can be folded-over to form multiple layers, to reinforce the prosthesis in the region 26 where fasteners are placed; and/or denser weave patterns or stronger fibers can be used, selected from, e.g., Kevlar™ material or Vectran™ material or metallic wire woven alone or interwoven with typical polyester fibers in the region 26 were fasteners are placed. It may also be desirable to fluoroscopically indicate this region 26 with auxiliary radiopaque markers 30 on the prosthetic material 14, and/or auxiliary stent rings 32 to aid in positioning the fasteners.


The fasteners 28 can be variously constructed. They can, e.g., comprise helical fasteners or staples.


Desirably, like the prosthesis 10 itself, the fasteners 28 are introduced by an intra-vascular fastener attachment assembly. Details of various fastener attachment assemblies will be described in greater detail later.


B. Use of the Prosthesis


The targeted region for deployment of the tissue reinforcement prosthesis 10 as just described can vary. In FIG. 3, the trunk 12 is sized and configured to extend, for purposes of illustration, in the aorta adjacent the renal arteries distally to a location proximal the natural bifurcation of the iliac arteries. However, this targeted site of deployment is selected for purposes of illustrating the features of the prosthesis 10, and it is not intended to be limiting.


As shown in FIG. 3, the fastening region 26 is located in the neck of the aorta adjacent to the renal arteries. The features of the fastening region 26, previously described, make possible the secure attachment of the prosthesis 10, without migration.


In this arrangement (see FIG. 3), the trunk 12 may include a supra-renal stent 44 at its proximal end, which extends beyond the prosthetic material 14. When deployed within the aorta, this stent 44 would extend above the level of the renal arteries, as FIG. 3 shows. The supra-renal stent 44 orients the prosthesis 10 within the lumen and aids in maintaining the position of the prosthesis 10 in the aorta without obstructing the normal blood flow into the renal arteries.


During use (see FIGS. 4 and 5), a first catheter 20 is navigated over a guide wire 48 through an iliac to the desired location within the aorta near the renal arteries. The catheter 20 carries the prosthesis 10 in a radially reduced configuration. At the targeted site, the catheter 20 releases the prosthesis 10, which expands radially into the position shown in FIG. 5.


A fastener assembly 34 is next deployed (which is shown generally in FIG. 5) to place fasteners 28 into the fastening region 26 of the trunk 12. The prosthesis 10 is thereby secured in position.


II. Prosthesis Attachment Systems and Methods


The fastener assembly 34 can be variously constructed and configured.


In an illustrated arrangement (see FIG. 6), the fastener attachment assembly 34 comprises a fastener guide component 36 and a fastener applier component 38. The guide component 36 can comprise, e.g., a guide sheath that desirably has a steerable or deflectable distal tip. The guide component 36 can be initially deployed over the guidewire that is used to deliver and position the prosthesis 10. The guide wire can be withdrawn after the guide component 36 is deployed and positioned, so that the applier component 38 can be introduced.


In this arrangement, the applier component 38 is desirably deployed through the guide component 36. A fastener drive mechanism 40 on the fastener applier component 38 carries at least one fastener 28. The fastener drive mechanism 40 advances the fastener 28, causing it to penetrate the prosthesis 10 and underlying tissue wall. In this way, the fastener anchors the prosthesis 10 firmly in place.


In the illustrated embodiment (see FIG. 6), the fastener applier 38 comprises a catheter 42. The catheter 42 carries the fastener drive mechanism 40 at its distal tip.


The fastener drive mechanism 40 comprises carrier 50. The carrier 50 is sized and configured to carry a selected fastener 28. The fastener drive mechanism 40 also includes a driver 52, which is coupled to impart movement to the carrier 50. The driver 52 and carrier 50 can comprise an integrated unit, with the carrier 50 being formed on the distal end of the driver 52, as shown, or they can comprise separate components, e.g., with the driver comprising a clutch or the like for the carrier 50. The driven movement deploys the fastener 28. The type of driven movement that is imparted depends upon the type of fastener 28 that is used.


In the illustrated embodiment (see FIG. 7) the fastener 28 comprises is an open helical coil 54 with a sharpened leading tip 56. This type of helical fastener is deployed into tissue by rotational movement. Consequently, rotational movement is imparted by the driver 52 to the carrier 50, which is sized and configured to carry the fastener shown in FIG. 7.


The actuation of the driver 52 can, of course, be accomplished in various ways, e.g., mechanical (i.e., manual or hand-powered), electrical, hydraulic, or pneumatic.


In the illustrated embodiment (see FIG. 6), a drive motor 58 imparts rotation to the driver 52 through a drive cable 60. In the illustrated embodiment (FIG. 6), the drive motor 58 is housed in a handle 62, which is carried at the proximal end of the catheter 42. The drive cable 60 extends from the handle 62, through the catheter 42, and couples to the driver 52 at the distal end of the catheter 42. The drive cable 60 is desirably made of a suitable material that allows for both bending and rotation.


Activation of the drive motor 58 (e.g., by a physician controlled switch 64 on the handle 62) rotates, as a unit, the drive shaft 60, the driver 52, the carrier 50, and the fastener 28 in the carrier 50. The rotational movement causes the helical fastener 28 to travel into the prosthesis 10 and the tissue wall.


The implantation force of the fastener drive mechanism 40 is desirably resolved in some manner to provide positional stability and resist unintended movement of the carrier 50 relative to the implantation site. A resolution force is desirably applied to counteract and/or oppose the implantation force of the fastener drive mechanism 40. It is desirable to resolve some or all or a substantial portion of the implantation force within the vessel lumen (or other hollow body organ) itself, and preferably as close to the implantation site as possible.


The tubular body of the guide component 36 and/or the shaft of the catheter 42 can be sized and configured to possess sufficient column strength to resolve some or all or at least a portion of the implantation force within the vessel lumen or hollow body organ. FIG. 5 shows the guide component 36 braced against the vessel wall to apply a counterbalancing resolution force. In addition, or alternatively, the guide component 36 and/or the fastener applier component 38 can include some form of stabilization means for applying a counteracting force at or near the carrier 50. Various types of stabilization means are disclosed in co-pending U.S. patent application Ser. No. 10/669,881, filed Sep. 24, 2003, and entitled “Catheter-Based Fastener Implantation Apparatus and Methods with Implantation Force Resolution.”


The carrier 50 itself can be various constructed, as can the fastener 28 to facilitate its coupling to the carrier 50. Representative embodiments will now be described.


A. Carriers with Independent Fastener Release Mechanisms


1. Carriers with Fastener Support Elements Having Release Mechanisms


The proximal end of the fastener 28 desirably includes a fitting 66 that, in use, couples the fastener 28 to the carrier 50. In one illustrated embodiment (see FIG. 7), the fitting 66 comprises an L-shaped brace or leg 66. The L-shape leg 66 desirably bisects the entire interior diameter of the coil 54; that is, the L-shaped leg 66 extends completely across the interior diameter of the coil 54, as FIG. 7 shows.


In this arrangement, the carrier 50 is sized and configured to engage the fitting 66, i.e., L-shaped leg 66, to thereby impart rotation to the helical fastener 28 to achieve implantation. The L-shaped leg 66 also serves as a stop to prevent the helical fastener 28 from penetrating too far into the tissue.


In one illustrated embodiment, the carrier 50 (see FIGS. 8A(1) and 8A(2)) includes a fastener support element 68 that permits the selective release of the fastener 28. The support element 68 has at least two operating conditions.


In a first condition (see FIG. 8A(1)), the support element 68 engages the L-shaped leg 66 of the fastener 28 to hold the fastener 28 on the carrier 50. In the first condition, rotation of the carrier 50 imparts rotation to the fastener 28 (as shown by the rotational arrow in FIG. 8A(2), to allow implantation of the fastener 28 into the prosthesis 10/tissue wall without releasing the fastener 28 (i.e., in response to rotation in one direction, as FIG. 8A(2) shows), as well as allow the withdrawal the fastener 28 from the prosthesis 10/tissue wall without releasing the fastener 28 (i.e., in response to rotation in an opposite direction, as FIG. 8C shows).


In a second condition (see FIGS. 8B(1) and 8(B)(2)), the support element 68 releases the fastener 28. In the second condition, the fastener 28 and the carrier 50 can be separated. Release of the fastener 28 from the carrier 50 can be and desirably is accomplished without rotation of the carrier 50. It is desirable that the support element 68 can affect separation of the fastener 28 while the carrier 50 is stationary and not rotating.


The support element 68 therefore differentiates the step of operating the carrier 50 to implant the fastener 28 (by rotation of the carrier 59 with the support element 68 in its first condition) from the step of releasing the fastener 28 from the carrier 50 (by placing the support element 68 in its second condition, which is desirably achieved independent of rotation of the carrier 50). The support element 68 thereby also makes possible the use of the carrier 50 to withdraw the fastener 28 from tissue and to retrieve or reposition the fastener 28, if desired. Operation of the support element 68 independent of operation of the carrier 50 makes possible the release of the fastener 28 from the carrier 50 in a separate releasing step, which can be delayed to assure that implantation of the fastener 28 has been satisfactorily completed.


The features of the support element 68 just described can be achieved by the use of various structural embodiments. In the embodiment shown in FIGS. 8A(1) and 8B(1), for example, the support element takes the form of hinged gripping jaws 70 on the distal end of the carrier 50. The gripping jaws 70 are moveable between a mutually closed condition (i.e., the first condition, as shown in FIG. 8A(1)) and a mutually opened condition (i.e., the second condition, as shown in FIG. 8B(1)). The L-shaped leg 66 of the fastener 28 is gripped by interference fit within a receptacle 72 formed between the jaws 70 when the jaws 70 are mutually closed, as FIGS. 8A(1) and 8A(2) show. The receptacle 72 opens and frees the L-shaped leg 66 when the gripping jaws 70 are mutually opened, as FIGS. 8B(1) and 8B(2) show.


In this embodiment, a physician-manipulated actuator 74 selectively pivots the hinged gripping jaws 70 from their mutually closed condition to their mutually opened condition. In the illustrated embodiment (see FIGS. 8A(1) and 8B(1)), the actuator 74 comprises a pull cable 76 or stylet, which is coupled at its proximal end to a controller 78 on the handle (see FIGS. 8A(2) and 8B(2)). The pull cable 76 extends through the catheter 42 and terminates at its distal end with a shaped cam element 78. The cam element 78 in the illustrated embodiment is ball-shaped. It occupies the area defined between tapered, facing cam surfaces 80 formed on the interior of the gripping jaws 70. When the jaws 70 are mutually closed (FIG. 8A(1)), the cam element 78 rests in the region of greatest distance between cam surfaces 80, adjacent the distal end of the gripping jaws 70. In this arrangement, when the physician manipulates the controller 78 to pull the cable 76 in an aft direction (i.e., toward the handle 62) (FIG. 8B), the cam element 78 travels on the tapered cam surfaces 80 toward the region of least distance between the surfaces 80. As it moves, the cam element 78 applies force against the cam surfaces 80 to pivot the jaws 70 open, i.e., moving them from the mutually closed to the mutually opened condition, as FIG. 8B(1) shows.


In the illustrated embodiment, the hinged gripping jaws 70 are desirably biased toward the mutually closed condition. A spring can be used for the purpose. Desirably, the gripping jaws 70 are formed by machining or molding from an elastic, spring-like material (metal or plastic). The formed material includes an integral hinge 82, which normally biases the gripping jaws 70 closed. The hinge 82 yields to the force applied by the cam element 78 against the cam surfaces 80, but returns the jaws 70 to their mutually closed condition in the absence of the force. In this arrangement (see FIG. 8A(1)), a physician can snap fit the L-shaped leg 66 of a fastener 28 into the receptacle 72 between the gripping jaws 70 at time of use. The snap fit provides tactile assurance that the fastener 28 has been properly engaged within the receptacle 72 of the gripping jaws 70.


In an alternative embodiment (see FIGS. 9A(1) and 9B(1)), the support element 68 takes the form of spring-biased struts 84 on the carrier 50. The struts 84 resiliently open to accommodate snap-fit passage of the L-shaped leg 66 into a retaining space 87 between the struts 84, allowing the coil 54 of the fastener 28 to nest upon the struts 84 (as FIG. 9A(2) shows). The resilient, normally closed condition of the struts 84 comprises the first operating condition, which holds the fastener 28 on the struts 84, thereby securing the fastener 28 to the carrier 50. In this condition, rotation of the carrier 50 rotates the fastener 28, to allow implantation of the fastener 28 into tissue and/or withdrawal of the fastener 28 from tissue.


In this arrangement, a physician-manipulated actuator 86 comprising, e.g., a push cable or stylet, can be advanced forward through the catheter by operation of a controller 88 on the handle 62. The carrier 50 need not be and desirably is not rotated during this operation. The push cable 86, when advanced (see FIGS. 8B(1) and 8B(2), contacts the L-shaped leg 66 and urges the leg 66 out of the retaining space 87 against the resiliently closed struts 84. The struts 84 are resiliently displaced by force of the L-shaped leg 66, which are caused to assume a temporary, mutually opened condition. The fastener 28 can thereby be ejected from the carrier 50.


In an alternative arrangement (see FIGS. 10A(1) and 10B(2)), the support element 68 may include normally open struts 90 that define a receptacle 92 and include a detent 94 that governs passage of the L-shaped leg 66 into and out of the receptacle 92. A physician-manipulated actuator 96 comprising, e.g., a push-pull cable or stylet, can be advanced fore and aft through the catheter 42 into and out of contact with the detent 94, e.g., by operation of a controller 98 on the handle 62 (see FIGS. 10A(2) and 10(B)(2)). The cable 96, when advanced into contact with detent 94 (see FIG. 10A(1)(1)) locks the detent 94 in a position projecting into the receptacle 92. The detent 94, when locked, blocks entry into or out of the receptacle 92. The cable 96, when withdrawn from contact with detent 94, unlocks the detent 94, and allows movement of the detent 94 out of the position blocking the receptacle 92.


The detent 94, when unlocked (see FIGS. 10A(1) and 10A(2)), accommodates passage of the L-shaped leg 66 into the retainer 92 between the struts 90, while the remainder of the fastener 28 nests upon the struts 90. The fastener 28 can be loaded onto the carrier 50 in this fashion. The subsequent locking of the detent 94 (see FIG. 10A(2)) blocks release of the L-shaped leg 66, securing the fastener 28 to the carrier 50. This corresponds to the above-described first operating condition. In this condition, rotation of the carrier 50 rotates the fastener 28 (as shown by the rotational arrow in FIG. 10A(2)), to allow implantation of the fastener 28 into the prosthesis 10/tissue wall and/or withdrawal of the fastener 28 from the prosthesis 10/tissue wall.


The cable 96, when advanced out of contact with detent 94, unlocks the detent 94 (see FIGS. 10B(1) and 10B(2)). The carrier 50 need not be and desirable is not rotated during this operation. This allows passage of the L-shaped leg 66 past the detent 94 and free of the receptacle 92, as previously described, in response to aft movement of the catheter 42 and attached carrier 50.


Alternatively, as shown in FIG. 11, the detent 94 may be biased by a spring 100 toward a normally projecting condition to serve the same function.


2. Carriers with Releasable Fastener Cap Assemblies


In another illustrated embodiment (sees FIGS. 12A and 12B), the fastener 28 takes the form of a fastener cap assembly 102 that is releasably fitted onto a specially adapted carrier 104 (see FIGS. 14A and 14B) at time of use. In the illustrated arrangement (see FIGS. 12A and 12B), the fastener cap assembly 102 includes a helical fastener 106 on which a proximal cap 108 is mounted. The cap 108 can comprise a plastic, metal, or ceramic biocompatible material. The cap 108 can be secured to the proximal end of the fastener 206, e.g., by adhesives, machining, molding, or welding. The cap 108 includes preformed side mounts 110. In this arrangement, the cap 108 serves the same general function as the L-shaped leg 66 shown in FIG. 7, i.e., it is a fitting secured to the fastener that enables the coupling of the fastener 28 to the carrier.


In this arrangement (see FIGS. 14A and 14B), the carrier 104 includes an attachment mechanism 112, which will be described in greater detail later. The attachment mechanism 112 is sized and configured to engage the mounts 110, to thereby couple the fastener assembly 102 to the carrier 104 at time of use. The attachment mechanism 112 imparts rotation to the fastener assembly 102 when the carrier 104 is rotated (see FIG. 15A) to achieve implantation of the fastener assembly 102 into the prosthesis 10/tissue wall without releasing the fastener assembly 102 (i.e., in response to rotation of the carrier 104 in one direction, as FIG. 15A shows). The attachment mechanism 112 can also withdraw the fastener assembly 102 from the prosthesis 10/tissue wall (see FIG. 15C) without releasing the fastener assembly 102 (i.e., in response to rotation of the carrier 104 in an opposite direction, as FIG. 15C shows).


The carrier 104 also includes a release mechanism 114, as will be described in greater detail later. The release mechanism 114 selectively releases the fastener assembly 102 from the attachment mechanism 112 (see FIG. 15B). Release of the fastener assembly 102 from the attachment mechanism 112 can be and desirably is accomplished without rotation of the carrier 104.


The carrier 104 with an attachment mechanism 112 to which a fastener assembly 102 can be fitted at time of use, as well as an independent, selectively operable release mechanism 114 allows a physician to operate the carrier 104 to implant the fastener assembly 102 separate from the step of releasing the fastener assembly 102 after implantation has been accomplished. The carrier 104 with a selective release for the fastener assembly 102 also makes possible the withdrawal the fastener assembly 102 from tissue and the retrieval and/or reposition the fastener assembly 104, if desired, while the carrier 104 remains secured to the fastener assembly 102. In this arrangement, release of the fastener assembly 102 from the carrier 104 can be accomplished once fastener assembly 102 has been satisfactorily implanted, or otherwise at a time controlled by the operator.


The features of the carrier 104 as just described can be achieved by the use of various structural embodiments. In the embodiment shown in FIGS. 13A and 13B, the attachment mechanism 112 comprises a pair of gripper arms 116 coupled to the driver 52. The gripper arms 116 can be made by machining or molding from a metal or plastic material. The gripper arms 116 can be normally biased toward an inwardly deflected condition. The bias can be achieved, e.g., by imparting a spring memory to the arms 116. Alternatively, the arms 116 need not be biased inwardly, but instead include outside edges that are inclined, as FIG. 13B shows. The arms include outwardly projecting tabs 126 that are sized to snap into mounts 110 on the cap 108 (as FIG. 14B shows).


In this arrangement, the release mechanism 114 comprises a spacer rod 118 extends between the gripper arms 116. The rod 118 carries at its distal end a cam element 120. When withdrawn from contact with the gripper arms 116 (as FIG. 13B shows), the gripper arms 116 are positioned such that the tabs 126 will snap into the mounts 110 on the cap 108, as FIG. 14A shows. The cam element 120, when disposed in contact with the gripper arms 116 (as shown in FIG. 13A), spreads the gripper arms 116 apart, into an outwardly deflected condition, locking the tabs 116 into the mounts 110, as FIG. 14B shows.


A spring 122 normally urges the cam element 120 toward contact with the gripper arms 116 (as shown in FIGS. 13A and 14B). The rod 118, when pulled aft (as FIGS. 13B and 14A show) withdraws the cam element 120, and the gripper arms 116 are positioned to receive the cap 108. The rod 118 extends through the catheter 42 and is coupled to a controller 124 on the handle 62 (see FIGS. 15A and 15B).


When the gripper arms 116 are maintained by the cam element 120 in their outwardly deflected condition (see FIG. 14B), the tabs 126 lock into the mounts 110 on the fastener cap 108, securing the fastener assembly 102 to the carrier 104. Conversely, when the cam element 120 is withdrawn, the tabs 126 allow the fastener assembly 102 to be inserted onto or separated from the carrier 104.


In use, the physician pulls back on the control 124 to withdraw the cam element 120 against the bias of the spring 122 and snap-fits a fastener assembly 102 onto the carrier 104. The physician then releases the control 124 to allow the spring 122 to return forward and lock the fastener assembly 102 onto the carrier 104. The physician then deploys the catheter 42 holding the fastener assembly 102 to the targeted site (see FIG. 15A). By rotating the carrier 104, the physician implants the fastener assembly 102 into the prosthesis 10/tissue wall.


When the fastener assembly 102 has been satisfactorily implanted, the physician pulls back on the control 124 and the catheter 42 (see FIG. 15B) to separate the fastener assembly 102 from the carrier 104. The physician withdraws the catheter 42 and repeats the forgoing steps until the desired number of fastener assemblies 102 has been implanted.


B. Carriers with Two-Phase Ejection of Fasteners


The above-described embodiments provide the ability to withdraw a given fastener from a prosthesis/tissue wall prior to completion of the implantation step. The above-described embodiments make this feature possible by providing a fastener applier 38 that includes a fastener release mechanism that works independent of the fastener implantation mechanism.


In FIGS. 16A(1)/A(2), 16B, and 16C, a fastener applier 38 includes a fastener carrier 128 that implements this feature without an independent release mechanism. In FIGS. 16A(1)/A(2), 16B, and 16C, the fastener carrier 128 is operated in two phases. The first or initial phase advances a fastener 28 into an incomplete implantation position within a prosthesis 10/tissue wall (FIG. 16B), which represents a sufficient distance to gain purchase, but which is short of full implantation. That is, given that full implantation of the fastener 28 requires the application of an implantation force under prescribed conditions, i.e., for a prescribed time period or for a prescribed number of rotations of the fastener—the implantation force is applied to the fastener 28 during the first phase under conditions that do not achieve the prescribed conditions. Thus, full implantation is not achieved. During the first phase, the fastener 28 remains coupled to the fastener carrier 128, to allow the physician to operate the fastener carrier 128 to withdraw/retrieve the fastener 28, if desired (see FIG. 16D).


The first phase presents a decision point to the physician. At end of the first phase, a lull phase exists, during which operation of the fastener carrier 128 is interrupted. A prescribed input command is required to move out of the lull phase. During the lull phase, the physician can elect to withdraw or retrieve the fastener 28 (FIG. 160). Alternatively, the physician can elect to continue implantation and proceed to the second phase. In the second or final phase, the fastener carrier 128 advances the fastener 28 from the incomplete implantation position (FIG. 16B) to the complete implantation position (FIG. 16C), at the end of which the fastener 28 itself automatically separates from the fastener carrier 128. That is, during the second phase, implantation force is applied to the fastener 28 under conditions that supplement the conditions of the first phase in order to meet the conditions prescribed for full implantation.


The fastener applier 38 can implement this feature in various structural embodiments. In the illustrative embodiment shown in FIG. 16A(1), the carrier 128, coupled to a driver 52, includes a slot 130, which receives the L-shaped leg 66 to couple the fastener 28 for rotation with the carrier 128. In this embodiment, the turns of the coil 54 rest in complementary internal grooves 132 that surround the carrier 128. The grooves 132 could be positioned along the entire length of the fastener 28 or within a portion of its length. Activation of the drive mechanism rotates, as a unit, the driver 52, the carrier 128, and the helical fastener 28 (as FIG. 16A(2) shows). This rotation causes the helical fastener 28 to travel within the internal grooves 132 of the fastener applier and into the prosthesis 10 and tissue wall. Uninterrupted rotation of the carrier 128 will cause the helical fastener 28 to be rotated completely off the carrier and through the prosthesis 10 and into the tissue wall (as FIG. 16C shows).


In the illustrated embodiment, the drive mechanism includes a motor control unit 134 (see FIGS. 16A(2), 168, and 16D). The motor control unit 134 is conditioned to operate the carrier 128 in the two distinct phases, as above described. The first phase of fastener implantation is initiated by the physician activating a rotation command, e.g., by manipulating a first switch 136 on the handle 62. During the first phase of deployment (FIG. 16B), the carrier 128 is driven sufficient to rotate the helical fastener 28 to a position in which the distal portion of the fastener 28 has implanted itself into the target tissue, but in which the proximal portion of the fastener 28 is still retained within the internal threads 132 of the carrier 128. At this point, the first phase ends, and the motor control unit 134 enters the lull phase, automatically interrupting rotation of the carrier 128. The motor control unit 134 can accomplish motor control in this fashion by either conventional mechanical and or electronic means, e.g., through a programmable microprocessor.


At this juncture, the physician has the option of reversing the insertion process and removing the fastener 28, if desired (see FIG. 16D), e.g., by reversing the switch 136 or activating another switch 138 on the handle 62. At this juncture, the physician also has the option of completing the implantation process, e.g., by manipulating the switch 136 in a preprogrammed fashion (for example, by double switching).


In one variation, the motor control unit 136 can receive input reflecting a performance criteria measured during the first phase of deployment. The motor control unit 136 assesses the value of the performance criteria, to determine whether it falls within a predetermined acceptable range. If so, the second phase of deployment may occur automatically without a pause and without a second input from the user. For example, motor current used during the first phase of fastener deployment could be measured, and from this the fastener driving torque could be calculated. A torque within a range of acceptable values would imply that the fastener 28 had successfully entered the target tissue and fastener implantation could be completed automatically. A torque that was outside the acceptable range could result in either a pause at the end of phase one, where the user could make the decision to continue or reverse the fastener deployment, or an automatic reversal of fastener deployment.


In an alternative embodiment, a fastener release mechanism 114 of the type shown, e.g., in FIGS. 13A/B and 14A/B can be used in association with a motor control unit 134. In this arrangement, the motor control unit 134 is conditioned to operate the carrier 104 to drive the fastener assembly 102 in a single phase of deployment into tissue. At this point, the release mechanism 114 can be operated in the manner previously described, to separate the fastener assembly 102 from the carrier 104. The motor control unit 134 can be conditioned by mechanical and/or electronic means to indicate and/or control the number of revolutions and/or the torque applied to accomplish the installation of the fastener assembly 102 in tissue. In this embodiment, there is no need for multiple phases, because the physician ultimately controls the release of the fastener assembly 102 by manipulation of the release mechanism 114.


C. Carriers with Tethered Fasteners


In all of the above embodiments, or as an alternative embodiment in and of itself, a fastener applier 38 can include an element 140 to releasably tether a fastener 28 to the applier 38 even after the fastener 28 has been separated from the applier 38 (see FIG. 17A). The tether element 140 serves as a “life line,” maintaining a connection of last resort between the applier 38 and a fastener 28. The tether element 28 allows the fastener 28 to be retrieved if, for any reason, the fastener 28 inadvertently breaks loose from tissue and/or the applier 38 during or after implantation. The connection between the tether element 140 and the applier 38 requires a deliberate act of the physician to be broken, adding a confirming, final step to the implantation process (see FIG. 17B).


The tether element 140 can be variously constructed. In FIG. 17A, the tether element 140 comprises a thread, braid, wire, or tubing structure 142. The proximal end of the tether element structure 142 is attached to the fastener applier 38 in a manner that can be detached by application of a deliberate pulling force. The distal end of the tether element structure 142 is frangible and can be broken by a force less than the deliberate pulling force once desired deployment of the fastener 28 is confirmed, as FIG. 17B shows. The tether element structure 142 has sufficient length to be able to retract the fastener applier 38 enough to visualize the fastener in position (as FIG. 17A shows). The force to break the frangible distal end of the tether element structure 142 is less than the force required to dislodge the fastener 28 from tissue. Desirably, the frangible distal end of the tether element structure 142 detaches from the fastener 28 without leaving remnants on the fastener 28 (as FIG. 17B shows).


The tether element structure 142 can be sized and configured in other, different ways to form a frangible connection with a fastener 28. For example (see FIGS. 18A and 18B), the L-shaped leg 66 could be crimped to form an area of weakness 144 (FIG. 18A), to which the tether element structure 142 applies force to free the tether element structure 142 from the fastener 28 (FIG. 18B).


Alternatively, the junction between the tether element structure 142 and the fastener 28 can comprise an area of weakness 146 (e.g., by melding, soldering, gluing, heating, or shearing) that is broken by the application of a prescribed force in a prescribed manner, e.g., by rotation (FIG. 19A) or pulling (FIG. 19B). Alternatively, the junction between the tether element structure 142 and the fastener 28 may comprise a threaded joint 146 (see FIGS. 20A and 20B); or a snap-fit ball and socket joint 148 (see FIGS. 21A and 21B); or a slide-fit joint 150 (see FIGS. 22A and 22B; or a knotted joint 152 (FIGS. 23A and 23B); or a frictional junction 154 that is relieved by split open a tube 156 using a rip cord 158 (FIGS. 24A and 24B). Still, alternatively, the junction between the tether element 140 and the fastener 28 can comprise an interlocking mechanism 160, for example, a slidable outer sleeve 162 that, when advanced (FIG. 25A), captures an appendage 164 on the fastener 28 and, when retracted (FIG. 25B), frees the appendage 164.


The preferred embodiments of the invention are described above in detail for the purpose of setting forth a complete disclosure and for the sake of explanation and clarity. Those skilled in the art will envision other modifications within the scope and sprit of the present disclosure.


The above described embodiments of this invention are merely descriptive of its principles and are not to be limited. The scope of this invention instead shall be determined from the scope of the following claims, including their equivalents.

Claims
  • 1. A tool for applying an implantation force to a helical fastener sized and configured for penetration in tissue comprising: a tool body comprising internal threads;a driven member carried by the tool body and operable to apply the implantation force;a carrier on the driven member configured to couple the fastener to the driven member to transfer the implantation force from the driven member to the fastener, the carrier comprising a distal portion wherein the distal portion remains within the tool body during implantation of the fastener; andwherein the tool is configured to operate in phases including:an initial phase operating the carrier to partially implant the fastener into tissue such that a proximal portion of the fastener remains coupled to the carrier, wherein the proximal portion of the fastener is retained within the internal threads of the tool body at the end of the initial phase;a lull phase interrupting operation of the carrier, wherein the fastener may be removed; anda final phase operating the carrier to release the fastener therefrom and implant the fastener in tissue.
  • 2. A tool according to claim 1, wherein the tool requires a final phase command to advance from the lull phase to the final phase.
  • 3. A tool according to claim 2, wherein the driven member is also operable to apply a removal force to withdraw the fastener from tissue, and wherein the tool includes a removal phase operating the carrier to transfer the removal force to the fastener, the tool requiring a removal phase command different from the final phase command to advance from the lull phase to the removal phase.
  • 4. A tool according to claim 3, wherein the carrier is rotated in one direction to apply the implantation force and rotated in an opposite direction to transfer the removal force.
  • 5. A tool according to claim 1, further including an element tethering the fastener to the tool body, the element including a frangible portion.
  • 6. A tool according to claim 1, wherein the driven member is rotated to apply the implantation force.
  • 7. A tool according to claim 1, wherein the carrier comprises a distal portion having a configuration that corresponds to a configuration of a proximal end of the fastener, such that the proximal end of the fastener engages with the distal portion of the carrier to couple the fastener to the carrier throughout the initial phase.
  • 8. A tool according to claim 7, wherein the proximal end of the fastener comprises a leg portion that engages with the distal portion of the carrier throughout the initial phase.
  • 9. A tool according to claim 1, wherein the tool is configured to carry and deploy a single helical fastener at a time.
  • 10. A tool according to claim 1, wherein the tool is configured to rotatably drive the fastener into tissue.
  • 11. A method for implanting a helical fastener in tissue comprising: providing a tool as defined in claim 1;coupling a helical fastener to the carrier;accessing a tissue region;operating the tool in the initial phase to partially implant the fastener in the tissue region;deciding during the lull phase to commence the final phase; andentering a final phase command to advance the tool from the lull phase to the final phase, thereby completing the implantation of the fastener in the tissue region.
  • 12. A tool for applying an implantation force to a helical fastener sized and configured for penetration in tissue comprising: a tool body comprising a tubular member comprising internal threads;a driven member, disposed within the tubular member of the tool body and operable to apply the implantation force;a carrier disposed on the driven member and within the tubular member of the tool body, the carrier configured to couple the fastener to the driven member to transfer the implantation force from the driven member to the fastener, the carrier comprising a distal portion having a configuration that corresponds to a configuration of a proximal end of the fastener wherein the distal portion remains within the tool body during implantation of the fastener, andwherein the tool is configured to operate in phases including:an initial phase operating the carrier partially to implant the fastener into tissue such that a proximal portion of the fastener is retained within the internal threads of the tool body at the end of the initial phase, wherein the proximal end of the fastener engages with the distal portion of the carrier to couple the fastener to the carrier throughout the initial phase,a lull phase interrupting operation of the carrier, wherein the fastener may be removed, anda final phase operating the carrier to release the fastener therefrom and implant the fastener in tissue.
  • 13. A tool according to claim 12, wherein the proximal end of the fastener comprises a leg portion that engages with the distal portion of the carrier throughout the initial phase.
RELATED APPLICATIONS

This application is a continuation application of U.S. patent application Ser. No. 10/786,465, filed on Feb. 25, 2004 (now U.S. Pat. No. 8,231,639), which is a continuation-in-part of U.S. patent application Ser. No. 10/693,255, filed Oct. 24, 2003 (now U.S. Pat. No. 6,929,661), which claims the benefit of U.S. Provisional Patent Application Ser. No. 60/489,011, filed Jul. 21, 2003. U.S. patent application Ser. No. 10/786,465 is also a continuation-in-part of U.S. patent application Ser. No. 10/307,226, filed Nov. 29, 2002 (now U.S. Pat. No. 8,075,570), which is a continuation-in-part of U.S. patent application Ser. No. 10/271,334, filed Oct. 15, 2002 (now U.S. Pat. No. 6,960,217), which claims the benefit of U.S. Provisional Patent Application Ser. No. 60/333,937, filed Nov. 28, 2001.

US Referenced Citations (296)
Number Name Date Kind
2033039 Limpert Mar 1936 A
3499222 Linkow et al. Mar 1970 A
3686740 Shiley Aug 1972 A
3799172 Szpur Mar 1974 A
4140126 Choudhury Feb 1979 A
4255820 Rothermel et al. Mar 1981 A
4307722 Evans Dec 1981 A
4580568 Gianturco Apr 1986 A
4625597 Cast Dec 1986 A
4694827 Weiner et al. Sep 1987 A
4781682 Patel Nov 1988 A
4898577 Badger et al. Feb 1990 A
4899747 Garren et al. Feb 1990 A
4921484 Hillstead May 1990 A
4990151 Wallsten Feb 1991 A
4994071 MacGregor Feb 1991 A
5030204 Badger et al. Jul 1991 A
5042707 Taheri Aug 1991 A
5044519 Aoyama Sep 1991 A
5071407 Termin et al. Dec 1991 A
5104399 Lazarus Apr 1992 A
5185004 Lashinski Feb 1993 A
5192314 Daskalakis Mar 1993 A
5195968 Lundquist et al. Mar 1993 A
5207695 Trout, III May 1993 A
5282824 Gianturco Feb 1994 A
5290295 Querals et al. Mar 1994 A
5318525 West et al. Jun 1994 A
5320630 Ahmed Jun 1994 A
5330490 Wilk et al. Jul 1994 A
5330503 Yoon Jul 1994 A
5334196 Scott et al. Aug 1994 A
5352197 Hammersmark et al. Oct 1994 A
5364351 Heinzelman et al. Nov 1994 A
5383880 Hooven Jan 1995 A
5387235 Chuter Feb 1995 A
5409498 Braddock et al. Apr 1995 A
5456713 Chuter Oct 1995 A
5456714 Owen Oct 1995 A
5470337 Moss Nov 1995 A
5474568 Scott Dec 1995 A
5480382 Hammerslag et al. Jan 1996 A
5480423 Ravenscroft et al. Jan 1996 A
5489295 Piplani et al. Feb 1996 A
5522881 Lentz Jun 1996 A
5531686 Lundquist et al. Jul 1996 A
5534007 St. Germain et al. Jul 1996 A
5562728 Lazarus et al. Oct 1996 A
5571171 Barone et al. Nov 1996 A
5571173 Parodi Nov 1996 A
5582616 Bolduc et al. Dec 1996 A
5591195 Taheri et al. Jan 1997 A
5609627 Goicoechea et al. Mar 1997 A
5626613 Schmieding May 1997 A
5628788 Pinchuk May 1997 A
5632772 Alcime et al. May 1997 A
5634936 Linden et al. Jun 1997 A
5639278 Dereume et al. Jun 1997 A
5662675 Polanskyj Stockert et al. Sep 1997 A
5662683 Kay Sep 1997 A
5662700 Lazarus Sep 1997 A
5676696 Marcade Oct 1997 A
5676697 Mcdonald Oct 1997 A
5683450 Goicoechea et al. Nov 1997 A
5693084 Chuter Dec 1997 A
5693086 Goicoechea et al. Dec 1997 A
5700269 Pinchuk et al. Dec 1997 A
5702343 Alferness Dec 1997 A
5702365 King Dec 1997 A
5702408 Wales et al. Dec 1997 A
5707376 Kavteladze et al. Jan 1998 A
5713907 Hogendijk et al. Feb 1998 A
5733325 Robinson et al. Mar 1998 A
5749921 Lenker et al. May 1998 A
5755777 Chuter May 1998 A
5762458 Wang et al. Jun 1998 A
5776142 Gunderson Jul 1998 A
5782844 Yoon et al. Jul 1998 A
5797933 Snow et al. Aug 1998 A
5800528 Lederman et al. Sep 1998 A
5810882 Bolduc et al. Sep 1998 A
5814016 Valley et al. Sep 1998 A
5824008 Bolduc et al. Oct 1998 A
5824037 Fogarty et al. Oct 1998 A
5824041 Lenker et al. Oct 1998 A
5830221 Stein et al. Nov 1998 A
5830229 Konya et al. Nov 1998 A
5843160 Rhodes Dec 1998 A
5855565 Bar-Cohen et al. Jan 1999 A
5855598 Pinchuk Jan 1999 A
5861003 Latson et al. Jan 1999 A
5865791 Whayne et al. Feb 1999 A
5876432 Lau et al. Mar 1999 A
5904713 Leschinsky May 1999 A
5906619 Olson et al. May 1999 A
5906641 Thompson et al. May 1999 A
5916263 Goicoechea et al. Jun 1999 A
5944750 Tanner et al. Aug 1999 A
5957940 Tanner et al. Sep 1999 A
5964772 Bolduc et al. Oct 1999 A
5968053 Revelas Oct 1999 A
5972023 Tanner et al. Oct 1999 A
5980548 Evans et al. Nov 1999 A
5993401 Inbe et al. Nov 1999 A
5993466 Yoon Nov 1999 A
5997556 Tanner Dec 1999 A
6016810 Ravenscroft Jan 2000 A
6024703 Zanelli et al. Feb 2000 A
6024763 Lenker et al. Feb 2000 A
6027462 Greene et al. Feb 2000 A
6070589 Keith et al. Jun 2000 A
6074418 Buchanan et al. Jun 2000 A
6077214 Mortier et al. Jun 2000 A
6077297 Robinson et al. Jun 2000 A
6086582 Altman et al. Jul 2000 A
6090137 Schmitt Jul 2000 A
6123722 Fogarty et al. Sep 2000 A
6126685 Lenker et al. Oct 2000 A
6129685 Howard, III Oct 2000 A
6145509 Tanner Nov 2000 A
6146339 Biagtan et al. Nov 2000 A
6152144 Lesh et al. Nov 2000 A
6162168 Schweich, Jr. et al. Dec 2000 A
6168610 Marin et al. Jan 2001 B1
6174323 Biggs et al. Jan 2001 B1
6179809 Khairkhahan et al. Jan 2001 B1
6197049 Shaolian et al. Mar 2001 B1
6203550 Olson Mar 2001 B1
6203568 Lombardi et al. Mar 2001 B1
6206827 Chin et al. Mar 2001 B1
6217597 Tanner Apr 2001 B1
6224540 Lederman et al. May 2001 B1
6231561 Frazier et al. May 2001 B1
6248118 Tanner et al. Jun 2001 B1
6250974 Kerek Jun 2001 B1
6258021 Wilk Jul 2001 B1
6258119 Hussein et al. Jul 2001 B1
6270516 Tanner et al. Aug 2001 B1
6273858 Fox et al. Aug 2001 B1
6286514 Lemelson Sep 2001 B1
6287315 Wijeratne et al. Sep 2001 B1
6293906 Vanden Hoek et al. Sep 2001 B1
6296656 Bolduc et al. Oct 2001 B1
6302906 Goicoechea et al. Oct 2001 B1
6309403 Minor et al. Oct 2001 B1
6319278 Quinn Nov 2001 B1
6336933 Parodi Jan 2002 B1
6343605 Lafontaine Feb 2002 B1
6346118 Baker et al. Feb 2002 B1
6352561 Leopold et al. Mar 2002 B1
6361556 Chuter Mar 2002 B1
6368345 Dehdashtian et al. Apr 2002 B1
6371919 Tanner et al. Apr 2002 B1
6398803 Layne et al. Jun 2002 B1
6402680 Mortier et al. Jun 2002 B2
6402780 Williamson, IV et al. Jun 2002 B2
6409757 Trout, III et al. Jun 2002 B1
6416522 Strecker Jul 2002 B1
6423059 Hanson et al. Jul 2002 B1
6425856 Shapland et al. Jul 2002 B1
6428565 Wisselink Aug 2002 B1
6454796 Barkman et al. Sep 2002 B1
6458152 Khosravi et al. Oct 2002 B1
6461365 Bolduc et al. Oct 2002 B2
6468260 Bumbalough et al. Oct 2002 B1
6482224 Michler et al. Nov 2002 B1
6520974 Tannerq et al. Feb 2003 B2
6544253 Tanner Apr 2003 B1
6558425 Rockwood, Jr. May 2003 B2
6562051 Bolduc et al. May 2003 B1
6565597 Fearnot et al. May 2003 B1
6576009 Ryan et al. Jun 2003 B2
6580417 Rosenberg et al. Jun 2003 B2
6592593 Parodi et al. Jul 2003 B1
6592615 Marcade et al. Jul 2003 B1
6595912 Lau et al. Jul 2003 B2
6607555 Patterson et al. Aug 2003 B2
6616684 Vidlund et al. Sep 2003 B1
6639278 Sumida et al. Oct 2003 B2
6652555 Vantassel et al. Nov 2003 B1
6652572 Kugler et al. Nov 2003 B2
6663558 Lau et al. Dec 2003 B2
6675809 Stack et al. Jan 2004 B2
6685620 Gifford, III et al. Feb 2004 B2
6702763 Murphy et al. Mar 2004 B2
6702844 Lazarus Mar 2004 B1
6709442 Miller et al. Mar 2004 B2
6719174 Swift Apr 2004 B1
6730119 Smalling et al. May 2004 B1
6746460 Gannoe et al. Jun 2004 B2
6800081 Parodi Oct 2004 B2
6878164 Kujawski et al. Apr 2005 B2
6929661 Bolduc et al. Aug 2005 B2
6960217 Bolduc Nov 2005 B2
6984241 Lubbers et al. Jan 2006 B2
6986775 Morales et al. Jan 2006 B2
6986784 Weiser et al. Jan 2006 B1
7033384 Gannoe et al. Apr 2006 B2
7037343 Imran May 2006 B2
7060021 Wilk Jun 2006 B1
7060023 French et al. Jun 2006 B2
7081086 Lau et al. Jul 2006 B2
7081129 Chobotov Jul 2006 B2
7128754 Bolduc Oct 2006 B2
7147657 Chiang et al. Dec 2006 B2
7155295 Lau et al. Dec 2006 B2
7179225 Shluzas et al. Feb 2007 B2
7306623 Watson Dec 2007 B2
7335213 Hyde et al. Feb 2008 B1
7361137 Taylor et al. Apr 2008 B2
7404824 Webler et al. Jul 2008 B1
7422558 Lau et al. Sep 2008 B2
7491232 Bolduc et al. Feb 2009 B2
7544198 Parodi Jun 2009 B2
7563267 Goldfarb et al. Jul 2009 B2
7591842 Parodi Sep 2009 B2
7637932 Bolduc et al. Dec 2009 B2
7704269 St. Goar et al. Apr 2010 B2
7727189 Vantassel et al. Jun 2010 B2
7753922 Starksen Jul 2010 B2
7811295 Kortenbach Oct 2010 B2
7823267 Bolduc et al. Nov 2010 B2
7828267 Iwabuchi et al. Nov 2010 B2
7828838 Bolduc et al. Nov 2010 B2
7959663 Bolduc Jun 2011 B2
7959670 Bolduc Jun 2011 B2
8075570 Bolduc et al. Dec 2011 B2
8080050 Chiang et al. Dec 2011 B2
8083752 Bolduc Dec 2011 B2
8092519 Bolduc Jan 2012 B2
8231639 Bolduc et al. Jul 2012 B2
20020026144 Patterson Feb 2002 A1
20020029077 Leopold et al. Mar 2002 A1
20020058855 Schweich, Jr. et al. May 2002 A1
20020065485 Dubois et al. May 2002 A1
20020087169 Brock et al. Jul 2002 A1
20020099432 Yee Jul 2002 A1
20020133054 Murphy et al. Sep 2002 A1
20020156365 Tsekos Oct 2002 A1
20030018358 Saadat Jan 2003 A1
20030060674 Gifford, III et al. Mar 2003 A1
20030078465 Pai et al. Apr 2003 A1
20030100943 Bolduc May 2003 A1
20030105519 Fasol et al. Jun 2003 A1
20030130731 Vidlund et al. Jul 2003 A1
20030149463 Solymar et al. Aug 2003 A1
20030158570 Ferrazzi Aug 2003 A1
20030163085 Tanner et al. Aug 2003 A1
20030204249 Letort Oct 2003 A1
20030233140 Hartley et al. Dec 2003 A1
20040002731 Aganon et al. Jan 2004 A1
20040039405 Petrovic et al. Feb 2004 A1
20040049207 Goldfarb et al. Mar 2004 A1
20040054352 Adams et al. Mar 2004 A1
20040093057 Bolduc et al. May 2004 A1
20040127916 Bolduc et al. Jul 2004 A1
20040138734 Chobotov et al. Jul 2004 A1
20040186566 Hindrichs et al. Sep 2004 A1
20040206363 Mccarthy et al. Oct 2004 A1
20040210304 Seguin et al. Oct 2004 A1
20040243170 Suresh et al. Dec 2004 A1
20040260322 Rudko et al. Dec 2004 A1
20040260383 Stelter et al. Dec 2004 A1
20050038506 Webler et al. Feb 2005 A1
20050043790 Seguin Feb 2005 A1
20050070992 Bolduc et al. Mar 2005 A1
20050113906 Bolduc et al. May 2005 A9
20050177180 Kaganov et al. Aug 2005 A1
20050187613 Bolduc et al. Aug 2005 A1
20050197716 Sharkey et al. Sep 2005 A1
20050240258 Bolduc et al. Oct 2005 A1
20050240260 Bolduc Oct 2005 A1
20060100640 Bolduc May 2006 A1
20060184224 Angel Aug 2006 A1
20060259125 Peacock, III Nov 2006 A1
20060287661 Bolduc et al. Dec 2006 A1
20070021753 Bolduc et al. Jan 2007 A1
20070021829 Bolduc Jan 2007 A1
20070032860 Brooks et al. Feb 2007 A1
20070073389 Bolduc et al. Mar 2007 A1
20070083255 Chiang et al. Apr 2007 A1
20080065117 Bolduc et al. Mar 2008 A1
20080065189 Bolduc Mar 2008 A1
20080065191 Bolduc et al. Mar 2008 A1
20080097489 Goldfarb et al. Apr 2008 A1
20080132996 Drasler et al. Jun 2008 A1
20090082852 Bolduc et al. Mar 2009 A1
20090099650 Bolduc et al. Apr 2009 A1
20090112302 Stafford Apr 2009 A1
20090112303 Bolduc Apr 2009 A1
20090138072 Gendreau May 2009 A1
20100094400 Bolduc et al. Apr 2010 A1
20110087320 Bolduc et al. Apr 2011 A1
20110238088 Bolduc et al. Sep 2011 A1
20110276062 Bolduc Nov 2011 A1
20120065661 Bolduc Mar 2012 A1
Foreign Referenced Citations (123)
Number Date Country
2004277897 Apr 2005 AU
2004287355 Jun 2011 AU
2006305688 Dec 2012 AU
2265131 Sep 1999 CA
2344252 Mar 2000 CA
2729464 Jun 2003 CA
2539265 May 2005 CA
2626505 Apr 2007 CA
2626106 May 2007 CA
2625082 Jul 2008 CA
2740831 Apr 2010 CA
2464900 Apr 2011 CA
2554022 Nov 2012 CA
2546721 Sep 2013 CA
1019461 Dec 1992 CN
1422139 Jun 2003 CN
1596087 Mar 2005 CN
1856280 Nov 2006 CN
1870949 Nov 2006 CN
1870951 Nov 2006 CN
1997318 Jul 2007 CN
101151002 Mar 2008 CN
101267788 Sep 2008 CN
101330882 Dec 2008 CN
101360466 Feb 2009 CN
101460104 Jun 2009 CN
101466316 Jun 2009 CN
100525719 Aug 2009 CN
101330882 Apr 2011 CN
101466316 Jun 2012 CN
3333427 May 1991 DE
69228184 Sep 1999 DE
10034105 Apr 2002 DE
10297483 Dec 2004 DE
0321912 Jun 1989 EP
0663184 Jul 1995 EP
0835642 Feb 2002 EP
1369098 Dec 2003 EP
1440673 Jul 2004 EP
1448117 Aug 2004 EP
1675528 Jul 2006 EP
1725172 Nov 2006 EP
1734872 Dec 2006 EP
1948080 Jul 2008 EP
2119416 Nov 2009 EP
2349086 Aug 2011 EP
2349087 Aug 2011 EP
2299548 Aug 1976 FR
2396824 Jul 2004 GB
2417208 Feb 2006 GB
2001509398 Jul 2001 JP
2001522292 Nov 2001 JP
2001526574 Dec 2001 JP
2002526193 Aug 2002 JP
2005046648 Feb 2005 JP
2005510293 Apr 2005 JP
2005510303 Apr 2005 JP
2007508894 Apr 2007 JP
2007508895 Apr 2007 JP
2007523694 Aug 2007 JP
2007535339 Dec 2007 JP
2009512497 Mar 2009 JP
2009512498 Mar 2009 JP
2009512499 Mar 2009 JP
2009095684 May 2009 JP
2009106763 May 2009 JP
2009106768 May 2009 JP
2009106775 May 2009 JP
2009112827 May 2009 JP
2009519046 May 2009 JP
10506026 Feb 2010 JP
2010051786 Mar 2010 JP
4465359 May 2010 JP
2011062570 Mar 2011 JP
4699445 Jun 2011 JP
WO-9300868 Jan 1993 WO
WO-9521592 Aug 1995 WO
WO-9603925 Feb 1996 WO
WO-9703616 Feb 1997 WO
WO-9712562 Apr 1997 WO
WO-9717039 May 1997 WO
WO-9717913 May 1997 WO
WO-9853761 Dec 1998 WO
WO-9930637 Jun 1999 WO
WO-9933402 Jul 1999 WO
WO-9933402 Sep 1999 WO
WO-9953845 Oct 1999 WO
WO-0064357 Jan 2000 WO
WO-0016701 Mar 2000 WO
WO-0035350 Jun 2000 WO
WO-0160432 Aug 2001 WO
WO-03032870 Apr 2003 WO
WO-03045283 Jun 2003 WO
WO-03045467 Jun 2003 WO
WO-03045467 Jul 2003 WO
WO-03079935 Oct 2003 WO
WO-2005032333 Apr 2005 WO
WO-2005037076 Apr 2005 WO
WO-2005044073 May 2005 WO
WO-2005044147 May 2005 WO
WO-2005044148 May 2005 WO
WO-2005067660 Jul 2005 WO
WO-2005081936 Sep 2005 WO
WO-2007046955 Oct 2005 WO
WO-2005102181 Nov 2005 WO
WO-2005032333 Apr 2006 WO
WO-2005067660 Apr 2007 WO
WO-2007046953 Apr 2007 WO
WO-2007046954 Apr 2007 WO
WO-2007046955 Apr 2007 WO
WO-2007047023 Apr 2007 WO
WO-2007053233 May 2007 WO
WO-2007046953 Jun 2007 WO
WO-2007047023 Oct 2007 WO
WO-2005081936 Nov 2007 WO
WO-2007053233 Jan 2008 WO
WO-2007046954 Nov 2008 WO
WO-2005044073 Mar 2009 WO
WO-2010004856 Jan 2010 WO
WO-2010044851 Apr 2010 WO
WO-2010044854 Apr 2010 WO
WO-2010044855 Apr 2010 WO
WO-2010044856 Apr 2010 WO
Non-Patent Literature Citations (396)
Entry
“5mm Origin Tracker It Runs in Circles Around Staples”, Guidant Origin Advertising Literature, (1995), 2 pgs.
“U.S. Appl. No. 10/271,334, Examiner Interview Summary mailed Feb. 11, 2005”, 2 pgs.
“U.S. Appl. No. 10/271,334, Non Final Office Action mailed May 18, 2004”, 9 pgs.
“U.S. Appl. No. 10/271,334, Notice of Allowance mailed Feb. 11, 2005”, 6 pgs.
“U.S. Appl. No. 10/271,334, Notice of Allowance mailed Mar. 17, 2005”, 3 pgs.
“U.S. Appl. No. 10/271,334, Notice of Allowance mailed Aug. 26, 2005”, 3 pgs.
“U.S. Appl. No. 10/271,334, Response filed Mar. 15, 2004 to Restriction Requirement mailed Sep. 23, 2003”, 1 pg.
“U.S. Appl. No. 10/271,334, Response filed Nov. 22, 2004 to Non Final Office Action mailed May 18, 2004”, 6 pgs.
“U.S. Appl. No. 10/271,334, Restriction Requirement mailed Sep. 23, 2003”, 4 pgs.
“U.S. Appl. No. 10/271,334, Supplemental Response filed Jan. 28, 2005 to Non Final Office Action mailed May 18, 2004”, 6 pgs.
“U.S. Appl. No. 10/307,226, 312 Amendment filed Oct. 24, 2011”, 3 pgs.
“U.S. Appl. No. 10/307,226, Appeal Brief filed Oct. 14, 2010”, 15 pgs.
“U.S. Appl. No. 10/307,226, Final Office Action mailed Jun. 27, 2008”, 6 pgs.
“U.S. Appl. No. 10/307,226, Final Office Action mailed Dec. 12, 2006”, 5 pgs.
“U.S. Appl. No. 10/307,226, Non Final Office Action mailed Mar. 13, 2006”, 6 pgs.
“U.S. Appl. No. 10/307,226, Non Final Office Action mailed Jun. 12, 2007”, 5 pgs.
“U.S. Appl. No. 10/307,226, Non Final Office Action mailed Sep. 9, 2009”, 16 pgs.
“U.S. Appl. No. 10/307,226, Notice of Allowance mailed Jul. 22, 2011”, 8 pgs.
“U.S. Appl. No. 10/307,226, Preliminary Amendment filed Jul. 22, 2005”, 3 pgs.
“U.S. Appl. No. 10/307,226, PTO Response to 312 Amendment mailed Nov. 10, 2011”, 3 pgs.
“U.S. Appl. No. 10/307,226, Response filed Apr. 9, 2007 to Final Office Action mailed Dec. 12, 2006”, 7 pgs.
“U.S. Appl. No. 10/307,226, Response filed Jun. 23, 2009 to Final Office Action mailed Jun. 27, 2008”, 10 pgs.
“U.S. Appl. No. 10/307,226, Response filed Sep. 15, 2006 to Non Final Office Action mailed Mar. 13, 2006”, 6 pgs.
“U.S. Appl. No. 10/307,226, Response filed Dec. 14, 2007 to Non Final Office Action mailed Jun. 12, 2007”, 7 pgs.
“U.S. Appl. No. 10/669,881, Final Office Action mailed Jan. 25, 2008”, 7 pgs.
“U.S. Appl. No. 10/669,881, Non Final Office Action mailed Jan. 27, 2006”, 5 pgs.
“U.S. Appl. No. 10/669,881, Notice of Allowance mailed Oct. 8, 2008”, 16 pgs.
“U.S. Appl. No. 10/669,881, Preliminary Amendment May 6, 2005”, 3 pgs.
“U.S. Appl. No. 10/669,881, Response filed Mar. 11, 2008 to Final Office Action mailed Jan. 25, 2008”, 8 pgs.
“U.S. Appl. No. 10/669,881, Response filed May 15, 2006 to Non Final Office Action mailed Jan. 27, 2006”, 9 pgs.
“U.S. Appl. No. 10/669,881, Response filed Sep. 7, 2007 to Restriction Requirement mailed Jun. 19, 2007”, 4 pgs.
“U.S. Appl. No. 10/669,881, Response filed Oct. 2, 2006 to Restriction Requirement mailed Jul. 27, 2006”, 6 pgs.
“U.S. Appl. No. 10/669,881, Restriction Requirement Jul. 27, 2006”, 5 pgs.
“U.S. Appl. No. 10/669,881, Restriction Requirement mailed Jun. 19, 2007”, 5 pgs.
“U.S. Appl. No. 10/692,282, Non Final Office Action mailed Aug. 30, 2005”, 6 pgs.
“U.S. Appl. No. 10/692,282, Notice of Allowance mailed Jun. 13, 2006”, 6 pgs.
“U.S. Appl. No. 10/692,282, Response filed Feb. 22, 2005 to Restriction Requirement mailed Aug. 17, 2004”, 4 pgs.
“U.S. Appl. No. 10/692,282, Response filed Feb. 28, 2006 to Non Final Office Action mailed Aug. 30, 2005”, 5 pgs.
“U.S. Appl. No. 10/692,282, Restriction Requirement mailed Aug. 17, 2004”, 6 pgs.
“U.S. Appl. No. 10/693,255, Examiner Interview Summary mailed Feb. 17, 2005”, 3 pgs.
“U.S. Appl. No. 10/693,255, Non Final Office Action mailed Dec. 9, 2004”, 6 pgs.
“U.S. Appl. No. 10/693,255, Notice of Allowance mailed Mar. 9, 2005”, 9 pgs.
“U.S. Appl. No. 10/693,255, Response filed Feb. 17, 2005 to Non Final Office Action mailed Dec. 9, 2004”, 6 pgs.
“U.S. Appl. No. 10/752,435, Final Office Action mailed May 14, 2010”, 8 pgs.
“U.S. Appl. No. 10/752,435, Final Office Action mailed Jul. 12, 2007”, 8 pgs.
“U.S. Appl. No. 10/752,435, Final Office Action mailed Dec. 8, 2008”, 8 pgs.
“U.S. Appl. No. 10/752,435, Non Final Office Action mailed Mar. 18, 2008”, 7 pgs.
“U.S. Appl. No. 10/752,435, Non Final Office Action mailed Jul. 21, 2009”, 7 pgs.
“U.S. Appl. No. 10/752,435, Non Final Office Action mailed Oct. 19, 2006”, 17 pgs.
“U.S. Appl. No. 10/752,435, Response filed Jan. 9, 2008 to Final Office Action mailed Jul. 12, 2007”, 10 pgs.
“U.S. Appl. No. 10/752,435, Response filed Jan. 25, 2010 to Non Final Office Action mailed Jul. 21, 2009”, 9 pgs.
“U.S. Appl. No. 10/752,435, Response filed Apr. 9, 2007 to Non Final Office Action mailed Oct. 19, 2006”, 13 pgs.
“U.S. Appl. No. 10/752,435, Response filed May 12, 2009 to Final Office Action mailed Dec. 8, 2008”, 9 pgs.
“U.S. Appl. No. 10/752,435, Response filed Sep. 19, 2008 to Non Final Office Action mailed Mar. 18, 2008”, 7 pgs.
“U.S. Appl. No. 10/786,465, Applicant's Summary of Examiner Interview filed Jun. 6, 2012”, 2 pgs.
“U.S. Appl. No. 10/786,465, Corrected Notice of Allowability mailed Jul. 2, 2012”, 4 pgs.
“U.S. Appl. No. 10/786,465, Examiner Interview Summary mailed Mar. 3, 2008”, 2 pgs.
“U.S. Appl. No. 10/786,465, Examiner Interview Summary mailed Apr. 26, 2011”, 3 pgs.
“U.S. Appl. No. 10/786,465, Final Office Action mailed Jan. 21, 2009”, 8 pgs.
“U.S. Appl. No. 10/786,465, Non Final Office Action mailed Mar. 26, 2010”, 8 pgs.
“U.S. Appl. No. 10/786,465, Non Final Office Action mailed Jul. 23, 2007”, 7 pgs.
“U.S. Appl. No. 10/786,465, Notice of Allowance mailed Mar. 14, 2012”, 11 pgs.
“U.S. Appl. No. 10/786,465, Preliminary Amendment filed May 16, 2005”, 3 pgs.
“U.S. Appl. No. 10/786,465, Response filed Jan. 25, 2008 to Non Final Office Action mailed Jul. 23, 2007”, 8 pgs.
“U.S. Appl. No. 10/786,465, Response filed Apr. 9, 2007 to Restriction Requirement mailed Dec. 8, 2006”, 4 pgs.
“U.S. Appl. No. 10/786,465, Response filed Apr. 26, 2011 to Non Final Office Action mailed Mar. 26, 2010”, 14 pgs.
“U.S. Appl. No. 10/786,465, Response filed Jul. 22, 2009 to Final Office Action mailed Jan. 21, 2009”, 5 pgs.
“U.S. Appl. No. 10/786,465, Response filed Sep. 19, 2008 to Restriction Requirement mailed Jul. 24, 2008”, 4 pgs.
“U.S. Appl. No. 10/786,465, Restriction Requirement mailed Jul. 24, 2008”, 5 pgs.
“U.S. Appl. No. 10/786,465, Restriction Requirement mailed Dec. 8, 2006”, 6 pgs.
“U.S. Appl. No. 10/786,465, Supplemental Amendment filed Mar. 18, 2008”, 8 pgs.
“U.S. Appl. No. 10/786,465, Supplemental Notice of Allowability mailed May 8, 2012”, 6 pgs.
“U.S. Appl. No. 10/808,216, Preliminary Amendment filed Jun. 15, 2005”, 3 pgs.
“U.S. Appl. No. 11/166,411, 312 Amendment filed Nov. 23, 2011”, 3 pgs.
“U.S. Appl. No. 11/166,411, Final Office Action mailed Dec. 3, 2009”, 5 pgs.
“U.S. Appl. No. 11/166,411, Non Final Office Action mailed May 5, 2009”, 8 pgs.
“U.S. Appl. No. 11/166,411, Notice of Allowance mailed Jan. 6, 2011”, 4 pgs.
“U.S. Appl. No. 11/166,411, Notice of Allowance mailed Aug. 23, 2011”, 5 pgs.
“U.S. Appl. No. 11/166,411, Preliminary Amendment filed Oct. 2, 2006”, 5 pgs.
“U.S. Appl. No. 11/166,411, PTO Response to 312 Communication mailed Dec. 13, 2011”, 2 pgs.
“U.S. Appl. No. 11/166,411, Response filed Jan. 12, 2009 to Restriction Requirement mailed Jul. 15, 2008”, 5 pgs.
“U.S. Appl. No. 11/166,411, Response filed Jun. 7, 2010 to Final Office Action mailed Dec. 3, 2009”, 5 pgs.
“U.S. Appl. No. 11/166,411, Response filed Nov. 9, 2009 to Non Final Office Action mailed May 5, 2009”, 8 pgs.
“U.S. Appl. No. 11/166,411, Restriction Requirement mailed Jul. 15, 2008”, 5 pgs.
“U.S. Appl. No. 11/166,411, Supplemental Preliminary Amendment filed Oct. 30, 2007”, 7 pgs.
“U.S. Appl. No. 11/166,428, Final Office Action mailed Jan. 12, 2009”, 10 pgs.
“U.S. Appl. No. 11/166,428, Final Office Action mailed Mar. 16, 2010”, 8 pgs.
“U.S. Appl. No. 11/166,428, Non Final Office Action mailed May 14, 2008”, 6 pgs.
“U.S. Appl. No. 11/166,428, Non Final Office Action mailed Jun. 16, 2009”, 10 pgs.
“U.S. Appl. No. 11/166,428, Response filed May 12, 2009 to Final Office Action mailed Jan. 12, 2009”, 6 pgs.
“U.S. Appl. No. 11/166,428, Response filed Nov. 17, 2008 to Non Final Office Action mailed May 14, 2008”, 6 pgs.
“U.S. Appl. No. 11/166,428, Response filed Dec. 22, 2009 to Non Final Office Action mailed Dec. 16, 2009”, 8 pgs.
“U.S. Appl. No. 11/254,444, Notice of Allowance mailed Mar. 9, 2010”, 7 pgs.
“U.S. Appl. No. 11/254,444, Notice of Allowance mailed Apr. 5, 2010”, 4 pgs.
“U.S. Appl. No. 11/254,444, Notice of Allowance mailed Jun. 29, 2010”, 6 pgs.
“U.S. Appl. No. 11/254,444, Preliminary Amendment filed Oct. 20, 2005”, 8 pgs.
“U.S. Appl. No. 11/254,444, Preliminary Amendment filed Nov. 15, 2005”, 8 pgs.
“U.S. Appl. No. 11/254,444, Response filed Dec. 18, 2009 to Restriction Requirement mailed Jun. 19, 2009”, 2 pgs.
“U.S. Appl. No. 11/254,444, Restriction Requirement mailed Jun. 19, 2009”, 6 pgs.
“U.S. Appl. No. 11/254,619, Final Office Action mailed Jun. 30, 2010”, 11 pgs.
“U.S. Appl. No. 11/254,619, Final Office Action mailed Oct. 20, 2011”, 12 pgs.
“U.S. Appl. No. 11/254,619, Non Final Office Action mailed Feb. 3, 2011”, 9 pgs.
“U.S. Appl. No. 11/254,619, Non Final Office Action mailed Oct. 1, 2009”, 6 pgs.
“U.S. Appl. No. 11/254,619, Response filed Apr. 1, 2010 to Non Final Office Action mailed Oct. 1, 2009”, 5 pgs.
“U.S. Appl. No. 11/254,619, Response filed Apr. 20, 2012 to Final Office Action mailed Oct. 20, 2011”, 11 pgs.
“U.S. Appl. No. 11/254,619, Response filed Aug. 3, 2011 to Non Final Office Action mailed Feb. 3, 2011”, 13 pgs.
“U.S. Appl. No. 11/254,619, Response filed Dec. 29, 2010 to Final Office Action mailed Jun. 30, 2010”, 12 pgs.
“U.S. Appl. No. 11/254,950, Non Final Office Action mailed Mar. 30, 2009”, 6 pgs.
“U.S. Appl. No. 11/254,950, Notice of Allowance mailed Feb. 26, 2010”, 4 pgs.
“U.S. Appl. No. 11/254,950, Notice of Allowance mailed Jun. 22, 2010”, 4 pgs.
“U.S. Appl. No. 11/254,950, Preliminary Amendment filed Nov. 18, 2005”, 4 pgs.
“U.S. Appl. No. 11/254,950, Response filed Jan. 5, 2009 to Restriction Requirement mailed Jul. 9, 2008”, 7 pgs.
“U.S. Appl. No. 11/254,950, Response filed Oct. 5, 2009 to Non Final Office Action mailed Mar. 30, 2009”, 5 pgs.
“U.S. Appl. No. 11/254,950, Restriction Requirement mailed Jul. 9, 2008”, 9 pgs.
“U.S. Appl. No. 11/255,116, Non Final Office Action mailed May 14, 2008”, 15 pgs.
“U.S. Appl. No. 11/255,116, Notice of Allowance mailed Aug. 10, 2009”, 4 pgs.
“U.S. Appl. No. 11/255,116, Preliminary Amendment filed Nov. 18, 2005”, 4 pgs.
“U.S. Appl. No. 11/255,116, Response filed May 20, 2009 to Restriction Requirement mailed Mar. 18, 2009”, 4 pgs.
“U.S. Appl. No. 11/255,116, Response filed Nov. 17, 2008 to Non Final Office Action mailed May 24, 2008”, 7 pgs.
“U.S. Appl. No. 11/255,116, Restriction Requirement mailed Mar. 18, 2009”, 7 pgs.
“U.S. Appl. No. 11/365,056, Final Office Action mailed Dec. 9, 2010”, 13 pgs.
“U.S. Appl. No. 11/365,056, Non Final Office Action mailed Mar. 23, 2010”, 11 pgs.
“U.S. Appl. No. 11/365,056, Response filed Sep. 28, 2010 to Non Final Office Action mailed Mar. 23, 20100”, 5 pgs.
“U.S. Appl. No. 11/365,056, Response filed Dec. 10, 2009 to Restriction Requirement mailed Jun. 10, 2009”, 44 pgs.
“U.S. Appl. No. 11/365,056, Restriction Requirement mailed Jun. 10, 2009”, 5 pgs.
“U.S. Appl. No. 11/488,305, Advisory Action mailed Jun. 7, 2013”, 3 pgs.
“U.S. Appl. No. 11/488,305, Final Office Action mailed Mar. 6, 2013”, 9 pgs.
“U.S. Appl. No. 11/488,305, Final Office Action mailed Apr. 13, 2011”, 9 pgs.
“U.S. Appl. No. 11/488,305, Non Final Office Action mailed Sep. 1, 2010”, 8 pgs.
“U.S. Appl. No. 11/488,305, Non Final Office Action mailed Sep. 14, 2012”, 9 pgs.
“U.S. Appl. No. 11/488,305, Non Final Office Action mailed Oct. 31, 2011”, 6 pgs.
“U.S. Appl. No. 11/488,305, Response filed Feb. 1, 2011 to Non Final Office Action mailed Sep. 1, 2010”, 12 pgs.
“U.S. Appl. No. 11/488,305, Response filed Feb. 13, 2013 to Non Final Office Action mailed Sep. 14, 2012”, 10 pgs.
“U.S. Appl. No. 11/488,305, Response filed Apr. 26, 2012 to Non Final Office Action mailed Oct. 31, 2011”, 12 pgs.
“U.S. Appl. No. 11/488,305, Response filed May 3, 2013 to Final Office Action mailed Mar. 6, 2013”, 11 pgs.
“U.S. Appl. No. 11/488,305, Response filed Jul. 2, 2010 to Restriction Requirement mailed Jan. 5, 2010”, 8 pgs.
“U.S. Appl. No. 11/488,305, Response filed Oct. 13, 2011 to Final Office Action mailed Apr. 13, 2011”, 11 pgs.
“U.S. Appl. No. 11/488,305, Restriction Requirement mailed Jan. 5, 2010”, 6 pgs.
“U.S. Appl. No. 11/540,427, Appeal Brief filed Aug. 26, 2010”, 26 pgs.
“U.S. Appl. No. 11/540,427, Final Office Action mailed Jul. 21, 2009”, 9 pgs.
“U.S. Appl. No. 11/540,427, Non Final Office Action mailed Oct. 6, 2008”, 10 pgs.
“U.S. Appl. No. 11/540,427, Notice of Allowance mailed Apr. 11, 2011”, 8 pgs.
“U.S. Appl. No. 11/540,427, Notice of Allowance mailed Apr. 29, 2011”, 8 pgs.
“U.S. Appl. No. 11/540,427, Preliminary Amendment filed Oct. 3, 2007”, 5 pgs.
“U.S. Appl. No. 11/540,427, Response filed Apr. 10, 2009 to Non Final Office Action mailed Oct. 6, 2008”, 6 pgs.
“U.S. Appl. No. 11/540,428, Final Office Action mailed Aug. 4, 2011”, 9 pgs.
“U.S. Appl. No. 11/540,428, Non Final Office Action mailed Nov. 12, 2010”, 8 pgs.
“U.S. Appl. No. 11/540,428, Response filed May 12, 2011 to Non Final Office Action mailed Nov. 12, 2010”, 12 pgs.
“U.S. Appl. No. 11/540,428, Response filed Oct. 1, 2010 to Restriction Requirement mailed Mar. 29, 2010”, 6 pgs.
“U.S. Appl. No. 11/540,428, Restriction Requirement mailed Mar. 29, 2010”, 9 pgs.
“U.S. Appl. No. 11/580,584, Appeal Brief filed Nov. 15, 2010”, 11 pgs.
“U.S. Appl. No. 11/580,584, Final Office Action mailed Jan. 22, 2009”, 9 pgs.
“U.S. Appl. No. 11/580,584, Final Office Action mailed Oct. 16, 2009”, 8 pgs.
“U.S. Appl. No. 11/580,584, Non Final Office Action mailed Apr. 18, 2008”, 6 pgs.
“U.S. Appl. No. 11/580,584, Notice of Allowance mailed Feb. 4, 2011”, 7 pgs.
“U.S. Appl. No. 11/580,584, Response filed Jul. 22, 2009 to Final Office Action mailed Jan. 22, 2009”, 6 pgs.
“U.S. Appl. No. 11/580,584, Response filed Oct. 20, 2008 to Non Final Office Action mailed Apr. 18, 2008”, 5 pgs.
“U.S. Appl. No. 11/978,752, Final Office Action mailed Dec. 22, 2010”, 6 pgs.
“U.S. Appl. No. 11/978,752, Non Final Office Action mailed May 20, 2010”, 6 pgs.
“U.S. Appl. No. 11/978,752, Notice of Allowance mailed Aug. 31, 2011”, 5 pgs.
“U.S. Appl. No. 11/978,752, Response filed May 10, 2010 to Restriction Requirement mailed Nov. 6, 2009”, 4 pgs.
“U.S. Appl. No. 11/978,752, Response filed Jun. 22, 2011 to Final Office Action mailed Dec. 22, 2010”, 6 pgs.
“U.S. Appl. No. 11/978,752, Response filed Nov. 5, 2010 to Non Final Office Action mailed May 20, 2010”, 4 pgs.
“U.S. Appl. No. 11/978,752, Restriction Requirement mailed Nov. 6, 2009”, 7 pgs.
“U.S. Appl. No. 11/978,753, Final Office Action mailed May 2, 2011”, 8 pgs.
“U.S. Appl. No. 11/978,753, Non Final Office Action mailed Sep. 3, 2010”, 8 pgs.
“U.S. Appl. No. 11/978,753, Response filed Mar. 3, 2011 to Non Final Office Action mailed Sep. 3, 2010”, 9 pgs.
“U.S. Appl. No. 11/981,112, Final Office Action mailed Apr. 29, 2010”, 9 pgs.
“U.S. Appl. No. 11/981,112, Final Office Action mailed Oct. 8, 2013”, 9 pgs.
“U.S. Appl. No. 11/981,112, Non Final Office Action mailed Jul. 8, 2009”, 11 pgs.
“U.S. Appl. No. 11/981,112, Response filed Jan. 6, 2010 to Non Final Office Action mailed Jul. 8, 2009”, 7 pgs.
“U.S. Appl. No. 11/981,112, Response filed Nov. 1, 2010 to Final Office Action mailed Apr. 29, 2010”, 7 pgs.
“U.S. Appl. No. 12/288,031, Advisory Action mailed Apr. 12, 2013”, 3 pgs.
“U.S. Appl. No. 12/288,031, Final Office Action mailed Jan. 3, 2012”, 9 pgs.
“U.S. Appl. No. 12/288,031, Non Final Office Action mailed May 10, 2012”, 8 pgs.
“U.S. Appl. No. 12/288,031, Non Final Office Action mailed Jul. 15, 2013”, 9 pgs.
“U.S. Appl. No. 12/288,031, Response filed Mar. 25, 2013 to Final Office Action mailed Jan. 3, 2013”, 11 pgs.
“U.S. Appl. No. 12/288,031, Response filed Apr. 4, 2012 to Restriction Requirement mailed Nov. 4, 2011”, 3 pgs.
“U.S. Appl. No. 12/288,031, Response filed Oct. 10, 2012 to Non Final Office Action mailed May 10, 2012”, 11 pgs.
“U.S. Appl. No. 12/288,031, Restriction Requirement mailed Nov. 4, 2011”, 9 pgs.
“U.S. Appl. No. 12/288,032, Restriction Requirement mailed Nov. 4, 2011”, 9 pgs.
“U.S. Appl. No. 12/288,034, Final Office Action mailed Nov. 4, 2013”, 8 pgs.
“U.S. Appl. No. 12/288,034, Non Final Office Action mailed Jun. 22, 2012”, 7 pgs.
“U.S. Appl. No. 12/288,034, Response filed May 1, 2012 to Restriction Requirement mailed Nov. 3, 2011”, 4 pgs.
“U.S. Appl. No. 12/288,034, Response filed Dec. 21, 2012 to Non Final Office Action mailed Jun. 22, 2012”, 12 pgs.
“U.S. Appl. No. 12/288,034, Restriction Requirement mailed Nov. 3, 2011”, 9 pgs.
“U.S. Appl. No. 12/288,045, Restriction Requirement mailed Nov. 16, 2011”, 9 pgs.
“U.S. Appl. No. 12/315,015, Advisory Action mailed Sep. 12, 2012”, 3 pgs.
“U.S. Appl. No. 12/315,015, Final Office Action mailed Apr. 26, 2012”, 7 pgs.
“U.S. Appl. No. 12/315,015, Non Final Office Action mailed Sep. 27, 2013”, 7 pgs.
“U.S. Appl. No. 12/315,015, Non Final Office Action mailed Oct. 6, 2011”, 11 pgs.
“U.S. Appl. No. 12/315,015, Preliminary Amendment filed Mar. 10, 2009”, 3 pgs.
“U.S. Appl. No. 12/315,015, Response filed Apr. 6, 2012 to Non Final Office Action mailed Oct. 6, 2011”, 12 pgs.
“U.S. Appl. No. 12/315,015, Response filed Aug. 27, 2012 to Final Office Action mailed Apr. 26, 2012”, 6 pgs.
“U.S. Appl. No. 12/653,219, Non Final Office Action mailed May 30, 2012”, 16 pgs.
“U.S. Appl. No. 12/917,842, Non Final Office Action mailed Nov. 13, 2012”, 6 pgs.
“U.S. Appl. No. 12/917,842, Notice of Allowance mailed May 20, 2013”, 8 pgs.
“U.S. Appl. No. 12/917,842, Notice of Allowance mailed Aug. 27, 2013”, 6 pgs.
“U.S. Appl. No. 12/917,842, Response filed Apr. 15, 2013 to Non Final Office Action mailed Nov. 13, 2012”, 9 pgs.
“U.S. Appl. No. 12/917,842, Response filed Oct. 15, 2012 to Restriction Requirement mailed Sep. 14, 2012”, 2 pgs.
“U.S. Appl. No. 12/917,842, Restriction Requirement mailed Sep. 14, 2012”, 5 pgs.
“U.S. Appl. No. 12/942,232, Non Final Office Action mailed Oct. 9, 2013”, 13 pgs.
“U.S. Appl. No. 13/157,242, Advisory Action mailed Jul. 30, 2013”, 3 pgs.
“U.S. Appl. No. 13/157,242, Final Office Action mailed May 16, 2013”, 7 pgs.
“U.S. Appl. No. 13/157,242, Non Final Office Action mailed Jun. 18, 2012”, 9 pgs.
“U.S. Appl. No. 13/157,242, Non Final Office Action mailed Oct. 31, 2013”, 6 pgs.
“U.S. Appl. No. 13/157,242, Preliminary Amendment filed Jun. 9, 2011”, 7 pgs.
“U.S. Appl. No. 13/157,242, Response filed Jun. 1, 2012 to Restriction Requirement mailed May 1, 2012”, 3 pgs.
“U.S. Appl. No. 13/157,242, Response filed Jul. 16, 2013 to Final Office Action mailed May 16, 2013”, 9 pgs.
“U.S. Appl. No. 13/157,242, Response filed Dec. 18, 2012 to Non Final Office Action mailed Jun. 18, 2012”, 11 pgs.
“U.S. Appl. No. 13/157,242, Restriction Requirement mailed May 1, 2012”, 6 pgs.
“U.S. Appl. No. 13/162,384, Final Office Action mailed Aug. 27, 2013”, 14 pgs.
“U.S. Appl. No. 13/162,384, Non Final Office Action mailed Mar. 28, 2013”, 8 pgs.
“U.S. Appl. No. 13/162,384, Preliminary Amendment filed Jun. 16, 2011”, 7 pgs.
“U.S. Appl. No. 13/162,384, Response filed Jun. 27, 2013”, 9 pgs.
“U.S. Appl. No. 13/162,384, Response filed Oct. 18, 2013 to Final Office Action mailed Aug. 27, 2013”, 5 pgs.
“Australian Application Serial No. 2002351188, Office Action mailed Mar. 30, 2007”, 1 pg.
“Australian Application Serial No. 2002351188, Office Action mailed Dec. 8, 2008”, 3 pgs.
“Australian Application Serial No. 2004277897, First Examiner Report mailed Oct. 14, 2009”, 2 pgs.
“Australian Application Serial No. 2004277897, Response filed Jul. 14, 2011 to First Examiner Report mailed Oct. 14, 2009”, 9 pgs.
“Australian Application Serial No. 2004287354, Office Action mailed Oct. 13, 2009”, 2 pgs.
“Australian Application Serial No. 2004287355, Office Action mailed May 11, 2009”, 2 pgs.
“Australian Application Serial No. 2005204615, Office Action mailed Jan. 20, 2010”, 4 pgs.
“Australian Application Serial No. 2005235108, Office Action mailed Feb. 26, 2010”, 3 pgs.
“Australian Application Serial No. 2006302908, Office Action mailed Mar. 4, 2011”, 8 pgs.
“Australian Application Serial No. 2006305688, First Examiner Report mailed Mar. 10, 2011”, 3 pgs.
“Australian Application Serial No. 2006305688, Response filed Oct. 22, 2012 to First Examiner Report mailed Mar. 10, 2011”, 16 pgs.
“Australian Application Serial No. 2006305689, Office Action mailed Sep. 5, 2011”, 3 pgs.
“Australian Application Serial No. 2006309241, Office Action mailed Mar. 4, 2011”, 6 pgs.
“Australian Application Serial No. 2011224089, First Examiners Report mailed Mar. 27, 2013”, 3 pgs.
“Australian Application Serial No. 2011253682, Office Action mailed Sep. 27, 2012”, 4 pgs.
“Australian Application Serial No. 2011253682, Response filed Jul. 17, 2013 to Office Action mailed Sep. 27, 2012”, 19 pgs.
“Canadian Application Serial No. 2,464,900, Office Action mailed Sep. 29, 2009”, 3 pgs.
“Canadian Application Serial No. 2,539,585, Office Action mailed Aug. 31, 2010”, 2 pgs.
“Canadian Application Serial No. 2,539,585, Office Action mailed Sep. 19, 2012”, 2 pgs.
“Canadian Application Serial No. 2,546,681, Office Action mailed Feb. 25, 2011”, 3 pgs.
“Canadian Application Serial No. 2,546,721, Office Action mailed Feb. 25, 2011”, 3 pgs.
“Canadian Application Serial No. 2,551,685, Office Action mailed Jan. 17, 2011”, 3 pgs.
“Canadian Application Serial No. 2,554,022, Office Action mailed Jun. 22, 2011”, 3 pgs.
“Canadian Application Serial No. 2,554,022, Office Action mailed Aug. 31, 2010”, 2 pgs.
“Canadian Application Serial No. 2,558,317, Office Action mailed Aug. 31, 2010”, 2 pgs.
“Canadian Application Serial No. 2,558,317, Office Action mailed Sep. 28, 2011”, 3 pgs.
“Canadian Application Serial No. 2,626,403, Office Action mailed Apr. 2, 2013”, 3 pgs.
“Chinese Application Serial No. 02823581.9, Office Action mailed Mar. 1, 2006”, 7 pgs.
“Chinese Application Serial No. 02823581.9, Office Action mailed Apr. 18, 2008”, 6 pgs.
“Chinese Application Serial No. 02823581.9, Office Action mailed Aug. 8, 2007”, 4 pgs.
“Chinese Application Serial No. 02823581.9, Office Action mailed Nov. 17, 2006”, 7 pgs.
“Chinese Application Serial No. 02823581.9, Response filed Jan. 31, 2007 to Office Action mailed Nov. 17, 2006”, 8 pgs.
“Chinese Application Serial No. 02823581.9, Response filed Apr. 7, 2006 to Office Action mailed Mar. 1, 2006”, 4 pgs.
“Chinese Application Serial No. 02823581.9, Response filed May 19, 2008 to Office Action mailed Apr. 18, 2008”, (W/ English Translation), 38 pgs.
“Chinese Application Serial No. 02823581.9, Response filed Dec. 3, 2007 to Office Action mailed Aug. 8, 2007”, 6 pgs.
“Chinese Application Serial No. 200480027649.7, Office Action mailed Jun. 23, 2008”, w/English translation, 5 pgs.
“Chinese Application Serial No. 200480027649.7, Office Action mailed Sep. 4, 2009”, w/English translation, 18 pgs.
“Chinese Application Serial No. 200480027649.7, Office Action mailed Dec. 24, 2010”, w/English translation, 6 pgs.
“Chinese Application Serial No. 200480027649.7, Response filed Jan. 19, 2010 to Office Action mailed Sep. 4, 2009”, 5 pgs.
“Chinese Application Serial No. 200480027649.7, Response filed Mar. 8, 2011 to Office Action mailed Dec. 24, 2010”, w/English translation, 7 pgs.
“Chinese Application Serial No. 200480031226.2, Office Action mailed Jan. 23, 2009”, 9 pgs.
“Chinese Application Serial No. 200480031226.2, Office Action mailed Apr. 27, 2010”, (W/ English Translation), 7 pgs.
“Chinese Application Serial No. 200480031226.2, Office Action mailed Dec. 21, 2010”, (W/ English Translation), 10 pgs.
“Chinese Application Serial No. 200480031226.2, Response filed Feb. 25, 2011 to Office Action mailed Dec. 21, 2010”, (W/ English Translation), 18 pgs.
“Chinese Application Serial No. 200480031226.2, Response filed May 22, 2009 to Office Action mailed Jan. 23, 2009”, 5 pgs.
“Chinese Application Serial No. 200480031226.2, Response filed Jul. 12, 2010 to Office Action mailed Apr. 27, 2010”, 5 pgs.
“Chinese Application Serial No. 200580002026.9, Office Action mailed Jun. 19, 2009”, (W/ English Translation), 12 pgs.
“Chinese Application Serial No. 200580002026.9, Response filed Jan. 4, 2010 to Office Action mailed Jun. 19, 2009”, 10 pgs.
“Chinese Application Serial No. 200580006169.7, Office Action mailed Mar. 1, 2010”, w/English translation, 12 pgs.
“Chinese Application Serial No. 200580006169.7, Response filed Jul. 14, 2010 to Office Action mailed Mar. 1, 2010”, w/English translation, 32 pgs.
“Chinese Application Serial No. 200580009570.6, Office Action mailed May 9, 2008”, (W/ English Translation), 2 pgs.
“Chinese Application Serial No. 200580009570.6, Response filed Nov. 21, 2008 to Office Action mailed May 9, 2008”, 7 pgs.
“Chinese Application Serial No. 200680034052.4, Office Action mailed May 11, 2010”, w/English translation, 7 pgs.
“Chinese Application Serial No. 200680034052.4, Office Action mailed Aug. 14, 2009”, w/English translation, 13 pgs.
“Chinese Application Serial No. 200680034052.4, Response filed Mar. 1, 2010 to Office Action mailed Aug. 14, 2009”, 4 pgs.
“Chinese Application Serial No. 200680034052.4, Response filed Sep. 26, 2010 to Office Action mailed May 11, 2010”, 5 pgs.
“Chinese Application Serial No. 200680038882.4, Office Action mailed May 11, 2010”, (W/ English Translation), 18 pgs.
“Chinese Application Serial No. 200680046854.7, Office Action mailed Apr. 14, 2010”, (W/ English Translation), 18 pgs.
“Chinese Application Serial No. 200680046854.7, Response filed Sep. 26, 2010 to Office Action mailed Apr. 14, 2010”, 10 pgs.
“Chinese Application Serial No. 200680047552.1, Office Action mailed Jun. 4, 2010”, (W/ English Translation), 7 pgs.
“Chinese Application Serial No. 200680047552.1, Response filed Dec. 20, 2010 to Office Action mailed Jun. 4, 2010”, 10 pgs.
“Chinese Application Serial No. 200910139527.1, Office Action mailed Jul. 12, 2010”, w/English translation, 9 pgs.
“Chinese Application Serial No. 200910139527.1, Response filed Nov. 28, 2011 to Office Action mailed Jul. 12, 2010”, 9 pgs.
“European Application Serial No. 04788653.6, Office Action mailed May 19, 2006”, 2 pgs.
“European Application Serial No. 05704902.5, European Search Report mailed Aug. 29, 2011”, 3 pgs.
“European Application Serial No. 05713941.2, Office Action mailed Dec. 13, 2007”, 2 pgs.
“European Application Serial No. 06802573.3, Extended European Search Report mailed Feb. 15, 2012”, 6 pgs.
“European Application Serial No. 06802573.3, Office Action mailed Mar. 5, 2012”, 1 pg.
“European Application Serial No. 06802573.3, Office Action mailed May 28, 2008”, 2 pgs.
“European Application Serial No. 06802573.3, Response filed Sep. 3, 2012 to Office Action mailed Mar. 5, 2012”, 15 pgs.
“European Application Serial No. 06802578.2, European Search Report mailed Mar. 7, 2013”, 10 pgs.
“European Application Serial No. 06802580.8, Office Action mailed Feb. 25, 2013”, 3 pgs.
“European Application Serial No. 09075319.5, Extended European Search Report mailed Oct. 14, 2009”, 6 pgs.
“European Application Serial No. 09075319.5, Office Action mailed Jan. 14, 2010”, 1 pgs.
“European Application Serial No. 09075319.5, Office Action mailed Oct. 14, 2010”, 4 pgs.
“European Application Serial No. 09820886.1, Office Action mailed Jun. 7, 2011”, 2 pgs.
“European Application Serial No. 09820886.1, Response filed Dec. 8, 2011 to Office Action mailed Jun. 7, 2011”, 3 pgs.
“European Application Serial No. 09820891.1, Office Action mailed Jun. 7, 2011”, 2 pgs.
“European Application Serial No. 09820891.1, Response filed Dec. 8, 2011 to Office Action mailed Jun. 7, 2011”, 2 pgs.
“European Application Serial No. 09075319.5, Response filed Feb. 21, 2011 to Office Action mailed Oct. 14, 2010”, 5 pgs.
“European Application Serial No. 09075319.5, Response filed Jul. 20, 2010 to Office Action mailed Jan. 14, 2008”, 13 pgs.
“German Application Serial No. 10297483.7, Office Action mailed Jan. 9, 2006”, 4 pgs.
“German Application Serial No. 10297483.7, Office Action mailed Jul. 8, 2006”, 2 pgs.
“German Application Serial No. 10297483.7, Office Action mailed and Response filed Oct. 30, 2006”, 8 pgs.
“German Application Serial No. 10297483.7, Response filed Jul. 7, 2006 to Office Action mailed Jan. 9, 2006”, 14 pgs.
“German Application Serial No. 10297483.7, Response filed Oct. 26, 2006 to Office Action mailed Jul. 8, 2006”, 3 pgs.
“Great Britain Application Serial No. 0411107.6, Office Action mailed Feb. 28, 2005”, 3 pgs.
“Great Britain Application Serial No. 0411107.6, Office Action mailed Sep. 29, 2005”, 1 pg.
“Great Britain Application Serial No. 0411107.6, Response filed Aug. 23, 2005 to Office Action mailed Feb. 28, 2005”, 3 pgs.
“Great Britain Application Serial No. 0411107.6, Response filed Oct. 31, 2005 to Office Action mailed Sep. 29, 2005”, 4 pgs.
“Great Britain Application Serial No. 0522152.8, Office Action mailed Dec. 5, 2005”, 5 pgs.
“Great Britain Application Serial No. 0522152.8, Response filed Apr. 26, 2006 to Office Action mailed Dec. 5, 2005”, 48 pgs.
“International Application Serial No. PCT/US2002/032753, International Preliminary Examination Report mailed Aug. 16, 2004”, 3 pgs.
“International Application Serial No. PCT/US2002/032753, International Search Report mailed Mar. 6, 2003”, 1 pg.
“International Application Serial No. PCT/US2002/032753, Written Opinion mailed Aug. 26, 2003”, 4 pgs.
“International Application Serial No. PCT/US2002/038365, International Preliminary Report on Patentability mailed Feb. 6, 2004”, 3 pgs.
“International Application Serial No. PCT/US2002/038365, International Search Report mailed May 8, 2003”, 3 pgs.
“International Application Serial No. PCT/US2002/038365, Written Opinion mailed Oct. 27, 2003”, 4 pgs.
“International Application Serial No. PCT/US2004/027589, International Preliminary Report on Patentability mailed Apr. 6, 2005”, 4 pgs.
“International Application Serial No. PCT/US2004/027589, International Search Report mailed Apr. 6, 2005”, 1 pg.
“International Application Serial No. PCT/US2004/027589, Written Opinion mailed Apr. 6, 2005”, 3 pgs.
“International Application Serial No. PCT/US2004/027590, International Preliminary Examination Report mailed Feb. 2, 16, 2006”, 3 pgs.
“International Application Serial No. PCT/US2004/027590, International Search Report mailed Jan. 12, 2005”, 1 pg.
“International Application Serial No. PCT/US2004/027590, Written Opinion mailed Jan. 12, 2005”, 3 pgs.
“International Application Serial No. PCT/US2004/029402, International Preliminary Report on Patentability mailed Jul. 10, 2006”, 3 pgs.
“International Application Serial No. PCT/US2004/029402, International Search Report mailed Feb. 24, 2006”, 1 pg.
“International Application Serial No. PCT/US2004/029402, Written Opinion mailed Feb. 24, 2006”, 3 pgs.
“International Application Serial No. PCT/US2005/00059, International Preliminary Report on Patentability mailed May 18, 2007”, 8 pgs.
“International Application Serial No. PCT/US2005/00059, International Search Report mailed Jan. 5, 2007”, 3 pgs.
“International Application Serial No. PCT/US2005/00059, Written Opinion mailed Jan. 5, 2007”, 8 pgs.
“International Application Serial No. PCT/US2005/005453, International Preliminary Examination Report mailed Mar. 13, 2006”, 3 pgs.
“International Application Serial No. PCT/US2005/005453, International Preliminary Report on Patentability mailed Feb. 16, 2006”, 3 pgs.
“International Application Serial No. PCT/US2005/005453, International Search Report mailed Aug. 30, 2005”, 1 pg.
“International Application Serial No. PCT/US2005/005453, International Written Opinion mailed Aug. 30, 2005”, 3 pgs.
“International Application Serial No. PCT/US2005/005453, Written Opinion mailed Aug. 30, 2005”, 3 pgs.
“International Application Serial No. PCT/US2005/005627, International Preliminary Examination Report mailed Apr. 7, 2009”, 3 pgs.
“International Application Serial No. PCT/US2005/005627, International Search Report mailed Sep. 25, 2007”, 1 pg.
“International Application Serial No. PCT/US2005/005627, Written Opinion mailed Sep. 25, 2007”, 3 pgs.
“International Application Serial No. PCT/US2006/033741, International Preliminary Report on Patentability mailed Jul. 28, 2007”, 5 pgs.
“International Application Serial No. PCT/US2006/033741, International Search Report mailed Mar. 30, 2007”, 1 pg.
“International Application Serial No. PCT/US2006/033741, Written Opinion mailed Mar. 30, 2007”, 4 pgs.
“International Application Serial No. PCT/US2006/033747, International Preliminary Report on Patentability mailed Mar. 1, 2011”, 4 pgs.
“International Application Serial No. PCT/US2006/033747, International Search Report mailed Jul. 8, 2008”, 1 pg.
“International Application Serial No. PCT/US2006/033747, Written Opinion mailed Jul. 8, 2008”, 3 pgs.
“International Application Serial No. PCT/US2006/033748, International Preliminary Report on Patentability mailed Jun. 18, 2008”, 7 pgs.
“International Application Serial No. PCT/US2006/033748, International Search Report mailed Aug. 15, 2007”, 1 pg.
“International Application Serial No. PCT/US2006/033748, Written Opinion mailed Aug. 15, 2007”, 5 pgs.
“International Application Serial No. PCT/US2006/033749, International Preliminary Report on Patentability mailed Jun. 18, 2008”, 6 pgs.
“International Application Serial No. PCT/US2006/033749, International Search Report mailed Aug. 15, 2007”, 1 pg.
“International Application Serial No. PCT/US2006/033749, Written Opinion mailed Aug. 15, 2007”, 5 pgs.
“International Application Serial No. PCT/US2006/037085, International Preliminary Report on Patentability mailed Jul. 24, 2008”, 9 pgs.
“International Application Serial No. PCT/US2006/037085, International Search Report mailed Aug. 30, 2007”, 1 pg.
“International Application Serial No. PCT/US2006/037085, Written Opinion mailed Aug. 30, 2007”, 7 pgs.
“International Application Serial No. PCT/US2009/005604, International Preliminary Report on Patentability mailed Jan. 13, 2011”, 10 pgs.
“International Application Serial No. PCT/US2009/005604, International Search Report mailed Dec. 11, 2009”, 2 pgs.
“International Application Serial No. PCT/US2009/005604, Written Opinion mailed Dec. 11, 2009”, 7 pgs.
“International Application Serial No. PCT/US2009/005607, International Preliminary Report on Patentability mailed Jan. 9, 2011”, 9 pgs.
“International Application Serial No. PCT/US2009/005607, International Search Report mailed Dec. 11, 2009”, 2 pgs.
“International Application Serial No. PCT/US2009/005607, Written Opinion mailed Dec. 11, 2009”, 6 pgs.
“International Application Serial No. PCT/US2009/005608, International Preliminary Report on Patentability mailed Jan. 14, 2011”, 7 pgs.
“International Application Serial No. PCT/US2009/005608, International Search Report mailed Dec. 10, 2009”, 2 pgs.
“International Application Serial No. PCT/US2009/005608, Written Opinion mailed Dec. 10, 2009”, 4 pgs.
“International Application Serial No. PCT/US2009/005609, International Preliminary Report on Patentability mailed Jan. 9, 2011”, 9 pgs.
“International Application Serial No. PCT/US2009/005609, International Search Report mailed Dec. 18, 2009”, 2 pgs.
“International Application Serial No. PCT/US2009/005609, Written Opinion mailed Dec. 18, 2009”, 6 pgs.
“Japanese Application Serial No. 2006-528036, Office Action mailed Jan. 19, 2010”, 3 pgs.
“Japanese Application Serial No. 2006-528036, Office Action mailed Feb. 26, 2009”, w/English translation, 5 pgs.
“Japanese Application Serial No. 2006-528036, Office Action mailed Jun. 23, 2008”, w/English translation, 5 pgs.
“Japanese Application Serial No. 2006-528036, Response filed Dec. 25, 2008 to Office Action mailed Jun. 23, 2008”, w/English translation, 9 pgs.
“Japanese Application Serial No. 2006-536616, Office Action mailed Jun. 23, 2008”, (W/ English Translation), 8 pgs.
“Japanese Application Serial No. 2006-536616, Response filed Dec. 19, 2008 to Office Action mailed Jun. 23, 2008”, (W/ English Translation), 9 pgs.
“Japanese Application Serial No. 2006-536617, Office Action mailed Jun. 17, 2008”, (W/ English Translation), 3 pgs.
“Japanese Application Serial No. 2006-536617, Response filed May 12, 2009 to Office Action mailed Jun. 17, 2008”, (W/ English Translation), 19 pgs.
“Japanese Application Serial No. 2006-547608, Office Action mailed Jun. 23, 2008”, (W/ English Translation), 5 pgs.
“Japanese Application Serial No. 2006-547608, Respone filed Dec. 19, 2008 to Office Action mailed Jun. 23, 2008”, (W/ English Translation), 10 pgs.
“Japanese Application Serial No. 2007500928, Office Action mailed Jul. 1, 2010”, w/English translation, 10 pgs.
“Japanese Application Serial No. 2007504965, Office Action mailed Mar. 7, 2012”, w/English translation, 4 pgs.
“Japanese Application Serial No. 2007504965, Office Action mailed Jun. 14, 2011”, w/English translation, 4 pgs.
“Japanese Application Serial No. 2007504965, Office Action mailed Sep. 14, 2010”, English translation, 1 pg.
“Japanese Application Serial No. 2007504965, Response filed Mar. 11, 2011 to Office Action mailed Sep. 14, 2010”, 8 pgs.
“Japanese Application Serial No. 2008-306790, Office Action mailed May 31, 2011”, 1 pg.
“Japanese Application Serial No. 2008-306790, Response filed Nov. 29, 2011 to Office Action mailed May 8, 2012”, 2 pgs.
“Japanese Application Serial No. 2008-306790, Response filed Nov. 29, 2011 to Office Action mailed May 31, 2011”, (W/ English Translation), 12 pgs.
“Japanese Application Serial No. 2008-316282, Office Action mailed May 16, 2011”, 2 pgs.
“Japanese Application Serial No. 2008-323279, Office Action mailed Sep. 30, 2010”, 1 pg.
“Japanese Application Serial No. 2008-323290, Office Action mailed Jun. 6, 2012”, (W/ English Translation), 8 pgs.
“Japanese Application Serial No. 2008-323290, Office Action mailed Jun. 8, 2011”, (W/ English Translation), 8 pgs.
“Japanese Application Serial No. 2008-323290, Response filed Dec. 7, 2011 to Office Action mailed Jun. 8, 2011”, (W/ English Translation), 16 pgs.
“Japanese Application Serial No. 2008-536574, Office Action mailed Mar. 11, 2010”, (W/ English Translation), 4 pgs.
“Japanese Application Serial No. 2008-536574, Office Action mailed Oct. 3, 2011”, (W/ English Translation), 7 pgs.
“Japanese Application Serial No. 2008-536575, Office Action mailed Jul. 7, 2011”, (W/ English Translation), 5 pgs.
“Japanese Application Serial No. 2008-536576, Office Action mailed Jul. 19, 2011”, (W/ English Translation), 4 pgs.
“Japanese Application Serial No. 2008-536577, Notice of Allowance mailed May 30, 2012”, 3 pgs.
“Japanese Application Serial No. 2008-536577, Office Action mailed Jul. 8, 2011”, w/English translation, 4 pgs.
“Japanese Application Serial No. 2008-536577, Response filed Jan. 6, 2012 to Office Action mailed Jul. 8, 2011”, (W/ English Translation), 3 pgs.
“Laparoscopic Surgery”, Medical Data International, Inc. MedPro, (1995), 190.
Bolduc, Lee, “Devices, Systems, and Methods for Prosthesis Delivery and Implantation, Including the Use of a Fastener Tool”, U.S. Appl. No. 12/917,842, filed Nov. 2, 2010, 120 pgs.
Gadacz, T., et al., “The Spiral Tracker: A New Technique for Stabilizing Prosthetic Mesh in Laparoscopic Hernia Repair”, Surgical Rounds, (Nov. 1995), 461-467.
Hatchett, R. L, et al., “Extraperitoneal Endoscopic Burch Repair Using a Tacker Mesh Technique”, (1995), 1-4.
Newman, L., et al., “Tacker-Assisted TAPP Procedure”, (1995), 2 pgs.
Related Publications (1)
Number Date Country
20120316578 A1 Dec 2012 US
Provisional Applications (2)
Number Date Country
60489011 Jul 2003 US
60333937 Nov 2001 US
Continuations (1)
Number Date Country
Parent 10786465 Feb 2004 US
Child 13495836 US
Continuation in Parts (3)
Number Date Country
Parent 10693255 Oct 2003 US
Child 10786465 US
Parent 10307226 Nov 2002 US
Child 10693255 US
Parent 10271334 Oct 2002 US
Child 10307226 US