Not Applicable
The present invention relates to systems for intraluminally delivering and deploying self-expanding stents and other prostheses, and more particularly to such systems that incorporate mechanisms for retrieving partially deployed prostheses.
Stents, stent-grafts, and other body implantable tubular devices are employed in a wide variety of applications to maintain the patency of body lumens and guide the flow of blood and other body fluids through the lumens. These devices are employed in vascular applications, e.g. in pulmonary and thoracic vessels, and in arteries such as the coronary, renal, carotid, and iliac arteries. In addition to these vascular applications, the devices are used in the esophagus, duodenum, biliary duct, and colon. These devices may be either radially self-expanding or balloon-expandable in character. When deployed within body lumens, self-expanding devices radially expand into contact with surrounding tissue, typically assuming a diameter less than a fully expanded or relaxed state diameter. Consequently, an internal elastic restoring force acts outwardly against the tissue to assist in fixation of the device. Self-expanding devices frequently are preferred, due to this self-fixation capability.
Most applications employing radially self-expanding devices require intraluminal delivery of the device in a configuration suitable for delivery, i.e. radially compressed to a reduced-radius state against its internal elastic restoring force. To this end, prosthesis delivery systems frequently include two catheters: an outer catheter releasably containing the radially compressed prosthesis in a lumen near its distal end, and an inner catheter contained in the lumen, positioned against or otherwise engaged with the prosthesis. The prosthesis is deployed by moving the outer catheter proximally while holding the inner catheter in place. This effectively moves the inner catheter and the prosthesis distally relative to the outer catheter, allowing the prosthesis to radially self-expand as it emerges from the distal end of the outer catheter.
In either event, there arises on occasion a need to reverse the deployment. The need may arise from the physician's desire to reposition the prosthesis along the intended treatment site. Once a substantial portion of the prosthesis is free of the outer catheter, it may be moved in the proximal direction. However, at this point it is virtually impossible to move the prosthesis in the distal direction without retracting it proximally, back into the outer catheter. Accurate positioning of the prosthesis during deployment is challenging, in that it usually requires fluoroscopic imaging, and the difficulty is increased by the tendency of the many self-expanding devices to axially shorten as they radially self-expand. The need to retract a prosthesis can arise from other factors, e.g. a realization during deployment that a prosthesis of a different axial length or radius would be more effective at the designated treatment site.
In many conventional deployment and delivery systems, retraction of a partially deployed prosthesis is virtually impossible. To provide a retractable prosthesis, an inner catheter or other member can be surrounded by a high friction sleeve or gripping member as shown in U.S. Pat. No. 5,026,377 (Burton et al.), with the portion of an inner catheter supporting the sleeve and surrounded by the prosthesis. When the outer catheter radially compresses the prosthesis, it simultaneously presses the prosthesis into a frictional engagement with the sleeve. Accordingly, when the outer catheter is moved relative to the inner catheter, the prosthesis tends to remain with the inner catheter rather than following the outer catheter. A similar approach is shown in U.S. Pat. No. 5,817,102 (Johnson et al.) in which an exterior catheter radially compresses a stent into contact with a restraining sleeve that surrounds an interior catheter.
While these arrangements permit proximal retraction of a partially deployed stent or other prosthesis, they rely on a frictional engagement of the prosthesis with the inner member, through the gripping member or restraining sleeve. The force due to the frictional engagement must be sufficient to overcome the tendency of the prosthesis to move with the outer catheter as the outer catheter moves relative to the inner member. This frictional force acts in the axial direction, but requires a force acting in the radial direction to urge the prosthesis against the gripping member. The required radial force adds to the radial force already exerted by the prosthesis against the outer catheter due to its internal elastic restoring force, thus to increase the axial pushing force required to overcome friction between the prosthesis and outer catheter, and deploy the prosthesis.
Another factor inherent in this approach is the reduction in the frictional holding force as prosthesis deployment progresses, largely due to the diminishing portion of the prosthesis length subject to the frictional hold. As deployment progresses, the prosthesis becomes increasingly easy to deploy. Conversely, when the prosthesis is being pulled back into the catheter to reconstrain it, the reconstrainment force increases as more and more of the prosthesis is pulled into the catheter. This tendency can be counteracted by increasing the frictional holding force, but this in turn increases the radial force required to overcome the frictional hold, once again increasing the force required for ordinary deployment.
Other arrangements involve axially tight or locking engagements of prostheses with inner member coupling structures. Examples of these arrangements are seen in U.S. Pat. No. 6,350,278 (Lenker et al.) and U.S. Pat. No. 5,733,325 (Robinson et al.). These systems permit prosthesis retraction, but impose unduly stringent tolerances upon the coupling structure. Further, they require close attention and care on the part of the physician or other user when loading a prosthesis into the system, to ensure that the required coupling is achieved.
Therefore, the present invention is disclosed in terms of several embodiments, each directed to at least one of the following objects:
To achieve these and other objects, there is provided a device for effecting an intraluminal delivery and controlled deployment of a body implantable prosthesis. The device includes an elongate prosthesis delivery member having a distal wall segment adapted to contain a radially self-expanding prosthesis in a reduced-radius delivery state against an internal restoring force. A radially self-expanding prosthesis is contained in the distal wall segment and thereby maintained in the reduced-radius delivery state. The prosthesis includes a linking structure near a proximal end of the prosthesis. An elongate prosthesis control member is mounted for axial travel relative to the delivery member, toward and away from a delivery position in which a distal end region of the control member extends along the distal wall segment of the delivery member and is disposed radially inwardly of the prosthesis. A control feature is disposed along the distal end region of the control member and extends radially outwardly from the control member beyond a radial midpoint of the linking structure when in the delivery position with the prosthesis so contained. Thus, the control feature is positioned to allow limited distal travel of the delivery member and prosthesis relative to the control member, and to effect a substantially non-frictional surface engagement with the linking structure upon said limited distal travel, to anchor the prosthesis against further distal travel relative to the control member.
The delivery member can comprise an outer catheter with a lumen running substantially along its complete length. The control member can comprise an elongate inner catheter disposed in the outer catheter lumen. Preferably a proximal region of the inner catheter extends beyond a proximal end of the outer catheter, to facilitate the use of the inner catheter proximal end to control the position of the inner catheter distal region relative to the outer catheter. This facilitates control of the prosthesis deployment from outside the body.
If desired, the control member can be provided with several control features, equally angularly spaced apart from each other about the control member, for use with a prosthesis in which the linking structure includes angularly spaced apart loops or other linking members. A one-to-one correspondence of control features and loops is workable, but not required. In one embodiment, three control features are used in conjunction with six loops formed at a proximal end of the prosthesis.
In a preferred embodiment, a tubular sleeve supports a symmetrical arrangement of control features, and is sized to facilitate its slideable installation onto the distal end region of the control member. The sleeve and control features are formed as a unitary member, preferably more rigid than the control member to provide more positive control over the prosthesis through engagement of the control features with the loops or other linking members. The control features can be surrounded by substantially closed loops of a prosthesis linking structure, in which case the features can control both proximal and distal prosthesis movement.
One aspect of the present invention is that the control feature outer ends define a control feature diameter less end than an inside diameter of the delivery member distal wall segment. At the same time, the radial spacing in between the control features and distal wall segment is less than half of a radial thickness dimension of the prosthesis linking structure. Consequently, the control member and control features are slideable relative to the delivery member with no frictional drag.
Yet, the control feature outer ends are sufficiently close to the distal wall section to prevent the linking structure or another part of the prosthesis from wedging into the space between the control features and distal wall segment.
A salient feature of the present invention is that the control member is operable to move the prosthesis proximally relative to the delivery device—or alternatively, to maintain the prosthesis substantially stationary while the delivery device is moved distally relative to the control member—through a surface engagement of each control feature with the prosthesis linking structure. The control features apply axial forces to the linking structure. Unlike the frictional prosthesis retraction systems discussed above, there is no need for frictional control of the prosthesis, and accordingly, no need for the additive radial force that undesirably increases the axial force required to deploy the prosthesis. Further, because the axial forces in the present system do not depend on friction, they do not diminish as prosthesis deployment progresses. As a result, the prosthesis can be fully retracted from a stage close to complete deployment, e.g. with up to ninety-five percent of its length positioned distally of the delivery device.
Another aspect of the present invention is a prosthesis delivery and deployment device. The device includes an elongate prosthesis delivery member having a distal wall segment adapted to contain a radially self-expanding prosthesis in a reduced-radius delivery state against an internal restoring force. An elongate control member is mounted for axial travel relative to the delivery member, toward and away from a delivery position in which a distal end region of the control member extends along the distal wall segment of the delivery member. A prosthesis anchor is mounted to the distal end region and comprises at least one elongate axially directed control feature extending radially outwardly from the control member. The control feature thereby is positioned to effect a releasable engagement with a proximal-end linking structure of a radially self-expanding prosthesis when in the delivery position and with the prosthesis so contained. The anchor, when in said engagement with the linking structure, is operable to anchor the prosthesis against distal travel relative to the control member.
Preferably, the anchor comprises a plurality of the elongate axially directed control features positioned to engage the linking structure. Then, the linking structure preferably includes a plurality of elongate axially directed loops, each associated with a different one of the control features. The anchor further can include a cylindrical anchoring body with a centrally located axial opening adapted to receive the control member and facilitate and mounting of the anchor in surrounding relation to the control member. The anchor advantageously can be more rigid than the control member, to provide a more positive engagement with its associated loop.
In one preferred version, the anchoring body has a recess directed inwardly from an outside surface of the anchoring body and adapted to receive a loop or other proximal-end linking structure of the prosthesis. The associated control feature is disposed in the recess, to be surrounded by the loop when the loop is received into the recess. In this version, the depth of the recess exceeds the radial thickness of the loop, so that the complete loop may be radially inwardly disposed relative to the outside surface.
A further aspect of the present invention is a prosthesis anchoring device adapted for fixation to a prosthesis deployment member. The device includes a generally cylindrical anchoring sleeve having a central opening extending axially there through to facilitate a slideable installation of the anchoring sleeve onto an elongate prosthesis deployment member for fixation along a distal end region of the deployment member. A control feature extends radially outwardly from the anchoring sleeve and is adapted to extend radially into a proximal-end linking structure of a radially self-expanding prosthesis when the prosthesis is maintained in a reduced-radius state against an internal restoring force and selectively axially aligned with the distal end region. The control feature, with the anchoring sleeve fixed to a deployment member and when so extending into a proximal-end linking structure of a radially self-expanding prosthesis so maintained and aligned, is adapted to engage the linking structure to prevent any substantial distal movement of the prosthesis relative to the deployment member.
Preferably, the control feature is elongate, directed axially, and adapted to extend into a prosthesis proximal-end linking structure taking the form of an elongate, axially extended loop. When surrounded by the loop, the control feature prevents any substantial distal movement of the loop relative to the anchoring body. In a more preferred version of the device, a plurality of the elongate control features are angularly spaced apart from one another about the anchoring body.
In another version of this device, the anchoring body includes a recess receding radially inwardly from its outside surface to receive the linking structure. The control feature is disposed within the recess. Typically, the depth of the recess exceeds the thickness of the linking structure. In systems that employ an outer catheter or other delivery device with a distal wall section designed to maintain a radially self-expandable prosthesis in a reduced-radius delivery state, the anchoring body can be dimensioned for a close fit within the distal wall section. As a result, the distal wall segment cooperates with the walls of the recess to capture the linking structure within the recess, while permitting the anchoring body to slide axially along the distal wall section.
To provide a more secure retention of the linking structure, the recess can be formed with a size and shape corresponding to that of the linking structure. For example, if the linking structure comprises an elongate linking strand formed into a loop, the recess can have a perimeter that closely corresponds to a perimeter of the loop. The control feature disposed in the recess is surrounded by the loop when the loop is retained in the recess. When surrounded by the loop, the control feature prevents any substantial distal movement of the loop relative to the anchoring body. As a result, the deployment member is operable through the anchoring body to deploy and retract the prosthesis.
In short, an anchoring body formed according to the present invention, with a central aperture sized according to a conventional prosthesis deployment catheter and with one or more control features sized according to the corresponding loops or other linking structure of a selected prosthesis, can considerably improve the prosthesis retraction capability of a prosthesis delivery and deployment system, without increasing the axial force required for deployment.
Several additional features enhance deployment system performance, regardless of whether the control features are recessed. For example, when the anchoring device is provided as a unitary structure including a cylindrical anchoring body and outwardly protruding control features, the device may be attached to a conventional inner catheter or other control member, fixed to the inner catheter at a location selected in accordance with the compressed length of the prosthesis to be deployed. Further, a relatively hard anchoring device can be fixed to a softer, more compliant inner catheter or control member, providing the capacity to negotiate serpentine internal passageways, while at the same time providing more positive control over the prosthesis through the relatively rigid control features.
Another useful feature arises from the provision of elongate control features and their axial orientation along the control member. This aligns the major dimension of each control feature with the direction of the forces applied through the control feature to the prosthesis, to overcome its tendency to follow the outer catheter or other prosthesis delivery member. As a result, the control features are more stable and less prone to unwanted flexure. The elongate axially directed features, as compared to pins or other features with circular cross sections, are better suited to limit twisting of the prosthesis relative to the control member. At the same time, the control features can have transverse widths selected to allow limited prosthesis rotation.
Yet another advantage arises from the positioning of each control feature to allow limited distal travel of the delivery member and prosthesis before the prosthesis engages the linking structure, and then to effect non-frictional surface engagement with the linking structure responsive to the limited distal travel. As compared to previous deployment systems with interlocks designed to prevent any axial movement of a prosthesis relative to an inner catheter or other control member, the novel coupling of the control feature and linking structure can be manufactured under tolerances that are less stringent. Further, loading the prosthesis into an outer catheter or other delivery member, while maintaining a prosthesis radially compressed and coupled to the control member through the control features, is much easier.
Yet another aspect of the present invention is a process for loading a radially self-expanding prosthesis for subsequent deployment in a body lumen, comprising the following steps:
Thus in accordance with the present invention, systems for intraluminally deploying radially self-expanding stents, stent-grafts and other implantable devices may be used to retract and withdraw such devices, even when deployment is near completion. There is no need for frictional retention of the device, and no resulting increase in axial force required for deployment. With the devices nearly deployed, yet retractable, physicians can evaluate prosthesis length, radius, placement relative to the treatment site, and other factors with more certainty as a basis for making critical decisions.
For a further understanding of the above and other features and advantages, reference is made to the following detailed description and to the drawings, in which:
Turning now to the drawings, there is shown in
An elongate and pliable inner member or catheter 28 extends along a length of the outer catheter, contained in lumen 20. When system 16 is configured for stent delivery as shown in
An anchoring device 40 is fixed in surrounding relation to inner catheter 28, near a proximal end of distal region 32. As is later explained, device 40 is operable to anchor stent 24 with respect to inner catheter 28, enabling use of the inner catheter to retract and recover a partially deployed stent.
A thrust member 42 is fixed in surrounding relation to inner catheter 28, proximally spaced apart from anchoring device 40. Inner catheter 28 is movable distally relative to outer catheter 18 to position thrust member 42 against the proximal end of stent 24, whereupon further distal travel of the inner catheter moves the stent distally relative to the outer catheter.
Inner catheter 28 is movable proximally relative to outer catheter 18 to bring anchoring device 40 into a surface engagement with stent 24. Alternatively, the inner catheter is movable distally to bring thrust member 42 into to surface contact with the stent. Thus, the inner catheter acts as a control member, to selectively control the position of stent 24 relative to the outer catheter.
As seen in
Stent 24 is radially compressible, against an internal elastic restoring force, to an axially elongated, reduced-radius delivery state. As seen in
In system 16, stent 24 closely surrounds but is not necessarily in contact with inner catheter 28. In contrast, in deployment systems that provide retraction through a frictional hold on the stent or other prosthesis, such contact not only is present, but must be maintained by exerting a radially inward force urging a stent against an inner catheter (or a sleeve or other gripping member along the inner catheter), to create a frictional hold that exceeds the frictional hold between the stent and the outer catheter. Thus, frictional systems provide for stent retraction, but at a cost: namely, a considerable increase in the axial force delivered by the inner catheter to deploy the stent. This is because the axial force must overcome not only the friction from the aforementioned restoring force of the stent, but the additional friction due to the additional radial force needed to press the stent against the inner catheter or gripping member. System 16, by providing an essentially non-frictional engagement of stent 24 with inner catheter 28, provides for stent retraction without increasing the axial force needed to deploy the stent.
As seen in
Anchoring device 40 preferably is a unitary member, formed of a polymer such as ABS, polycarbonate, or nylon 12. Thus, it can be harder or more rigid than inner catheter 28 and outer catheter 18. As a result, the anchoring device when engaged with stent 24 through loops 46 can more positively anchor and otherwise control the position of the stent.
The nature of the coupling between anchoring device 40 and stent 24 is best understood with reference to
In a satisfactory but less preferred arrangement, each fin extends radially to position its outer end beyond a radial midpoint of its associated loop, i.e. beyond the geometric center of strand 26 as indicated by the broken line at 62.
In
It is preferred to couple fin 58 and loop 46 as shown, to allow limited relative axial travel. As an alternative, the fin and loop could be configured to form a close or tight coupling that would virtually prevent relative axial movement of the stent and inner catheter. The looser, more flexible coupling has several advantages. The loops and fins can be formed under less demanding tolerances. Further, with the more flexible coupling it is much easier for the physician to load stent 24 into outer catheter 18 while maintaining the stent position relative to inner catheter 28.
As perhaps best seen in
Preferably a distance D between end surface 64 of the fin and an end surface 68 of the thrust member is selected in conjunction with a diameter d of strand 26 forming the loop, to determine a range of axial travel of stent 24 relative to inner catheter 28. In exemplary embodiments, distance D is from 1 mm to 2 mm and diameter d is 0.3 mm. The resulting range of axial travel is 0.7 mm to 1.7 mm, or in terms of the ratio D/d, is from 3.3 to 6.7. Advantageously, the ratio D/d is at least about 2.
Further, an axial length L1 of the interior of loop 46 exceeds an axial length L2 of fin 58 sufficiently to permit the required freedom of axial movement of the fin within the loop. For example, L1 can be 5.5 mm, with L2 being 3-4 mm. To allow limited rotation or transverse movement of the prosthesis relative to the inner catheter, an internal transverse width W1 of loop 46 exceeds a transverse width W2 of the fin. More specifically, W1 can be 1.5 mm and W2 can be 0.3 mm. Advantageously, W1 is at least about twice W2.
The use of anchoring device 40 to control stent deployment is illustrated in
At this stage, the user controls the proximal ends of the catheters, holding inner catheter 28 substantially stationary while proximally withdrawing outer catheter 18. Thrust member 42 engages stent 24 to prevent further proximal movement of the stent, in effect moving the stent distally relative to the outer catheter. As the stent emerges from the distal end of the outer catheter, it radially self-expands toward its relaxed state, as seen in
As depicted in
If the stent is properly positioned, and the earlier determinations as to stent size are confirmed, outer catheter 18 is moved further in the proximal direction, to completely release stent 24 for full radial expansion into contact with surrounding tissue, as indicated in
Conversely, if stent 24 needs to be repositioned or replaced, outer catheter 18 is moved distally to recompress and recapture the stent, restoring the configuration shown in
Several advantages of system 16, as compared to retraction devices that rely on friction, can be appreciated in conjunction with
Moreover, the coupling of stent 24 to inner catheter 28 through the anchoring device provides substantially the same anchoring force, regardless of the extent of stent deployment. Unlike friction-based systems, the amount of axial holding force available to retract the stent does not diminish as deployment progresses. Thus, the physician can deploy stent 24 to a point of near completion as indicated in
As seen in
In anchoring device 94, medial feature 100 and loop 102 form a coupling that is asymmetrical, in the sense that the axial force does not act through a central axis of the anchoring device. Nonetheless, the narrow spacing between outside surface 106 and the inside surface of outer catheter 86 facilitates a smooth sliding movement of inner catheter 88 within the outer catheter. In contrast, anchoring member 122 provides a symmetrical arrangement with a more balanced application of axial forces. In either arrangement, the number of recesses can be equal to, or an integral multiple of, the number of loops.
An advantage of anchoring devices 94 and 122, as compared to anchoring devices without recesses, is that they can more easily accommodate covered devices such as stent-grafts. This is because medial features 100 and 126 do not extend beyond the outer surfaces of their respective anchoring bodies, and thus do not interfere with a graft or other covering surrounding the stent.
While loop 140 provides a convenient proximal end linking member of a stent, it is apparent from
Thus in accordance with the present invention, stents and other prostheses of the radially self-expanding type are deployable at relatively low levels of axial force, and further are retrievable at multiple stages of deployment Inner catheters or other inner members are provided with anchoring devices that have radially extending fins, recesses, or other features designed to interact with loops or other proximal-end linking members of prostheses, to anchor the prostheses through surface-to-surface engagement rather than friction, thus to provide more positive anchoring without the need for any additional axial force for prosthesis deployment or retraction.
This application is a continuation of U.S. application Ser. No. 10/982,465 which was filed Nov. 5, 2012 and is incorporated herein in its entirety by reference.
Number | Name | Date | Kind |
---|---|---|---|
4300244 | Bokros | Nov 1981 | A |
4512338 | Balko et al. | Apr 1985 | A |
4553545 | Maass et al. | Nov 1985 | A |
4572186 | Gould et al. | Feb 1986 | A |
4580568 | Gianturco | Apr 1986 | A |
4665771 | Mitchell | May 1987 | A |
4665918 | Garza et al. | May 1987 | A |
4681110 | Wiktor | Jul 1987 | A |
4732152 | Wallsten et al. | Mar 1988 | A |
4733665 | Palmaz | Mar 1988 | A |
4740207 | Kreamer | Apr 1988 | A |
4762128 | Rosenbluth | Aug 1988 | A |
4768507 | Fischell et al. | Sep 1988 | A |
4795458 | Regan | Jan 1989 | A |
4830003 | Wolff et al. | May 1989 | A |
4848343 | Wallsten et al. | Jul 1989 | A |
4875480 | Imbert | Oct 1989 | A |
4878906 | Lindemann et al. | Nov 1989 | A |
4886062 | Wiktor | Dec 1989 | A |
4893623 | Rosenbluth | Jan 1990 | A |
4907336 | Gianturco | Mar 1990 | A |
4913141 | Hillstead | Apr 1990 | A |
4950227 | Savin et al. | Aug 1990 | A |
4969458 | Wiktor | Nov 1990 | A |
4969890 | Sugita et al. | Nov 1990 | A |
4990155 | Wilkoff | Feb 1991 | A |
4998539 | Delsanti | Mar 1991 | A |
5002560 | Machold et al. | Mar 1991 | A |
5026377 | Burton et al. | Jun 1991 | A |
5034001 | Garrison et al. | Jul 1991 | A |
5035706 | Giantureo et al. | Jul 1991 | A |
5037392 | Hillstead | Aug 1991 | A |
5037427 | Harada et al. | Aug 1991 | A |
5041126 | Gianturco | Aug 1991 | A |
5059166 | Fischell et al. | Oct 1991 | A |
5061275 | Wallsten et al. | Oct 1991 | A |
5064435 | Porter | Nov 1991 | A |
5071407 | Termin et al. | Dec 1991 | A |
5078720 | Burton et al. | Jan 1992 | A |
5089005 | Harada | Feb 1992 | A |
5089006 | Stiles | Feb 1992 | A |
5092877 | Pinchuk | Mar 1992 | A |
5108416 | Ryan et al. | Apr 1992 | A |
5123917 | Lee | Jun 1992 | A |
5135517 | McCoy | Aug 1992 | A |
5158548 | Lau et al. | Oct 1992 | A |
5163952 | Froix | Nov 1992 | A |
5163958 | Pinchuk | Nov 1992 | A |
5171262 | MacGregor | Dec 1992 | A |
5183085 | Timmermans | Feb 1993 | A |
5192297 | Hull | Mar 1993 | A |
5197978 | Hess | Mar 1993 | A |
5201757 | Heyn et al. | Apr 1993 | A |
5222969 | Gillis | Jun 1993 | A |
5222971 | Willard et al. | Jun 1993 | A |
5226913 | Pinchuk | Jul 1993 | A |
5234457 | Andersen | Aug 1993 | A |
5242451 | Harada et al. | Sep 1993 | A |
5256146 | Ensminger et al. | Oct 1993 | A |
5258020 | Froix | Nov 1993 | A |
5258098 | Wagner et al. | Nov 1993 | A |
5263964 | Purdy | Nov 1993 | A |
5282823 | Schwartz et al. | Feb 1994 | A |
5282824 | Gianturco | Feb 1994 | A |
5290295 | Querals et al. | Mar 1994 | A |
5304200 | Spaulding | Apr 1994 | A |
5306294 | Winston et al. | Apr 1994 | A |
5354308 | Simon et al. | Oct 1994 | A |
5354309 | Schnepp-Pesch et al. | Oct 1994 | A |
5372600 | Beyar et al. | Dec 1994 | A |
5378239 | Termin et al. | Jan 1995 | A |
5395390 | Simon et al. | Mar 1995 | A |
5403341 | Solar | Apr 1995 | A |
5405377 | Cragg | Apr 1995 | A |
5411507 | Heckele | May 1995 | A |
5411552 | Andersen et al. | May 1995 | A |
5415664 | Pinchuk | May 1995 | A |
5443496 | Schwartz et al. | Aug 1995 | A |
5453090 | Martinez et al. | Sep 1995 | A |
5456694 | Marin et al. | Oct 1995 | A |
5474563 | Myler et al. | Dec 1995 | A |
5478349 | Nicholas | Dec 1995 | A |
5484444 | Braunschweiler et al. | Jan 1996 | A |
5496277 | Termin et al. | Mar 1996 | A |
5507771 | Gianturco | Apr 1996 | A |
5522883 | Slater et al. | Jun 1996 | A |
5534007 | St. Germain et al. | Jul 1996 | A |
5554181 | Das | Sep 1996 | A |
5576006 | Smith | Nov 1996 | A |
5591230 | Horn et al. | Jan 1997 | A |
5690643 | Wijay | Nov 1997 | A |
5702364 | Euteneuer et al. | Dec 1997 | A |
5702418 | Ravenscroft | Dec 1997 | A |
5716393 | Lindenberg et al. | Feb 1998 | A |
5733325 | Robinson et al. | Mar 1998 | A |
5772669 | Vrba | Jun 1998 | A |
5797952 | Klein | Aug 1998 | A |
5800519 | Sandock | Sep 1998 | A |
5807327 | Green et al. | Sep 1998 | A |
5817102 | Johnson et al. | Oct 1998 | A |
5824041 | Lanker et al. | Oct 1998 | A |
5833707 | McIntyre et al. | Nov 1998 | A |
5836965 | Jendersee et al. | Nov 1998 | A |
5935135 | Bramfitt et al. | Aug 1999 | A |
5935161 | Robinson et al. | Aug 1999 | A |
5948017 | Taheri | Sep 1999 | A |
5954729 | Bachmann et al. | Sep 1999 | A |
6001123 | Lau | Dec 1999 | A |
6007574 | Pulnev et al. | Dec 1999 | A |
6017362 | Lau | Jan 2000 | A |
6027529 | Roychowdhury et al. | Feb 2000 | A |
6053941 | Lindenberg et al. | Apr 2000 | A |
6077295 | Limon et al. | Jun 2000 | A |
6102940 | Robichon et al. | Aug 2000 | A |
6120522 | Vrba et al. | Sep 2000 | A |
6241757 | An et al. | Jun 2001 | B1 |
6258099 | Mareiro et al. | Jul 2001 | B1 |
6264689 | Colgan et al. | Jul 2001 | B1 |
6302893 | Limon et al. | Oct 2001 | B1 |
6309415 | Pulnev et al. | Oct 2001 | B1 |
6350278 | Lenker et al. | Feb 2002 | B1 |
6352553 | van der Burg et al. | Mar 2002 | B1 |
6395017 | Dwyer et al. | May 2002 | B1 |
6419694 | Sandock | Jul 2002 | B1 |
6468301 | Amplatz et al. | Oct 2002 | B1 |
6514282 | Inoue | Feb 2003 | B1 |
6520983 | Colgan et al. | Feb 2003 | B1 |
6585758 | Chouinard et al. | Jul 2003 | B1 |
6607551 | Sullivan et al. | Aug 2003 | B1 |
6623518 | Thompson et al. | Sep 2003 | B2 |
6641608 | Pulnev | Nov 2003 | B1 |
7172617 | Colgan et al. | Feb 2007 | B2 |
7175654 | Bonsignore et al. | Feb 2007 | B2 |
7294146 | Chew et al. | Nov 2007 | B2 |
7517361 | Ravenscroft | Apr 2009 | B1 |
7655039 | Leanna et al. | Feb 2010 | B2 |
8337543 | Jordan et al. | Dec 2012 | B2 |
20010007082 | Dusbabek et al. | Jul 2001 | A1 |
20030040771 | Hyodoh et al. | Feb 2003 | A1 |
20030040789 | Colgan et al. | Feb 2003 | A1 |
20040204749 | Gunderson | Oct 2004 | A1 |
20050085896 | Bonsignore et al. | Apr 2005 | A1 |
20090177264 | Ravenscroft | Jul 2009 | A1 |
Number | Date | Country |
---|---|---|
0819411 | Jan 1998 | EP |
9173469 | Jul 1997 | JP |
0207795 | Jan 2002 | WO |
Number | Date | Country | |
---|---|---|---|
20120283816 A1 | Nov 2012 | US |
Number | Date | Country | |
---|---|---|---|
Parent | 10982465 | Nov 2004 | US |
Child | 13553877 | US |