SYSTEMS AND METHODS FOR FUSION OF ANATOMICAL JOINTS

Abstract

The present disclosure relates to improved plate and screw systems for use in fusion and other surgical procedures, which improve the ability to effectively affix adjacent bodies without gapping or experiencing loss of compression over time. The systems include plates having armatures configured to receive bushings, the bushings configured to pivot and rotate and thereby permit a greater degree of orientation of corresponding screws placed through the bushings. In embodiments, the bushings comprise anti-rotation elements which lock the bushings in a desired orientation. Methods for use of the components described herein are also disclosed.

Claims

1. A surgical system, comprising: a plate comprising one or more armatures, each of the one or more armatures offset from and extending about 90 degrees to the x-axis of the plate; the plate comprising at least one bore configured to receive a first screw oriented in a z-axis relative to the plate; the one or more armatures comprising a recess located at a distal end of the armature and having an inner surface; a bushing having an outer surface complementary to the inner surface of the recess and configured to be selectively received by and retained by the recess, wherein the bushing further comprises a through hole accessible via the recess when the bushing is retained therein; a second screw comprising a threaded portion, a non-threaded portion and a screw head having an outer surface complementary to the through hole of the bushing, wherein the threaded and non-threaded portions of the second screw pass through the through hole of the bushing, and wherein the outer surface of the screw head is configured to be retained within the through hole of the bushing, and wherein the second screw is oriented in the direction of and normal to the orientation of the first screw.

2. The surgical system of claim 1, wherein rotation of the screw once the screw head is retained within the bushing rotates the bushing relative to the recess.

3. The surgical system of claim 2, wherein further rotation of the bushing secures the position of the bushing relative to the recess, thereby securing the bushing and the screw in a fixed orientation relative to the plate.

4. The surgical system of claim 3, wherein the inner surface of the recess tapers from a proximal surface of the plate to a distal surface of the plate, and wherein the bushing is secured within the recess by a frictional or interference fit between the bushing and the recess after being advanced within the recess by a predetermined distance.

5. The surgical system of claim 3, wherein the bushing is permitted to pivot while retained by the recess but prior to being secured in the recess, allowing the screw orientation to be adjusted relative to the plate.

6. The surgical system of claim 3, wherein the screw head comprises threading on the outer surface and the through hole of the bushing comprises a complementary threading to the threading on the outer surface of the screw head, and wherein the bushing retains the screw head by threaded engagement between the screw head and the bushing.

7. The surgical system of claim 3, wherein the bushing further comprises a groove located about an outer circumference of the bushing and adapted to receive an anti-rotation element within the groove.

8. The surgical system of claim 7, wherein the anti-rotation element is configured to be positioned within the groove of the bushing, the anti-rotation element further comprising a key for engagement with a notch on the inner surface of the recess.

9. The surgical system of claim 8, wherein the anti-rotation element is substantially circular.

10. The surgical system of claim 8, wherein the anti-rotation element is c-shaped.

11. The surgical system of claim 10, wherein the anti-rotation element may be selectively removed from the groove of the bushing.

12. The surgical system of claim 7, wherein the groove does not extend about an entire outer circumference of the bushing.

13. The surgical system of claim 8, wherein the rotation of the bushing causes the key of the anti-rotation element to engage the notch of the inner surface of the recess and prohibit further rotation of the bushing.

14. The surgical system of claim 1, wherein the plate comprises two armatures, each of the armatures comprising a recess having an inner surface for respectively receiving and retaining a first and second bushing, each of the first and second bushings comprising a groove located about an outer circumference of the bushing and adapted to receive an anti-rotation element within the groove, the anti-rotation elements configured to be positioned within the grooves of the bushings, each anti-rotation element further comprising a key for engagement with a notch on the inner surface of the recess and locking the bushings relative to the recesses when the key engages the notch of the inner surface of the bushing.

15. The surgical system of claim 14 further comprising: a third screw configured to be received by the second bushing; wherein the armatures are located on opposing ends of the plate, and wherein the second and third screws are oriented to converge towards one another while avoiding contact; and wherein the first, second and third screws are oriented in three orthogonal planes.

16. The surgical system of claim 1, wherein the at least one bore is located at a distal end of the plate and about the x-axis of the plate.

17. A surgical assembly, comprising: a thin plate having first and second sides, the thin plate comprising one or more cylindrical bores extending therethrough; the thin plate further comprising two or more armatures extending from the first or second side of the plate; the two or more armatures comprising a recess having an inner surface and a notch located along the inner surface; each of the two or more armatures adapted to receive a bushing configured to fit within the recess of the corresponding armature and having an outer profile that is complementary to the inner surface of the recess within which it is received, the bushings permitted to pivot or rotate within the recesses; each bushing having at least one outwardly-extending protrusion; and wherein the bushing is prevented from pivoting or rotating once the outwardly-extending protrusion engages the notch along the inner surface of the recess.

18. The surgical assembly of claim 17, further comprising a screw adapted for operative engagement with a threaded hole of the bushing, wherein rotation of the screw beyond a predetermined amount rotates the bushing which urges the outwardly-extending protrusion to engage the notch and lock the position of the bushing relative to the thin plate.

19. The surgical assembly of claim 17, wherein the two or more armatures comprise a first armature having a curved shape and having a first recess offset from the x-axis of the thin plate by about 90 degrees, and further comprising a second armature having a curved shape and having a second recess offset from the x-axis of the thin plate by about 90 degrees.

20. The surgical assembly of claim 19, wherein the first and second armatures extend from the same side of the thin plate.

21. The surgical assembly of claim 19, wherein the first and second armatures extend from opposite sides of the thin plate.

22. The surgical assembly of claim 19, wherein the first and second armatures comprise different lengths.

23. The surgical assembly of claim 19 further comprising a third armature and a corresponding third recess.

24. The surgical assembly of claim 17, wherein the bushings are secured within the recesses by a frictional or interference fit.

25. The surgical assembly of claim 17, wherein the at least one outwardly-extending protrusion is selectively retractable, thereby allowing the bushing to pivot or rotate freely when the outwardly-extending protrusion is retracted.

26. The surgical assembly of claim 17, wherein the recess tapers from a proximal surface of the thin plate to a distal surface of the thin plate.

27. The surgical assembly of claim 26, wherein the outer surface of the bushing tapers to a matching degree as the recess.

28. The surgical assembly of claim 18, wherein the screw is a cortical bone screw, a cancellous bone screw or a cannulated bone screw.

29. An orthopedic implant system which comprises a spanning link having a longitudinal axis in the x direction and having a first spanning link fastener with a first spanning link fastener axis which forms an angle relative to the spanning link longitudinal axis from 80 degrees to 100 degrees, and a first leg link extending away in the y and z direction from the of the spanning link longitudinal axis and having a first leg link fastener aperture that receives a first leg link fastener which has a first leg link fastener axis that extends away from the first leg link fastener aperture in the direction of but not intersecting the first spanning link fastener axis.

30. The orthopedic implant system as set forth in claim 29, wherein the first leg link forms a curve that defines at least 60 degrees of an arc.

31. The orthopedic implant system as set forth in claim 29, wherein the first leg link length and the second leg link length are not the same.

32. The orthopedic implant of claim 29, wherein one of the first leg link and the second leg link forms an arc of at least 75 degrees in the z direction.

33. The orthopedic implant of claim 32, wherein one of the first leg link or the second leg link forms an arc of at least 85 degrees in the z direction.

34. The orthopedic implant of claim 29, wherein the long spanning link has a length of 15 to 60 mm, a width of 2 to 5 mm, and a thickness of 1 to 2.5 mm, and the first leg link has a length of 8 to 20 mm extending from the first spanning link and a width of 2 of 5 mm and a thickness of 1 of 2.5 mm.

35. The orthopedic implant as set forth in claim 29, wherein the spanning link further comprises an extension.

36. The orthopedic implant as set forth in claim 35, wherein the extension includes an aperture configured to receive a fastener.

37. The orthopedic implant as set forth in claim 35, wherein the extension receives the distal end of one of the fasteners.

38. An orthopedic implant system having an outline consisting of a single spanning link that extends from 15 to 60 mm along a long axis and has two opposing terminal ends joined across a short axis at a width of 2 to 5 mm by two opposing long sides, and each of the terminal ends include a through aperture each of which receives a cross screw at least one the cross screws being a polyaxial compression screw, and wherein the cross screw axes are in differing planes and form an X-shape but which do not contact each other.

39. An implant which comprises a first long curved spanning link having a top surface and a medial line along its length and a first end having a first ear having a first fastener aperture and a second end having a second ear having a second fastener aperture and the long spanning link is fixed at the first end by a first fastener that extends through the first fastener aperture at 90 degrees +/−10 degrees to the medial line of the spanning link and aperture and the long spanning link is fixed at the second end by a second fastener that extends through the second fastener aperture at 90 degrees +/−10 degrees to the medial line of the spanning link, a first leg link and a second leg link each extending away from the medial line of the spanning link and the first leg link and the second leg link each having a terminal aperture for a first and second leg link fastener respectively.

40. An orthopedic implant system having an outline comprising a spanning link that extends from 15 to 60 mm along a long axis and has two opposing terminal ends joined across a short axis at a width of 2 to 5 mm by two opposing long sides and each of the terminal ends that each have a top surface and extend away from the long axis to collectively form a T-shape, and the legs each have an eyelet defining a surface around an aperture in a plane at from 60 to 120 degrees relative to the top surface of the respective leg, and each of which receives a cross screw with at least one being a polyaxial compression screw, and wherein the cross screw axes are in differing planes that form an X-shape but which do not interfere with each other.

Description

BRIEF DESCRIPTION OF THE DRAWINGS

[0045] The accompanying drawings, which are incorporated herein and constitute a part of the specification, illustrate embodiments of the disclosure, and together with the Summary and the Detailed Description serve to explain the principles of these embodiments. In certain instances, details that are not necessary for an understanding of the disclosure or that render other details difficult to perceive may have been omitted. It should be understood, of course, that the present disclosure is not necessarily limited to the particular embodiments illustrated herein. In the drawings:

[0046] FIG. 1 shows a top perspective view of the system according to an embodiment of the present disclosure;

[0047] FIG. 2 shows a detailed perspective view of the system of FIG. 1;

[0048] FIG. 3 shows a top plan view of the system according to another embodiment of the present disclosure;

[0049] FIG. 4 shows a side perspective view of the system according to yet another embodiment of the present disclosure;

[0050] FIG. 5 shows another side perspective view of the system according to yet another embodiment of the present disclosure;

[0051] FIG. 6 shows a side elevation view of the system according to yet another embodiment of the present disclosure;

[0052] FIG. 7 shows a side perspective view of the system according to yet another embodiment of the present disclosure;

[0053] FIG. 8 shows a top plan view of the system according to yet another embodiment of the present disclosure;

[0054] FIG. 9 shows another top plan view of the system according to yet another embodiment of the present disclosure;

[0055] FIG. 10 shows a side perspective view of the system of FIG. 9;

[0056] FIG. 11 shows a top plan view of the system according to yet another embodiment of the present disclosure;

[0057] FIG. 12 shows a side elevation view of the system of FIG. 11;

[0058] FIG. 13 shows a perspective view of particular method steps according to an embodiment of the present disclosure;

[0059] FIG. 14 shows a perspective view of an additional method step according to an embodiment of the present disclosure;

[0060] FIGS. 15A-15C show detailed perspective views of the system and method according to embodiments of the present disclosure; and

[0061] FIG. 16 shows a perspective view of an instrument for use with the systems and methods according to embodiments of the present disclosure.

[0062] The foregoing drawing figures are not necessarily to scale. In certain figures, more or less detail has been shown to streamline the disclosure and/or provide clarity to the illustrations. It is expressly understood that certain embodiments shown in any one of the foregoing drawing figures may comprise other elements shown or described in relation to other embodiments, and that such combinations and sub-combinations are considered within the scope of the present disclosure.

DETAILED DESCRIPTION

[0063] It is the Applicant's intent that this specification and the inventions described herein be accorded a breadth in keeping with the scope and spirit of the disclosure and various embodiments disclosed, despite what might appear to be limiting language imposed by certain examples described in detail below. To acquaint persons skilled in the pertinent arts most closely related to the present disclosure, preferred and/or exemplary embodiments are described in detail without attempting to describe all of the various forms and modifications in which the novel apparatus, devices, systems and methods might be embodied. As such, the embodiments described herein are illustrative, and as will become apparent to those skilled in the arts, may be modified in numerous ways within the spirit of the disclosure.

[0064] Embodiments of the present disclosure present several advantages over the prior art including, for example, the speed and efficacy of the procedure, the minimally invasive aspects of the procedure, the disposability and/or reusability of components of the system, the ability to introduce tools, instrument and components of the system to a surgical site with minimal risk of damage to the surrounding tissue, lower risk of infection, more optimally placed fasteners, decreased risk of components of the system becoming misaligned or dislodged, and fewer and/or less expensive components required for a particular surgery, among other advantages.

[0065] Referring now to FIGS. 1-16, certain embodiments of the present disclosure are shown. Referring to FIG. 1, the system 100 in varying embodiments is comprised of components well suited for placement and use proximate to the Metatarsophalangeal joint. More particularly, components of the system 100 are adapted to be received against one or more bodies to facilitate, for example, fusion between the one or more bodies. Other procedures for use with the system 100 of the present disclosure include, but are not limited to, Calcaneocuboid fusions, Talonavicular fusions, Navicularcueiform fusions, Lapidus, Ankle fusions and other fusions of the foot and ankle. Details relating to the different components used in these and other procedures are provided below.

[0066] Referring to FIG. 2, the system 100 may be comprised of one or more components, and according to one embodiment comprises a plate 110. The plate 110 preferably comprises a central portion and one or more armatures 115. The armatures 115 preferably extend from the central portion of the plate 110 and may be close to perpendicular to the longitudinal or x-axis of the central portion. As shown in FIG. 2, the one or more armatures 115 are preferably arcuate or semi-arcuate in shape as the armatures 115 extend from the central portion of the plate 110. The plate preferably comprises one or more apertures or bores 140, while the one or more armatures 115 preferably comprise a substantially hollow collar 118 for inserting or guiding one or more fasteners, such as a cannulated, cortical or cancellous screw or similar fastener.

[0067] The bores 140 of the plate 110 may be oriented and/or aligned to permit fasteners, such as screws S2 to be inserted in a generally parallel manner, while the collar(s) 118 may be aligned in a manner to permit fixations devices, such as screws S1 to be inserted in a generally converging manner, but without permitting any of the fasteners to intersect when inserted into the adjoining bodies. This provides numerous benefits to the surgeon and the patient, such as orienting fixations devices in three orthogonal planes, as well as the other benefits addressed in the Summary.

[0068] To improve flexibility with respect to alignment of screws S1, the collars 118 may be configured to receive a bushing 120. The outer circumference of the bushing 120 may be configured to closely match the interior dimensions of the collar 118, such that the bushing 120 may be received and retained by the collar 118, including in either a threaded or non-threaded engagement. The collar 118 may comprise a rim or lip at its lower or bottom edge to prevent the bushing 120 from passing through the collar 118. The bushing 120 is preferably annular and may comprise an inner surface that has is part-spherical in cross-section. In an embodiment where the outer surface comprises a screw-thread, the bushing 120 may be sized such that the screw-thread on the outer surface interfaces with a complementary screw-thread lining the interior of the collar 118.

[0069] In one embodiment, placement of the fasteners through the bores 140 and collars 118 of the plate 110 permits a surgeon to accurately and securely place the plate 110 in its desired location and orientation, including as shown in FIGS. 1, 4, 5 10 and 12-14, so that the surgeon does not need to worry about movement of the adjacent bodies, movement of the components of the system, misalignment of the armatures 115 and associated collars 118, etc.

[0070] Each bushing 120, in turn, may comprise a substantially hollow opening for receiving a screw S2, as shown in FIG. 2. The bushing 120 may be oriented in each collar 118 so as to provide freedom of movement dorsally or plantarly or medially, or a combination thereof. The degree of freedom is determined by the orientation of the bushing 120 within the collar 118, which may be configured with increased or decreased tolerances (relative to the bushings) to increase or decrease the degree of freedom in orienting the bushings 120 and thereby the screws S2. The freedom of movement described above enables the screw S2 to rotate relative to the longitudinal plane of the plate 110 by up to 30 degrees of neutral in either side, therefore providing a total arc of 60 degrees.

[0071] Bushing 120 may further comprise an outwardly-extending protrusion or “key” 122 that protrudes radially from the outer surface of the bushing 120. The key 122 is preferably sized complementary to a notch 112 in the interior hollow surface of collar 118, as depicted in FIG. 2. The key 122 is preferably on a proximal end of the bushing 120 (relative to the user) so that the key 122 cannot engage the notch 112 until the bushing 120 is received by and retained by the collar 118. The engagement of the key 122 with the notch 112 prevents further rotation and preferably movement of the bushing 120 relative to the collar 118, as described in greater detail below.

[0072] Still referring to FIG. 2, a tool 150 may be used to position a screw S2 through the bushing 120 and collar 118 in a desired trajectory/orientation as described herein. Due to the close tolerances of the collar 118 and the bushing 120, and the bottom rim of the collar 118 described above, the bushing 120 may not pass through the collar 118 even when not engaged with the collar 118 in a threaded engagement. The collar 118 may alternatively be tapered, and it is to be expressly understood that other means of providing a stop for the bushing 120 relative to the collar 118 are contemplated. The screw S2 may also comprise a threaded head 130, which may be received within the bushing 120 including by way of a threaded engagement.

[0073] Advancement of the screw within the bushing 120 (when placed within the collar 118) may be achieved by tool 150 without disturbing the bushing 120, as the shaft of the screws S2 is preferably narrower than the interior dimension of the bushing 120. However, further advancement of the screw S2 that causes threaded engagement with bushing 120 will result in rotation of the bushing 120, and ultimately engagement of the key 122 in the notch 112 of the collar 118. Engagement of the key 122 in notch 112 prevents further rotation of the bushing 120 and thereby locks the bushing 120 relative to the collar 118. This locking engagement is depicted in FIG. 2. Any of the components described in this section may be provided with a high-friction surface to facilitate this locking of the bushing 120 relative to the collar 120. Thus, in use, the screw S2 may be threaded into the bushing until it reaches a limit of travel, whereupon further rotation of the screw S2 also rotates the bushing 120 causing the radially extending key 122 to translate rotationally so as to engage with the notch 112.

[0074] Alternatively, the bushing 120 may comprise a groove for receiving an anti-rotation element. The anti-rotation element of this embodiment may comprise a key for engaging with the notch of the collar, as described above, rather than the bushing itself. Upon insertion of the screw, the initial threaded portion passes through the bushing from the upper side of the plate and into the underlying bodies. The threaded screw head then begins to engage with the internal thread of the bushing. As the thread advances, the friction begins to rotate the bushing within the cavity. The anti-rotation element is engaged within the groove of the bushing, and is unable to rotate with the bushing once the key has engaged with the notch. Accordingly, the friction between these components and the engagement between the key and the notch create an interference frictional fit, thereby locking the assembly in a desired axial alignment. In embodiments, the anti-rotation element is circular and sized to be placed securely on an outer circumference of the bushing and within a groove in the bushing. The groove does not necessarily extend about an entire perimeter of the bushing. In other embodiments, the anti-rotation element is substantially in the shape of a “C” and the anti-rotation element may be selectively removed from the bushing if desired, thereby changing the assembly from a locking type to a non-locking type. Alternatively, the key described herein may be selectively retractable relative to the anti-rotation element, thereby permitting the assembly to change from a locking to a non-locking type without deviating from the other aspects of the assembly described herein.

[0075] In yet another alternative embodiment, the bushing may be provided with no threading in the hole, the hole having a tapered configuration, and a screw may be provided with a tapered section for cooperation with this tapered hole in the bushing. Provided a force is applied in the axial direction which drives the tapered section of the screw into the tapered section of the bushing, rotation of the screw will result in rotation of the bushing and the locking mechanism of the polyaxial assembly will activate. Such a force may for example be applied in the instance that the screw has a lower section which is screwed into a substrate, resulting in a force which pulls the upper tapered section of the screw into the tapered hole of the bushing.

[0076] Thus, in embodiments, the inner surface of the recess is configured to taper from a proximal surface of the plate, relative to the user, to a distal surface of the plate. A bushing may be secured within the tapered recess by a frictional or interference fit between the bushing and the recess after being advanced within the recess by a predetermined distance. In embodiments, the bushing is permitted to pivot while retained by the recess, prior to being secured. This in turn allows the screw orientation to be adjusted relative to the plate.

[0077] As shown in FIGS. 1 and 2, the plate 110 is configured to be positioned dorsally, in one placement of the system, while the armatures extend away and downwardly from the central portion of the plate 110 such that the collars 118 are oriented in a generally facing direction relative to the adjacent bodies. This configuration in turn permits screws or other fasteners to be inserted in a converging but complementary manner, and without risk of intersecting one another. This configuration also permits screws or other fasteners (S1, S2) to be oriented in multiple orthogonal planes, while also permitting converging trajectories, thereby greatly improving compression and simultaneously avoiding undesired collision among the different fasteners.

[0078] The plates 110 described herein may further comprise one or more fenestrations 117, 119, which in certain embodiments are located and sized to accommodate 2 mm or other sized K-wires. The placement of K-wires and other temporary fasteners may be used to temporarily position and/or stabilize the plate 110 prior to insertion of permanent fasteners. The fenestrations may be different in size and/or shape to accommodate placement of other tools, implants, etc. In certain embodiments, no fenestrations are provided with the plate.

[0079] Any of the fasteners or screws referred to herein may be temporary or permanent during a fusion or other surgery practiced using the systems or methods described herein. Screws and other fasteners used with the systems and methods described herein may be locking or non-locking type. By way of example but not limitation, the screws S1 may be self-drilling, self-tapping poly-axial locking screws. The screws may be cortical or cancellous, however, as the diameter of the screw is increased, the resistance to fatigue and ultimately failure also increases. Therefore, cortical screws are preferred over cancellous screws. Alternatively, screws may have a larger than standard core diameter to account for this issue.

[0080] Any of the fasteners described herein may be used with or without pre-drilled holes in the underlying boney anatomy. In the embodiment where pre-drilled holes are employed, the diameter of the drill is preferably smaller than that of the core diameter of the screw such that insertion of the screw causes radial expansion and impaction of the surrounding bone. This in turn improves pull-out resistance. Furthermore, the fasteners may be inserted through the bores 140 and/or collars 118 by only making very small incisions, and in embodiments described herein may be performed via MIS procedures.

[0081] In embodiments, the system may be referred to as an orthopedic implant system. The system preferably comprises a central portion or spanning link having a longitudinal axis in the x direction. The spanning link is configured to receive at least one fastener. The fastener received by the spanning link preferably has an axis which forms an angle relative to the spanning link's longitudinal axis in the range of 80 degrees to 100 degrees. The spanning link may comprise a first leg link extending away in the y and z direction (as taken from the longitudinal axis in the x direction), which has an aperture for receiving, for example, another fastener. This fastener preferably has an axis that extends away from the first leg link fastener aperture in the direction of but not intersecting the axis of the fastener received by the spanning link. In one embodiment, the first leg link extends away in both the y and z direction to form a curve that defines at least 60 degrees of an arc.

[0082] In certain embodiments, the first leg link aperture defines a plane which is not parallel to the spanning link's longitudinal axis. In yet another embodiment, the implant system comprises a second leg link extending away from the spanning link in the y-z direction and having a length that may be the same as or different from the first leg link length. The second leg link preferably has an aperture which receives a fastener, and that fastener has an axis that extends away from the second leg link fastener aperture. In a preferred embodiment, the second leg link fastener axis is in the direction of a desired area of fusion for a particular surgery. Also, the first leg link fastener axis and the second leg link fastener axis preferably converge toward each other, but do not intersect or otherwise cause interference between the two leg link fasteners.

[0083] In embodiments, the second leg link aperture defines a plane which is not parallel to the spanning link's longitudinal axis. In other embodiments, the first leg link defines an arc of more than 45 degrees relative to the spanning link's longitudinal axis. In still other embodiments, the first leg link defines an arc of more than 75 degrees relative to the spanning link's longitudinal axis.

[0084] The first leg link length and the second leg link length are not necessarily the same. In one embodiment, the spanning link has a length of 15 to 60 mm, a width of 2 to 5 mm, and a thickness of 1 to 2.5 mm, and the first leg link has a length of 8 to 20 mm extending from the first spanning link and a width of 2 of 5 mm and a thickness of 1 of 2.5 mm.

[0085] In embodiments, the first and second leg links are formed of a material to cuase the leg links to flex in response to a force applied to the same. The first leg link or the second leg link may form an arc of at least 85 degrees in the z direction.

[0086] The fasteners described above preferably have at least 30 degrees of conical freedom about their axes, and in another embodiment have at least 40 degrees of conical freedom. The first and second leg link fasteners preferably cross one another, although in differing planes, to form an X-shape. However, even with the above-recited degrees of freedom, the two fasteners do not contact each other. One or more of the leg link fasteners may contact an extension of the spanning link and by received by the extension, such as the distal tip of a fastener being threaded into an aperture in the extension.

[0087] In FIG. 3, an alternate embodiment of the present disclosure is shown in a top plan view. The plate 110 is similar to the ones described above, and the content relating to the plate of FIG. 2 is incorporated here by reference. The plate 110 of FIG. 3 comprises an extension 113 having an aperture for capturing the distal end of a screw S1 inserted through the opposite collar 118, as shown in FIG. 3. In this manner, the screw S1 can be captured and retained by the extension 113, which both provides rigidity of the screw S1 and prevents subsidence after implantation, and also ensures proper alignment of the screw S1 along a trajectory intersecting the aperture of the extension 113. The aperture is preferably threaded with a female thread to receive the threaded end of the screw S1. In this manner, the screw S1 passing through the aperture provides stability and rigidity, while the other screw S1 (which in a preferred embodiment is only partially threaded) is configured to provide compression through introduction in the underlying boney anatomy.

[0088] Referring now to FIG. 4, one particular orientation of the plate and fasteners described above is shown. In this arrangement, the plate 110 is positioned to address a Lapidus indication, whereby the armatures and terminating collars are positioned plantarly. Here, the primary fasteners are inserted through the collars of the armatures in a crossing but non-intersecting manner to facilitate a fusion of the first TMT joint, such as in a Lapidus procedure. FIG. 5 illustrates another orientation for facilitating a Lapidus procedure, wherein the armatures and collars are positioned dorsally. The system may be positioned in other manners than shown in FIGS. 4-5 while still achieving the benefits described above, including in other fusion and non-fusion surgical procedures.

[0089] In one embodiment, the fasteners are prohibited from contacting one another, but nonetheless converge to pass close to one another to achieve the greatest possible compressive strength when coupled to the plate. Furthermore, the fasteners may be desirably oriented relative to the z-axis so as to avoid the fasteners passing only partially through the dense area of the adjacent bodies where subsidence is less likely to occur, and also to avoid gapping in certain areas of the joint. Secondary fasteners may also be inserted through the bores in the plate without interfering with the primary fasteners. The placement of the plate is such that there is adequate boney anatomy for the fasteners to be inserted without penetrating the bodies, and without intersecting each other.

[0090] The armatures may be oriented at more of a tangential angle relative to the central portion of the plate. This may permit placement of the plate more medially, or to conform more closely to the general shape of the adjacent bodies and thereby avoid discomfort to the patient.

[0091] FIG. 6 shows a side elevation view of a system according to another embodiment. This view is particularly helpful in showing the multiple planes in which the fasteners are oriented, even more particularly how the fasteners may be positioned in three orthogonal planes to improve strength and resist movement. In this embodiment, the plate 110 comprises two differently sized armatures 115, 115′ with one of the armatures 115′ being shorter than the other 115. This permits the collar of the first armature 115′ to be offset in the z-axis from the other collar of the longer armature 115. This system may be beneficial to ensure placement of fixations devices in multiple bodies at desired areas (i.e., bone density) or to further avoid collision of fasteners used in a relatively small area. FIG. 7 depicts another embodiment where only a single armature 115′ is provided. The other aspects of the system described above apply equally to the components of these embodiments of FIGS. 6 and 7 and are incorporated herein by reference.

[0092] A person of ordinary skill in the art will recognize that the foregoing embodiments convey various manners of transmitting torque from a screw to a bushing so as to rotate the bushing and lock the bushing relative to a collar in which the bushing is placed. One of ordinary skill will appreciate that other means may be provided for this objective, and that the screw may be replaced with a bolt or equivalent component. In one alternate embodiment, the bushing may comprise a “slotted” upper surface to receive a flat-bladed or Phillips style screwdriver. One of ordinary skill will also appreciate that with the bushing in position within the collar of the armature, the bushing could then be rotated by means of a screwdriver until the key engages with the notch described above, so that the bushing locks in place in a desired orientation. Any screw or bolt or other item may then be attached to the bushing or driven through it with its axis in a particular desired orientation as then defined by the locked-in position of the bushing.

[0093] According to various embodiments described herein, the apertures for receiving primary fasteners (i.e., screws) are offset from the central portion of the compression plate. The offset nature of the apertures and the position of the armatures relative to the central portion of the plate provides for a more optimal placement and orientation of the fasteners relative to the joint. This is especially true when inserting the fasteners in a small area, in a difficult location or in a MIS application.

[0094] Referring now to FIG. 8, another embodiment of the present disclosure is shown. Here, the plate 110 comprises an extension 125 that includes an additional bore 140′. This additional bore 140′ facilitates placement of an additional fastener, thereby strengthening the connection between the plate and the underlying bodies. In this embodiment, one of the screws S1 may be captured as described above in relation to FIG. 3, although in other embodiments the screws S1 are not captured as shown in FIG. 2.

[0095] A greater or fewer number of bores and/or fenestrations may be provided without departing from the inventive concepts described herein. For example, FIG. 9 depicts a modified plate 110 that comprises four bores 140. In addition, this plate 110 also comprises a third armature for placement of an additional screw. Variations on the embodiments of FIGS. 8 and 9 are contemplated and considered within the scope of the present disclosure.

[0096] FIG. 10 shows the system of FIG. 9 positioned against the underlying boney anatomy. In this manner, the guide may be useful in a MTP fusion, and further beneficial in the sense the plate provides both dorsal and plantar-positioned collars for introducing fixations devices into the bodies, further assuring solid compression and avoiding gapping.

[0097] FIG. 11 shows a plate 110 having armatures 115 only about one longitudinal end of the central portion of the plate 110. This configuration is particularly beneficial when addressing Lapidus indications. The screws 51 may be retained by any of the bushings described above, including with the anti-rotation element. Accordingly, applicant incorporates those paragraphs of the Detailed Description herein by reference. FIG. 12 is the system of FIG. 11 shown with the underlying bodies, which may be used in a Lapidus surgery as described above in relation to FIG. 4.

[0098] According to embodiments, the armatures may reach from 60 to 120 degrees in range, unlike many plates that permit only 90 degree orientations. This is particularly beneficial for procedures on the foot and ankle, where degrees of freedom and corresponding flexibility allow a surgeon to perform procedures that are not permissible with current state of the art plate and screw systems. It is to be expressly understood that the plate and armatures described herein may be curved or angled to conform closely to the surrounding patient anatomy. The material of the plate and other components of the systems described herein may comprise stainless steel, titanium, titanium alloy, aluminum alloy, chromium alloy, vanadium and other metals or metal alloys. The components may further comprise PEEK, carbon fiber, polyurethane, polyethylene, ABS plastics, photo-polymers, resins, fiber-encased resinous materials, rubber, latex, synthetic rubber, synthetic materials, polymers, and natural materials.

[0099] Referring now to FIG. 13, an embodiment is shown where the central portion of the plate does not include extensions or armatures. This type of component may be particularly desirable for use in MIS applications. The general benefits of the system and methods described above in the Summary and Detailed Description are still achieved with this particular embodiment.

[0100] In FIG. 13, the plate 110 has been slightly elevated from the underlying anatomy to illustrate how adjacent bodies may be prepared in advance by a surgeon to achieve even greater alignment and compression when installing the system in its varying embodiments. For instance, the boney anatomy may be cut, drilled or debrided 210, 220 to allow opposite ends of the plate and the corresponding bores 140 to rest congruently along the surfaces removed by the surgeon. This site preparation may be quickly and easily performed and assist in placement of the components of the system described herein.

[0101] The preparation by cutting, drilling or debriding 210, 220 described above may also be performed in a manner so that any armatures associated with the plate 110 are required to deflect slightly in order to be positioned on the adjacent bodies, thereby creating an interference fit or snap-fit. The frictional engagement may also help increase compressive strength of the plate 110. However, it is not necessary to perform preparation of the surgical site in order to utilize the benefits of the system and methods described herein.

[0102] Methods of performing procedures using the aforementioned system are also within the scope of the present disclosure. Referring now to FIGS. 13-14, various stages or steps of the system being used in a surgical setting are shown. Although depicted relative to a foot joint, it is expressly understood that other joints and other adjacent bodies may employ the following systems and methods with equal efficacy. In FIG. 13, the plate 110 is shown positioned next to the adjacent bodies where compression is needed to ensure a successful fusion, to use one example. The plate 110 may be positioned without secondary fasteners and in a location where the plate 110 spans the joint between the adjacent bodies. The bodies may have been prepared in advance, such as by cutting or otherwise removing the surfaces (as described above) that would otherwise interfere with placement of the compression plate. In FIG. 14, an insertion instrument 250 is shown being inserted through one of the bores 140. Other instruments may comprise any of those known to a person of ordinary skill in the art for cutting, drilling, debriding, shaving or removing boney anatomy.

[0103] According to one embodiment, the system and method may comprise the use of one or more inserts. The inserts, such as insert 200 shown in FIG. 14, may have surfaces that are adapted to receive a fastener such as a screw and enhance the plate's 110 ability to promote crossing but non-intersecting placement of the fasteners therethrough and, once inserted, ensures that the adjacent bodies are in compression and that the fasteners will not subside during the surgery and recovery by the patient.

[0104] Referring again to FIG. 14, inserts 200 may be placed within one or more bores 140 of the plate 110 and further direct the fasteners through the plate 110. These inserts 200 may extend outwardly from the proximal surface of the plate 110, may extend inwardly from the distal surface of the plate 110, or may be positioned substantially flush with the plate 110, depending on the surgeon's preference and the particular demands of the surgical procedure to be performed. In one embodiment, the boney anatomy of the patient may be prepared (as described above in FIG. 13) to allow a surgeon to countersink the inserts 200 into the adjacent bodies. In embodiments, the insert 200 comprises a cam, a slope or equivalently-shaped surface to provide a pre-determined orientation to a screw or equivalent fastener, relative to the plate 110 that receives the insert 200.

[0105] The inserts 200 further promote use of the compression plate in a MIS procedure. Further illustration of the aspects of this particular embodiment is provided in FIGS. 15B-C. It is to be understood that the system of FIGS. 15A-C is preferably for use in a MIS procedure. The plate of this embodiment has a central portion, and two armatures having recesses at their distal ends. As distinguished form the embodiment of FIG. 2, however, the armatures extend parallel to the longitudinal or x-axis of the plate's central portion. In this embodiment, the fasteners may still converge and cross one another, albeit in different planes so as not to contact one another. This may be achieved, for example, by the orientation of the apertures of the inserts, or by the orientation of the apertures in the first and second armatures.

[0106] FIG. 15A illustrates the unique placement of the fasteners once placed through the compression plate and its inserts. The trajectories T1, T2 of the fasteners are shown as converging but having complementary planes so that, while not permitted to contact one another, generally achieve the greatest degree of compression by virtue of their respective vectors. The close placement of the converging fasteners also reduces the chance of gapping and misalignment of the joint after the compression plate has been secured to the adjacent bodies. The range of allowable trajectories for each of the fasteners may be configured via a selection of various inserts, each of which features a different pre-defined orientation relative to the holes of the plate.

[0107] FIG. 16 show a tool 350 according to one embodiment, which assists a surgeon in placement of a first and a second fastener through the plate. As shown, the tool 350 closely mimics the functionality of a jig, whereby the tool 350 permits registration via a primary fastener, or alternatively a temporary fastener 310. The tool 350 may comprise adjustable settings 320, 340 to lock the tool 350 in the precise location. The tool 350 is preferably adjustable in various dimensions, including by adjustment of the position of a first and a second alignment head 315 relative to the respective first and second apertures. Thus, an alignment head 315 may be positioned against any one fastener and then be adjusted to position the other alignment head 315 in the desired location for a second fastener. The alignment heads 315 provide the necessary alignment of the fasteners and may comprise indicia to facilitate the proper alignment. The use of multiple registration points allows a user to ensure that the tool is properly positioned before making adjustment to the adjustment heads. One or more of the registration points may be based upon a locking or non-locking fastener, a temporary or permanent fastener, or alternatively a segment of the plate or the inserts thereto. The tool 350 may also comprise a handle for positioning by the surgeon, and may comprise dials or gauges as depicted in FIG. 16.

[0108] Although specific aspects shown in these Figures are not expressly described, it should be understood that any of the features described above in connection with other embodiments apply equally to the embodiments of FIGS. 1-15C.

[0109] One having skill in the art will appreciate that embodiments of the present disclosure may have various sizes. The sizes of the various elements of embodiments of the present disclosure may be sized based on various factors including, for example, the anatomical variances of the patient, the person or other device operating with or otherwise using the components of the system, the surgical site location, physical attributes of the bodies and other anatomical features of a particular patient, and other dimensional variations including, for example, width, length and thickness, and the size of associated surgical tools or fasteners.

[0110] Any of the components described herein may be sized to only completement other components in a specific segment of the system, such as an insert being sized to only be received by a particular bore or collar of the system. Further, certain component(s) may comprise surface finishing, such as by electroplating, to imbue the components with coloring, shading, cross-hatching or other visually or tactile-observable features in order to aid identification of the component(s). Indicia may be included on the plate and/or segments of the plate to indicate a particular insert, screw, fastener, etc. to be used with that particular segment, or to indicate a sequence or order of performing various steps with the system described above. Indicia may also appear on an instrument or tool indicating which area of the system the particular instrument or tool is to be used, a direction for placing the instrument or tool, identifying a body or anatomical feature or landmark for accessing with the instrument or tool, etc.

[0111] While various embodiments of the present disclosure have been described in detail, it is apparent that modifications and alterations of those embodiments will occur to those skilled in the art. However, it is to be expressly understood that such modifications and alterations are within the scope and spirit of the present disclosure, as set forth in the following claims. For example, certain geometries have been shown where an armature is on one medial side of a plate, but could be reversed and still provide the same benefits as described herein. Similarly, armatures and collars could be lengthened or shortened or substituted for extensions, as described above, without departing from the novel concepts captured by the appended claims.

[0112] The foregoing discussion of the disclosure has also been presented for purposes of illustration and description. The foregoing is not intended to limit the disclosure to the form or forms disclosed herein. In the foregoing Detailed Description for example, various features of the disclosure are grouped together in one or more embodiments for the purpose of streamlining the disclosure. This method of disclosure is not to be interpreted as reflecting an intention that the claimed disclosure requires more features than are expressly recited in each claim. Rather, as the following claims reflect, inventive aspects lie in less than all features of a single foregoing disclosed embodiment.

[0113] The present inventions, in various embodiments, include components, methods, processes, systems and/or apparatuses substantially as depicted and described herein, including various embodiments, subcombinations, and subsets thereof. Those of skill in the art will understand how to make and use the present inventions after understanding the present disclosure. The present inventions, in various embodiments, include providing devices and processes in the absence of items not depicted and/or described herein or in various embodiments hereof, including in the absence of such items as may have been used in previous devices or processes, e.g., for improving performance, achieving ease and\or reducing cost of implementation.

[0114] Moreover, though the present disclosure has included description of one or more embodiments and certain variations and modifications, other variations and modifications are within the scope of the disclosure, e.g., as may be within the skill and knowledge of those in the art, after understanding the present disclosure. It is intended to obtain rights which include alternative embodiments to the extent permitted, including alternate, interchangeable and/or equivalent structures, functions, ranges or steps to those claimed, whether or not such alternate, interchangeable and/or equivalent structures, functions, ranges or steps are disclosed herein, and without intending to publicly dedicate any patentable subject matter.