Hip Arthroplasty Implants

Abstract

To provide an apparatus and method of removing a liner attached to an implanted acetabular shell.SOLUTION: At a surgical site where an acetabular shell 12 has already been implanted into a patient, a rim plate having a through opening is placed over the acetabular shell. A pilot hole is then drilled into the attached liner through the opening in the placed rim plate. After the drilling, the rim plate is removed to expose the drilled hole. A removal tool for removing the liner 14 from the acetabular shell is inserted into the drilled pilot hole. The attached liner is then disengaged from the implanted acetabular shell with the inserted removal tool.SELECTED DRAWING: Figure 3

Description

[Technical field]

[0001] (CROSS REFERENCE TO RELATED APPLICATIONS) This application is a continuation-in-part of U.S. patent application Ser. No. 17 / 024,876, filed September 18, 2020, which is a continuation-in-part of U.S. patent application Ser. No. 17 / 111,720, filed December 4, 2020, all of which are incorporated by reference herein.

[0002] FIELD OF THEINVENTION The present disclosure relates generally to hip arthroplasty, and more particularly to hip arthroplasty implants. [Background technology]

[0003] Hip arthroplasty, often referred to as hip replacement, is a surgical procedure used to reconstruct and replace surfaces in hip joints damaged by disease or injury, such as arthritis or hip fracture. A total hip arthroplasty replaces both the acetabulum and the femoral head, which contains the hip joint, against which the femur articulates. To replace the hip joint, a hip arthroplasty includes a femoral implant secured to the end of the femur, and an acetabular implant secured to the acetabulum, which forms a replacement articular surface that interfaces with the femoral implant. The femoral implant is pivotally coupled to the acetabular implant, thereby reconstructing the hip joint. Summary of the Invention

[0004] In one aspect of the present disclosure, an apparatus for removing a liner attached to an implanted acetabular shell is provided, the apparatus including a rim plate, a pilot hole drill tip, and a removal tool.

[0005] The rim plate has an opening and is adapted to be placed over the implanted acetabular shell. The pilot hole drill tip is sized to be inserted into the opening in the rim plate to create a pilot hole in the attached liner. The removal tool has an elongated shaft and a threaded tip extending from the shaft. The threaded tip is sized to be inserted into the pilot hole to remove the attached liner from the implanted acetabular shell.

[0006] In another aspect of the present disclosure, a method is provided for removing a liner attached to an implanted acetabular shell. A surgical site is accessed where an acetabular shell has already been implanted in a patient. A rim plate having a through opening is placed over the acetabular shell. Pilot holes are then drilled in the attached liner through the openings in the placed rim plate. After drilling, the rim plate is removed to expose the drilled holes. A removal tool is inserted into the drilled pilot holes. The attached liner is then disengaged from the implanted acetabular shell with the inserted removal tool.

[0007] In another aspect of the present disclosure, an implant removal instrument system is provided for removing a trial femoral head, preferably from a trial dual mobility (DM) mobile insert. A preferred system includes a trial femoral head, a trial mobile insert, a removal instrument, and an impactor for removing the trial femoral head from the trial mobile insert. The trial mobile insert with the femoral head attached is placed onto the removal instrument. An impaction tip of the impactor is inserted through an opening in the trial mobile insert, with its distal end configured to contact an outer surface of the attached femoral head. When a force is applied to the impactor, the attached trial femoral head is disengaged from the attached trial mobile insert.

[0008] Other objects and features of the present disclosure will be in part apparent and in part pointed out hereinafter. [Brief description of the drawings]

[0009] [Figure 1] FIG. 1 is a perspective view of an acetabular implant according to one embodiment of the present disclosure. [Diagram 2] FIG. 2 is a cross-sectional view of an acetabular implant. [Diagram 3] FIG. 2 is an exploded view of the acetabular implant. [Figure 4] FIG. 2 is a perspective view of the acetabular shell of the acetabular implant. [Diagram 5] FIG. 2 is a cross-sectional view of an acetabular shell. [Figure 6] FIG. 2 is an enlarged cross-sectional view of the acetabular shell. [Figure 7] FIG. 2 is a perspective view of an acetabular liner of an acetabular implant. [Figure 8] FIG. 2 is a cross-sectional view of an acetabular liner. [Figure 9] FIG. 2 is an enlarged cross-sectional view of the acetabular liner. [Figure 10] FIG. 13 is a perspective view of an acetabular shell according to another embodiment of the present disclosure. [Figure 11] FIG. 13 is a perspective view of an acetabular shell according to another embodiment of the present disclosure. [Figure 12] FIG. 13 is a perspective view of an acetabular shell according to another embodiment of the present disclosure. [Figure 13] FIG. 13 is a perspective view of an acetabular shell according to another embodiment of the present disclosure. [Figure 14] FIG. 13 is a perspective view of an acetabular shell according to another embodiment of the present disclosure. [Figure 15] FIG. 1 is a side view of a shell insert according to one embodiment of the present disclosure. [Figure 16] FIG. 13 is a perspective view of an acetabular implant according to another embodiment of the present disclosure. [Figure 17] FIG. 17 is a cross-sectional view of the acetabular implant of FIG. 16. [Figure 18] 17 is a cross-sectional view of the mobile insert of the acetabular implant of FIG. 16. [Figure 19A] FIG. 1 is a cross-sectional view of a shell insert according to one aspect of the present disclosure. [Figure 19B] FIG. 1 is a cross-sectional view of a shell insert according to one aspect of the present disclosure. [Figure 20A] 20 illustrates an exemplary anti-rotation protrusion of the shell insert of FIG. 19 according to one embodiment of the present disclosure. [Figure 20B] 20 illustrates an exemplary anti-rotation protrusion of the shell insert of FIG. 19 according to one embodiment of the present disclosure. [Figure 21] FIG. 13 is a cross-sectional view of a shell insert according to another aspect of the present disclosure. [Figure 22A] 1A and 1B are cross-sectional and perspective views, respectively, of a shell insert according to another aspect of the present disclosure. [Figure 22B] 1A and 1B are cross-sectional and perspective views, respectively, of a shell insert according to another aspect of the present disclosure. [Figure 23] 1 is a cross-sectional view of a shell insert attached to a rim plate according to one aspect of the present disclosure. [Figure 24A] FIG. 13 is a perspective view of a rim plate to which a shell insert is attached according to another aspect of the present disclosure. [Figure 24B] FIG. 13 is a perspective view of a rim plate to which a shell insert is attached according to another aspect of the present disclosure. [Figure 24C] FIG. 13 is a perspective view of a rim plate to which a shell insert is attached according to another aspect of the present disclosure. [Diagram 25] FIG. 1 is a side view of a pilot hole drill tip according to one aspect of the present disclosure. [Figure 26] FIG. 13 is a side view of a removal tool for removing a liner attached to an implanted acetabular shell. [Figure 27A] FIG. [Figure 27B] FIG. [Figure 28] FIG. 2 is a perspective top view of a rim plate placed on an acetabular shell. [Figure 29A] 13 illustrates the step of removing the liner from the acetabular shell. [Figure 29B] 13 illustrates the step of removing the liner from the acetabular shell. [Figure 29C]13 illustrates the step of removing the liner from the acetabular shell. [Diagram 30] 1 is a flow chart of a method for removing a liner from an acetabular shell. [Diagram 31] 13 illustrates another embodiment of a removal device for removing a liner attached to an acetabular shell implanted in a patient. [Diagram 32] 13 is a perspective view of another embodiment of a device for removing a liner attached to an acetabular shell. [Diagram 33] FIG. 33 is a perspective view of all the components of the removal device of FIG. 32. [Figure 34A] 33 illustrates the step of removing a liner from an acetabular shell using the removal device of FIG. 32. [Figure 34B] 33 illustrates the step of removing a liner from an acetabular shell using the removal device of FIG. 32. [Figure 34C] 33 illustrates the step of removing a liner from an acetabular shell using the removal device of FIG. 32. [Figure 35A] FIG. 13 is a perspective view of a trial mobile insert in a dual mobility hip replacement system. [Figure 35B] FIG. 35B is a cross-sectional view of the trial mobile insert of FIG. 35A. [Diagram 36] 35B illustrates the trial mobile insert of FIG. 35A placed onto a removal tool. [Figure 37] 13 shows a complete implant removal instrument system for removing the trial femoral head from the trial mobile insert. [Figure 38A] 1 shows a cross-sectional view of the removal tool system during the removal process. [Figure 38B] 1 shows a cross-sectional view of the removal tool system during the removal process.

[0010] The greyscale shading in the figures indicates the portion of the component cut by the cross section.

[0011] Corresponding reference characters indicate corresponding parts throughout the drawings. DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS

[0012] A variety of different systems and methods are disclosed herein for performing and administering a hip arthroplasty. The various systems for hip arthroplasty disclosed herein include an implant (e.g., an acetabular implant and its components) and an installation or arthroplasty instrument for installing the implant. The various methods for hip arthroplasty disclosed herein include a method for installing an acetabular implant.

[0013] 1-9, an acetabular implant for hip arthroplasty according to one embodiment of the present disclosure is generally designated by the reference numeral 10. In the illustrated embodiment, the implant 10 is a fixed-bearing implant. The implant 10 includes an acetabular shell 12, an acetabular liner 14, and a femoral head 16. The femoral head 16 is generally spherical and has a spherical outer surface. The femoral head 16 defines a stem cavity 18 that is sized and shaped to receive a stem (not shown) of a femoral implant (not shown) for coupling the femoral head to the femoral implant. In some embodiments, the femoral head 16 may be considered part of the femoral implant.

[0014] 4-6, the shell 12 is configured to be attached to a patient's acetabulum (not shown). Specifically, the shell 12 is implanted into the patient's acetabulum. The shell 12 includes a body (e.g., a generally spherical wall) having an outer surface 20 and an inner surface 22. The outer surface 20 and the inner surface 22 are generally spherical in shape. The outer surface 20 of the shell 12 is generally hemispherical in shape. The outer surface 20 may be porous to allow bone ingrowth into the shell 12 after the shell is placed in the bone to form a strong connection between the shell and the bone. The shell 12 has a proximal end 24 and a distal end 26. The shell's distal end 26 is generally located at the apex of the spherical body. The shell 12 includes (or defines) a central axis CA (e.g., a shell central axis) that extends between the proximal end 24 and the distal end 26. The central axis CA generally extends through the apex of the sphere. The inner surface 22 of the shell 12 defines a shell cavity 28. The shell cavity 28 is sized and shaped to receive the liner 14. The inner surface 22 of the shell 12 includes a tapered shell section 22A, a spherical shell section 22B, and a transition shell section 22C that extends generally between the tapered and spherical shell sections. The tapered shell section 22A is proximal to the spherical shell section 22B. The tapered shell section 22A tapers inwardly toward the central axis CA of the shell 12 as the tapered shell section extends distally toward the distal end 26. As such, the tapered shell section 22A has a generally frustoconical shape. In the illustrated embodiment, the tapered shell section 22A extends distally from the proximal end 24. The tapered shell section 22A is tapered at an angle α (as shown in FIG. 5) relative to the central axis CA (e.g., a line parallel to the central axis). Preferably, the angle α of the tapered shell section is within an inclusive range of about 10 degrees to about 30 degrees, more preferably within an inclusive range of about 15 degrees to about 25 degrees, more preferably about 19 degrees. For example, in one embodiment, the angle α of the tapered shell section 22A is about 18.8 degrees. The tapered shell section 22A and the transition shell section 22C extend circumferentially around the central axis CA. The spherical shell section 22B is generally spherically formed (e.g., is a partial sphere) with an apex generally aligned with the central axis CA. Other configurations of the shell 12 are within the scope of this disclosure.

[0015] The shell 12 includes (or defines) at least one fastener aperture 30. Each fastener aperture 30 is sized and shaped to receive a fastener (not shown), such as a bone screw, to secure the shell 12 to the acetabulum. Each fastener aperture 30 is disposed in the spherical shell section 22B of the inner surface 22. In the illustrated embodiment, the shell 12 includes three fastener apertures 30. The three fastener apertures 30 are in a triangular arrangement, although other arrangements are within the scope of the present disclosure. More or fewer fastener apertures 30 are also within the scope of the present disclosure. For example, the shell can include five fastener apertures 30. One embodiment of a shell 112 having five fastener apertures 30 is shown in FIG. 10, and another embodiment of a shell 212 having five fastener apertures 30 is shown in FIG. 11. The five fastener apertures 30 of the shell 112 are arranged in a generally X-shape. The five fastener openings 30 in shell 212 are arranged in approximately two circumferential rows stacked on top of one another, with the first row closest to the apex of spherical shell section 22B having two fastener openings and the second row furthest from the apex having three fastener openings radially offset from the two fastener openings in the first row. Other numbers and / or arrangements of fastener openings are within the scope of this disclosure. The large number of fastener openings 30 provides the surgeon with flexibility for placing fasteners within the acetabulum.

[0016] Referring back to FIG. 4, the shell 12 includes an instrument interlock structure 32. The instrument interlock structure 32 is configured to mate with a shell insert 90 (FIG. 15) to prevent the shell 12 from rotating relative to the shell insert when the shell and shell insert are coupled together. The shell insert 90 includes threads that mate with threads on the shell 12 (at the apex) to couple the shell and shell insert 90 together. The shell 12 includes a threaded opening 36 disposed at the apex of the spherical shell section 22B and thus generally aligned with the central axis CA. The shell insert 90 threads into the threaded opening 36 to couple to the shell 12. In the illustrated embodiment, the instrument interlock structure 32 includes an insert recess 34. The insert recess 34 is disposed at the apex of the spherical shell section 22B and thus generally aligned with the central axis CA. The insert recess 34 is sized and shaped to take advantage of the shell protrusion 92 of the shell insert 90. The insert recess 34 includes at least one anti-rotation segment 34A (e.g., lobe). In the illustrated embodiment, the insert recess 34 includes four anti-rotation segments 34A, although more or fewer anti-rotation segments 34A are within the scope of this disclosure. Each anti-rotation segment 34A is sized and shaped to receive a shell insert rotation prevention structure 92A (e.g., protrusion) to prevent the shell 12 from rotating about the central axis CA when the shell and shell insert 90 are coupled together. Each anti-rotation segment 34A is offset from the central axis CA. When the shell insert 90 and shell 12 are coupled together, the shell protrusion 92 extends into (e.g., mates with or aligns with) the insert recess 34 (e.g., each anti-rotation structure 92A extends into one of the anti-rotation segments 34A). The engagement between shell protrusion 92 and shell 12 at insert recess 34 (e.g., between anti-rotation structure 92A and the shell at anti-rotation section 34A) prevents the shell from inadvertently rotating (e.g., about central axis CA) and potentially becoming unthreaded (e.g., unscrewed) from shell insert 90, particularly when the insert is not threaded into the central threaded hole of shell 12.

[0017] The insert recess 34 may have generally any shape. In the illustrated embodiment, the insert recess 34 has a generally circular shape with four anti-rotation segments 34A extending radially outwardly at equal intervals from the circumference of the circle. Other configurations of the instrument interlock structure 32 are within the scope of this disclosure. For example, the insert recess can have other shapes and sizes. Whatever the shape and size of the insert recess, it is understood that the shell protrusion of the shell insert 90 has a corresponding (e.g., determined, matching) size and shape.

[0018] 10 and 11, an insert recess for a shell 112, 212 according to another embodiment of the present disclosure is generally designated by the reference numeral 134. In this embodiment, the insert recess 134 has a generally circular shape with two anti-rotation segments 134A extending radially outwardly from the circumference of the circle in generally opposed relation.

[0019] 12, an insert recess for a shell 312 according to another embodiment of the present disclosure is indicated generally by the reference numeral 334. In this embodiment, the insert recess 334 has a generally polygonal (e.g., rectangular, square, etc.) shape with corners (e.g., rounded corners) that form anti-rotation sections 334A. Other polygonal shapes are within the scope of the present disclosure.

[0020] 13, an insert recess for a shell 412 according to another embodiment of the present disclosure is indicated generally by the reference numeral 434. In this embodiment, the insert recess 434 has a generally triangular shape with a generally central circular section and three anti-rotation sections 434A having generally triangular or trapezoidal shapes extending radially outwardly at equal intervals from the circular section.

[0021] 14, an insert recess for a shell 512 according to another embodiment of the present disclosure is generally indicated by the reference numeral 534. In this embodiment, the insert recess 534 has a star shape (e.g., a rounded star shape) that forms an anti-rotation section 534A. In the illustrated embodiment, the star shape of the insert recess 534 has four points, although more or less points are within the scope of the present disclosure.

[0022] 7-9, the liner 14 of the implant 10 is configured to be attached to the shell 12. In particular, the liner 14 is sized and shaped to be disposed within the shell cavity 28 of the shell 12 (e.g., the shell cavity is sized and shaped to receive the liner). The liner 14 includes a body (e.g., a generally spherical wall) having an outer surface 38 and an inner surface 40. The outer surface 38 and the inner surface 40 are generally spherical in shape. The inner surface 40 defines a liner cavity 42. The liner cavity 42 is sized and shaped to receive at least one of a mobile insert or a femoral head 16, as described in more detail below. In the illustrated embodiment, the liner cavity 42 is sized and shaped to receive the femoral head 16. The inner surface 40 is generally hemispherical in shape. The inner surface 40 is smooth to allow the mobile insert or femoral head 16 received within the liner cavity 42 to articulate or pivot relative to the liner 14. Optionally, the inner surface 40 may be polished to a mirror finish, particularly if the component is metal. The liner 14 has a proximal end 44 and a distal end 46. The distal end 46 of the liner 14 is generally located at the apex of a spherical body. The liner 14 includes (or defines) a central axis CA1 (e.g., a shell central axis) that extends between the proximal end 44 and the distal end 46. The central axis CA1 extends generally through the apex of the sphere. When the liner 14 is coupled to the shell 12 (e.g., disposed within the shell cavity 28), the central axes CA, CA1 of the liner and shell are generally coextensive with one another.

[0023] The outer surface 38 of the liner 14 includes a tapered liner section 38A, a spherical liner section 38B, and a transition liner section 38C that generally extends between the tapered and spherical liner sections. The tapered liner section 38A is proximal to the spherical liner section 38B. The spherical liner section 38B generally corresponds to (e.g., is generally sized and shaped to match) the spherical shell section 22B of the shell 12. The liner 14 is designed to have a small gap between the spherical liner section 38B and the spherical shell section 22B because when the liner is inserted into the shell cavity 28 of the shell, the snap-fit ​​receiving portion 48 (see FIG. 6) and the snap-fit ​​retaining portion 50 (see FIG. 9) form a snap-fit ​​connection between the shell and the liner. Specifically, in one embodiment, the gap is preferably at least 0.1 mm and at most 0.4 mm. The gap provides the advantage of less friction between the liner 14 and the shell 12, reducing the chance of any shaving that may be harmful to the patient.

[0024] The spherical shell section 38B is generally spherical (e.g., a partial sphere) with an apex generally aligned with the central axis CA. The transition liner section 38C generally corresponds to (e.g., is sized and shaped to generally match) the transition shell section 22C of the shell 12 such that the transition liner section and the transition shell section generally mate (e.g., engage) when the liner 14 is coupled to the shell. In addition, the tapered liner section 38A generally corresponds to (e.g., is sized and shaped to generally match) the tapered shell section 22A of the shell 12 such that the tapered liner section and the tapered shell section generally mate (e.g., engage) when the liner 14 is coupled to the shell. The tapered liner section 38A has a taper that corresponds to (e.g., matches) the taper of the tapered shell section 22A of the shell 12. The tapered liner section 38A tapers inwardly toward the central axis CA1 of the liner 14 as the tapered liner section extends distally toward the distal end 46. Thus, the tapered liner section 38A has a generally frustoconical shape. In the illustrated embodiment, the tapered liner section 38A extends distally from the proximal end 44. The tapered liner section 38A tapers at an angle β (FIG. 8) relative to the central axis CA1 (e.g., a line parallel to the central axis). Preferably, the angle β of the tapered shell section is within the range of about 10 degrees to about 30 degrees (excluding 5 degrees to about 15 degrees), more preferably within the range of about 15 degrees to about 25 degrees (excluding 7.5 degrees to about 12.5 degrees), more preferably about 19 degrees (excluding 9.5 degrees). Preferably, the angle β is slightly greater than the angle α of the taper of the tapered shell section 22A. For example, in one embodiment, the angle β of the tapered liner section 38A is approximately 19 degrees. Angle β, which is slightly greater than angle α, ensures that the tapered liner section 38A is received by and engages with an interference fit with the tapered shell section 22A. The tapered liner section 38A is configured to engage the tapered shell section 22A to prevent movement of the liner 14 relative to the shell 12 when the liner is disposed within the shell cavity 28 of the shell. When coupled together, the tapered liner section 38A and the tapered shell section 22A engage each other to prevent movement of the liner 14 relative to the shell 12.Specifically, engagement of tapered liner section 38A and tapered shell section 22A prevents liner 14 from rotating relative to shell 12 about an axis of rotation perpendicular to central axes CA, CA1. Tapered liner section 38A and transition liner section 38C extend circumferentially about central axis CA1. Other configurations of the liner are within the scope of this disclosure.

[0025] The liner 14 is constructed using (e.g., may be made from) any suitable material, such as plastic, metal (such as cobalt chrome alloy), or ceramic. In certain applications, such as dual mobility applications (described in more detail below), it may be preferable to construct the liner from ceramic, as ceramics are harder and smoother than metals and provide better wear or bearing surfaces (e.g., inner surface 38 and / or inner surface 40). Ceramic liners are also good at preventing particle generation due to micromotion between the liner 14 and the shell 12, and then the metal liner.

[0026] 2, 6 and 9, the shell 12 and the liner 14 have corresponding connectors that secure the shell and the liner together when the liner is disposed within the shell cavity 28 of the shell. In the illustrated embodiment, the shell 12 and the liner 14 form a snap-fit ​​connection therebetween to couple and secure the shell and the liner together. The shell 12 includes a snap-fit ​​receiving portion 48 and the liner 14 includes a snap-fit ​​retaining portion 50 that is sized and shaped to be received by the snap-fit ​​receiving portion to form a snap-fit ​​connection between the shell and the liner when the liner is inserted into the shell cavity 28 of the shell. The snap-fit ​​receiving portion 48 includes a generally circumferential recess 52 and the snap-fit ​​retaining portion 50 includes a generally circumferential lip 54 (e.g., a detent, a catch) that is sized and shaped to be received by (e.g., inserted into) the recess. The circumferential recess 52 and the circumferential lip 54 extend circumferentially about the central axis CA, CA1. The lip 54 is resiliently deflectable to allow the liner 14 to be inserted into the shell cavity 28 of the shell 12. When the liner 14 is inserted distally into the shell cavity 28 of the shell 12, the shell (e.g., the tapered shell section 22A) deflects or deforms the lip 54. When the lip 54 aligns with the recess 52, the lip quickly recovers to its undeformed state (FIG. 9) and extends into the recess, forming a snap-fit ​​connection that secures the liner to the shell (FIG. 2). Other configurations of connectors that secure the shell and liner to one another are within the scope of this disclosure.

[0027] 2, 4, 5, 7 and 9, the shell 12 and the liner 14 may include corresponding interlocking structures to prevent movement (e.g., rotation) of the shell and the liner relative to one another. In the illustrated embodiment, the shell 12 includes at least one shell interlocking structure 56 and the liner 14 includes at least one liner interlocking structure 58. Preferably, the shell 12 includes multiple shell interlocking structures 56 and the liner 14 includes multiple liner interlocking structures 58. In the illustrated embodiment, the shell 12 includes twelve shell interlocking structures 56 and the liner 14 includes twelve liner interlocking structures 58, although more or fewer shell and liner interlocking structures are within the scope of the present disclosure. For example, the shell may include six shell interlocking structures and the liner may include six liner interlocking structures. The multiple shell interlocking structures 56 are circumferentially spaced apart from one another (around the central axis CA of the shell 12). Similarly, the liner interlocking structures 58 are circumferentially spaced apart from one another (around the central axis CA1 of the liner 14). Each shell interlocking structure 56 is configured to mate (e.g., interlock) with one of the liner interlocking structures 58 to prevent rotation of the liner 14 about the central axis CA, CA1 relative to the shell 12 when the liner is disposed in the shell cavity 28 of the shell. The shell interlocking structure 56 includes an interlocking recess 60, and the liner interlocking structure 58 includes an interlocking protrusion 62 sized and shaped to be received by the interlocking recess. In other words, the interlocking recess 60 and the interlocking protrusion 62 have corresponding (e.g., matching) shapes and sizes. In the illustrated embodiment, the shell interlocking structure 56 is disposed generally adjacent to the proximal end 24 of the shell 12. The liner interlocking structure 58 is also disposed generally adjacent to the proximal end 44 of the liner 14. When the shell 12 and liner 14 are coupled together, each interlocking protrusion 62 extends into (eg, fits, aligns, or interlocks with) one of the interlocking recesses 60 .Engagement between interlocking protrusions 62 of liner 14 and shell 12 at interlocking recesses 60 prevents the liner from inadvertently rotating relative to the shell (eg, about central axes CA, CA1).

[0028] 16-18, another embodiment of an acetabular implant according to the present disclosure is shown generally at 110. Implant 110 is generally similar to implant 10, and therefore, unless expressly stated or indicated otherwise, the description herein of implant 10 (and its elements, such as shell 12 and liner 14) also applies to implant 110. In this embodiment, the primary difference between implant 10 and implant 110 is that implant 110 is a dual mobility implant. Thus, implant 110 further includes a mobile insert 180. Mobile insert 180 is disposed between liner 114 and femoral head 116 and is capable of articulating (e.g., rotating) relative to both the liner and femoral head.

[0029] The mobile insert 180 is configured to couple to both the liner 114 and the femoral head 116. In particular, the mobile insert 180 is sized and shaped to be disposed (e.g., received) within the liner cavity 142 of the liner 114. In this embodiment, the liner cavity 142 of the liner 114 is sized and shaped to receive the mobile insert 180. The mobile insert 180 includes a body (e.g., a generally spherical wall) having an outer surface 182 and an inner surface 184. The mobile insert 180 has a proximal end 178 and a distal end 176 (generally at the apex of the sphere) with a central axis CA2 (e.g., the mobile insert central axis) extending therebetween (and through the apex of the sphere). In the position shown in FIG. 17, the central axis CA2 (see FIG. 18) of the mobile insert 180 is generally coextensive with the central axes CA, CA1 of the shell 612 and the liner 114. The outer surface 182 and the inner surface 184 are generally spherical. The outer surface 182 is smooth to allow the mobile insert 180 to articulate or pivot relative to the liner 114 (e.g., slide over the inner surface 140 of the liner). The spherical outer surface 182 forms a majority of a sphere. For example, in one embodiment, the height (e.g., the height of the outer surface 182) of the mobile insert 180 (extending between the proximal end 178 and the distal end 176) is within a range of about 55% to about 75% of the outer diameter (e.g., the diameter of the outer surface) of the mobile insert, or more preferably within a range of about 60% to about 70% of the outer diameter, or even more preferably about 65% of the outer diameter. This larger outer surface 182 increases the range of motion between the mobile insert 180 and the liner 114 over conventional mobile inserts, which are typically only hemispherical.

[0030] The inner surface 184 of the mobile insert 180 defines a mobile insert cavity 186 sized and shaped to receive the femoral head 116. The inner surface 184 is smooth to allow the mobile insert 180 to articulate or pivot relative to the femoral head 116 (e.g., to allow the femoral head to slide on the inner surface of the mobile insert). The mobile insert 180 is configured to be attached to the femoral head 116 to prevent the mobile insert and the femoral head from separating from one another. In the illustrated embodiment, the mobile insert 180 is configured to form a snap-fit ​​connection with the femoral head 116. The inner surface 184 has a proximal rim 185. The inner surface 184 extends proximally in a generally spherical manner from the apex of the sphere to the proximal rim 185. In the illustrated embodiment, the proximal rim 185 is distal to the proximal end 178. Like the outer surface 182, the inner surface 184 forms a majority of the sphere. For example, in one embodiment, the height of the inner surface 184 (extending parallel to the central axis CA2 between the apex of the spherical inner surface 183 and the proximal rim 185) (e.g., the height of the mobile insert cavity 186) is within a range encompassing about 55% to about 75% of the inner diameter of the inner surface 184, or more preferably within a range encompassing about 60% to about 70% of the inner diameter, or even more preferably about 65% of the inner diameter. As a result, the proximal portion of the inner surface 184 generally tapers toward the central axis CA2 as it extends proximally toward the proximal rim 185. This proximal portion of the inner surface 184 retains the femoral head 116 within the mobile cavity 186. Thus, the inner surface 184 surrounds a majority of the spherical femoral head 116 and retains the femoral head within the mobile insert cavity 186. The mobile insert 180 is constructed using an elastically deflectable material. Thus, the mobile insert 180 (e.g., the proximal rim 185) is resiliently deflectable to allow the femoral head 116 to be inserted into the mobile insert cavity 186. When the femoral head 116 is inserted distally into the mobile insert cavity 186, the mobile insert deflects or deforms (e.g., the proximal rim 185 expands radially outward) to enlarge the proximal end of the mobile insert cavity and allow the femoral head to pass therethrough.Once the femoral head 116 enters the mobile insert cavity 186 (e.g., the widest portion of the femoral head passes the proximal rim 185), the mobile insert 180 returns to its undeformed state ( FIG. 18 ) or quickly recovers to its original state, forming a snap-fit ​​connection and securing the femoral head to the mobile insert. In one embodiment, an insertion tool or press (not shown) may be required to insert the femoral head 116 into the mobile insert cavity 186.

[0031] The mobile insert 180 may also include a stem escape recess 188 at the proximal end of the mobile insert cavity 186. The stem escape recess 188 is configured to receive (optionally intermittently receive) a stem (not shown) of a femoral implant as the femoral implant (e.g., femoral head 116) rotates relative to the mobile insert 180. This increases the possible range of motion between the femoral implant and the mobile insert 180. In the illustrated embodiment, the stem escape recess 188 is generally defined by an inner circumferential chamfer (e.g., a tapered inner surface) of the mobile insert 180 that extends between the proximal rim 185 and the proximal end 178 of the mobile insert. Other configurations of the mobile insert 180 are within the scope of this disclosure.

[0032] In addition to the mobile insert 180, the implant 110 has a liner 114 with a different configuration. The liner 114 does not include a snap-fit ​​retainer, such as the snap-fit ​​retainer 50, for securing the liner to the shell 612. In this embodiment, the liner 114 is preferably made of a ceramic or metal alloy, such as a cobalt chrome alloy, which may not generally be suitable for forming a snap-fit ​​retainer (e.g., the snap-fit ​​retainer may break instead of elastically deforming when inserted into the shell 612). In the illustrated embodiment, the shell 612 still includes the snap-fit ​​receiver 648, but in other embodiments, the snap-fit ​​receiver may be eliminated from the shell. Additionally, in this embodiment, the liner 114 does not include the liner interlocking structure 58. In the illustrated embodiment, the shell 612 still includes the shell interlocking structure 56, but in other embodiments, the shell interlocking structure may be eliminated from the shell. Additionally, in this embodiment, the liner 114 includes an alignment protrusion 189. The alignment protrusion 189 generally extends distally from an apex of the spherical outer surface 138 of the liner 114. The alignment protrusion 189 is configured to be inserted into a threaded opening 636 (broadly, an alignment recess) in the shell 612. It is understood that the alignment protrusion 189 may be configured to extend into a different recess (e.g., opening) in the shell 612. Insertion of the alignment protrusion 189 into the alignment recess 612 facilitates alignment and positioning (e.g., centering) of the liner 114 relative to the shell 612 when the liner 114 is coupled to the shell.

[0033] In surgery, to implant an acetabular implant such as implant 10 into a patient's acetabulum, the surgeon first prepares the acetabulum to receive the shell 12 of the implant. Preparing the acetabulum may include one or more of reaming, cutting, etc., to shape the acetabulum to receive the shell 12. The surgeon then couples the shell 12 to the shell inserter 90. This can be done by threading the shell 12 onto the threads of the shell inserter. Coupling the shell 12 to the shell inserter 90 includes inserting the shell projection 92 of the shell inserter into the instrument interlock structure 32 (e.g., the inserter recess 34) of the shell. The engagement of the instrument interlock structure 32 with the shell inserter 90 (e.g., the shell projection 92) while the shell and shell inserter are coupled together prevents rotation (and inadvertent separation) of the shell relative to the shell inserter, particularly while the shell is being implanted. The surgeon then uses the shell inserter 90 to implant the shell 12. The surgeon generally moves the shell inserter 90 with the shell 12 distally into the prepared section of the acetabulum. The surgeon may use a hammer (not shown) to access the shell inserter 90 and drive the shell 12 into the acetabulum. After the shell 12 is in place, the surgeon removes the shell inserter 90 from the shell 12. This requires disengaging (e.g., removing) the shell projections 92 from the instrument interlock structure 32 and unthreading (e.g., rotating) the shell inserter 90 from the shell 12. If desired, the surgeon may then insert one or more fasteners (not shown) through one or more fastener openings 30 to secure the shell 12 to the acetabulum.

[0034] Next, the liner 14 is inserted into the shell cavity 28 of the shell 12. The liner 14 is moved distally into the shell cavity 28. If the liner includes an alignment protrusion 189, such as the liner 114, the surgeon aligns the alignment protrusion with the alignment recess 36, 136 (e.g., a threaded opening in the illustrated embodiment). As the surgeon moves the liner 114 distally, the alignment protrusion 189 moves distally into the alignment recess 36, 136. Insertion of the liner 14 also includes mating one or more liner interlocking structures 58 with one or more shell interlocking structures 56. The surgeon rotates the liner 14 about the central axis CA1 such that the liner interlocking structures 58 are aligned with the shell interlocking structures 56. As the liner 14 is moved distally, the liner interlocking structures 58 mate with the shell interlocking structures 56. Specifically, each liner interlocking projection 62 moves into one of the interlocking recesses 60 (through its open proximal side). The engagement of the shell interlocking structure 56 with the liner interlocking structure 58 prevents rotation of the liner 14 about the central axis CA, CA1 relative to the shell 12. The engagement of the shell interlocking structure 56 with the liner interlocking structure 58 and the alignment projection 189 with the alignment recesses 36, 136 can occur substantially simultaneously. When the surgeon moves the liner 14 completely into the shell cavity 28, a snap-fit ​​connection is formed between the liner and the shell, securing the liner in the shell cavity of the shell. The tapered portion 38A of the liner 14 and the tapered portion 22A of the shell 12 also create an interference fit to secure the liner in the shell. In fact, the interference fit of the tapered portions due to the difference in angles α and β can secure the liner 14 to the shell 12 even without a snap-fit ​​connection. As the surgeon moves the liner 14 into the shell cavity 28, the lip 54 of the liner compresses and then expands (eg, quickly rebounds) into the recess 52 of the shell 12 as they are aligned.

[0035] In a fixed bearing implant such as implant 10, after the liner 14 is coupled to the shell 12, the surgeon then inserts the femoral head 16 (which may already be attached to the stem of the femoral implant) into the liner cavity 42 of the liner. In a dual mobility implant such as implant 110, the surgeon first attaches the mobile insert 180 to the femoral head 116 before inserting the mobile insert (and femoral head) into the liner cavity 142 of the liner 114. The femoral head 116 may be attached to the stem of the femoral implant after being coupled to the mobile insert 180. To attach the mobile insert 180 to the femoral head 116, the surgeon moves the femoral head distally into the mobile insert cavity 186. As the femoral head 116 moves into the mobile insert cavity 186, it expands the mobile insert 180 (e.g., the proximal end of the mobile insert cavity) and then the mobile insert retracts (e.g., quickly returns to its original state) once the femoral head is in the mobile insert cavity. In one embodiment, the surgeon uses an instrument or press to couple the mobile insert 180 and the femoral head 116 together. The surgeon then inserts the mobile insert 180 along with the femoral head 116 into the liner cavity 142 of the liner 114.

[0036] The order of execution or performance of operations in embodiments of aspects of the disclosure described herein is not essential unless specifically stated or otherwise indicated. That is, operations may be performed in any order and / or simultaneously, and embodiments of aspects of the disclosure may include additional or fewer operations than those disclosed herein. For example, performing or executing a particular operation before, contemporaneously with, or after another operation is contemplated to be within the scope of the disclosure.

[0037] As will be apparent, the implants 10, 110 and elements thereof disclosed herein are generally similar to one another, and therefore, for ease of understanding, when similar, similar, or identical parts are used among various different implants (or elements thereof), reference numbers having the same last two digits are used (and the same subsequent letters are used, if applicable). For example, shell 12 is similar to shells 112, 212, 312, 412, 512, and 612, and therefore, all of these shells have the same last two digits "12". Thus, unless expressly stated otherwise, the above description of the implants and elements thereof applies equally to all similar implants and elements thereof. For example, at least some of the description of insert recess 34 may also apply to insert recess 134, and / or vice versa. As another example, at least some of the discussion regarding the inner surface 22 of shell 12 (eg, tapered shell section 22A, spherical shell section 22B, and transition shell section 22C) applies equally to shells 112, 212, 312, 412, 512, and 612.

[0038] Regarding the materials of each component for dual mobility applications as shown in FIG. 17, in one embodiment, the acetabular shell 12 may be made of a metal such as a titanium alloy, and the liner 14 may be made of either a ceramic material or a metal such as a cobalt chrome alloy. For a ceramic material, the preferred material may be aluminum oxide (Al2O3). A ceramic material for the liner 14 may be preferred when the fit between the liner and the shell 12 is not perfect and the two materials rub against each other. Metal-on-metal friction due to micro-motion may remove metal shavings or particles. The mobile insert 180 may be made of a polyethylene material such as compression molded GUR1020E material. The femoral head 160 may be made of a metal such as a cobalt chrome alloy, or a ceramic material, aluminum oxide (Al2O3) material.

[0039] 19A-24C disclose an impaction instrument system for seating an acetabular shell within the acetabular space. When seating an acetabular shell using a conventional impaction instrument having a tip threaded into a central bore 36, it is possible that a user may inadvertently disengage the instrument while orienting the shell within the acetabular space. It is therefore desirable to provide an impaction instrument that prevents a user from loosening or disengaging the instrument from the shell.

[0040] 19A and 19B illustrate a shell inserter 200 with anti-rotation control according to an embodiment of the present disclosure. The instrument 200 has a hollow outer shaft 202 and an inner shaft 204 disposed within the outer shaft. The outer shaft 202 includes a distal sleeve 208 and an impactor sleeve 206 extending proximally from a proximal end of the distal sleeve 208. The impactor sleeve 206 includes an impactor head 210. In the illustrated embodiment, the outer shaft 202 is a single, integral part formed from a single piece of metal. In other embodiments, the distal sleeve 208 of the outer shaft 202 and the impactor sleeve 206 may be made from two separate parts that are attached to one another, such as by welding. The impactor sleeve 206 has an internal flat stop 212 that engages a corresponding stop 214 on the inner shaft 204.

[0041] As shown in Figures 20A and 20B, the distal end of the outer shaft 202 has anti-rotation protrusion features 216, 218 that are complementary in shape to the anti-rotation recesses 34, 134, 334 of the acetabular shell 12. For example, Figure 20A has a circular protrusion 216 and four evenly spaced semi-circular protrusions extending laterally from the circular protrusion. The protrusion 216 of Figure 20A is configured to be received in a complementary anti-rotation recess 34 of the acetabular shell 12 as shown in Figure 4, and the square protrusion 218 of Figure 20B is configured to be received in a complementary anti-rotation recess 334 of the acetabular shell 312 as shown in Figure 12.

[0042] The distal end portion 219 of the inner shaft 204 has external threads configured to be threaded into the internal threads of the central bore 36, as shown, for example, in FIG. 5. The proximal end portion of the inner shaft 204 has a key mechanism, such as a hex key, configured to receive a hex driver for threading the inner shaft 204 into the acetabular shell 12.

[0043] This anti-rotation feature of the present design provides rotational stability and is concentric or centered with the threaded central hole of the shell. The new shell inserter instrument mates with the rotation control feature of the shell and can be threaded into the tip / center hole of the shell for insertion and impaction of the acetabular shell. Finally, the rotation control feature allows for fully seated positioning of the shell without the possibility of unscrewing the inserter from the shell.

[0044] FIG. 21 shows an insert 220 according to another embodiment of the invention. Unlike the insert 220 of FIG. 19A, the impactor head 210 is part of the inner shaft 222. An annular stop 214 on the inner shaft 222 and a flat stop 212 on the outer shaft 208 capture an internal spring 226 to provide a constant bias of counterforce at all times. In the rest state, the insert 220 is in an unthreaded position. The inner shaft 222 is captured in the outer shaft 208 by a pin 234 in an annular recess defined by stops 230 and 232. The pin 234 is permanently attached to the impactor sleeve 224, for example by welding. The distal end portions of the inner shaft 222 and the outer shaft 208 are the same as those in FIGS. 19A-B and 20A-B.

[0045] 22A and 22B show an insert 238 according to another embodiment of the invention. Unlike the other inserts, the insert 238 is comprised of a single shaft 240 with an integrated impaction head 242. The shaft 240 includes a distal end portion with a distal projection 244 having a lower outer surface designed to seat flush against the surface of the recess 34 without any rotational control, and a threaded tip 246 extending distally of the distal projection 244. When the threaded tip 246 is threaded into the threaded central bore 36, the distal projection 244 does not engage the key feature of the recess 34, and therefore the insert 238 can rotate relative to the acetabular shell 12 about the longitudinal axis of the central bore 36, possibly with some resistance.

[0046] 23 is a cross-sectional view of a shell inserter 200 attached to a rim plate, according to one embodiment of the present disclosure. The use of a rim plate is intended to be an optional secondary step after the initial impaction of the shell 12 into the acetabulum. This rim plate impaction method allows for a larger contact surface area where the impaction force is spread evenly across the outer surface of the shell. This helps ensure proper seating of the shell 12 into the acetabulum. Although the rim plate impaction method is intended to be an optional secondary step, it may be a primary step without first impacting the shell 12 with the instrument 200 locked into the central opening 36 of the shell 12.

[0047] The insert 200 of FIG. 23 is identical to the insert of FIG. 19A, except that it is attached to a rim plate as shown in FIGS. 24A-C. The rim plate is designed to fit over the top surface of the acetabular shell. Like the acetabular shell, the rim plate 248 of FIG. 24A has a central hole 254 with internal threads and an anti-rotation recess 256. Like the recess of FIG. 20A, the recess 256 has a circular protrusion and four evenly spaced semicircular protrusions extending laterally from the circular protrusion. The rim plate 250 of FIG. 24B has a square shaped anti-rotation recess 258. FIG. 24C is a bottom perspective view of the rim plate 248 of FIG. 24A. Like the liner 14 of FIG. 7, the rim plate 248 has evenly spaced interlocking tabs 260 that rest on corresponding interlocking recesses 60 in the shell 12. In the embodiment shown, there are six tabs 260 that rest in six of the twelve recesses 60 in the shell 12 .

[0048] Although only the insert 200 is shown with the rim plate, any of the inserts disclosed herein may be used with any of the rim plates.

[0049] All of the inserts disclosed herein may be provided as part of a complete instrument kit.

[0050] 25-30 show one embodiment of an apparatus for removing a liner 14 attached to an acetabular shell 312 implanted in a patient. The apparatus includes a rim plate 700, a pilot hole drill tip 702, and a removal tool 704.

[0051] The rim plate 700 is similar to the rim plate of Figures 24A-24C and is adapted to be placed over the attached liner 14 and acetabular shell 312. The rim plate 700 has a pair of downwardly extending tabs 706 having conical outer surfaces that extend downwardly and inwardly. The recesses 60 of the acetabular shell 312 have corresponding conical surfaces for receiving and interlocking the tabs 706 of the rim plate 700. When the tabs 706 are received in the corresponding recesses 60, the rim plate 700 is rotatably coupled to the liner 14 and shell 312.

[0052] The rim plate 700 includes a set of drill guide openings 708 (six evenly spaced circumferentially as shown in FIG. 27A ) that guide the pilot hole drill tip 702 for drilling into the liner 14. Each opening 708 is angled inward toward the bottom center of the shell 312 to guide the pilot hole drill tip 702 into the attached liner 14.

[0053] The angle G of each opening 708 relative to the central axis of the acetabular shell 312 (or relative to a perpendicular to the flat upper surface of the rim plate 700) is preferably the same as the taper angle β (see FIG. 8) of the liner 14. As shown in FIGS. 27A-29C, the taper angle β and angle G of the openings 708 are in the range of 5 degrees to 15 degrees, and preferably about 9.5 degrees (including 19 degrees when considering the angles for the two opposing openings 708). This ensures that the pilot hole drill tip 702 maximizes engagement with the liner 14 and prevents damage to the implanted acetabular shell 312.

[0054] The pilot hole drill tip 702 includes a threaded portion 710 sized to be inserted into the opening 708 to create a pilot hole 718 in the attached liner 14, and a drill stop 712 disposed a predetermined distance proximal to the threaded portion 710 configured to contact an upper surface of the rim plate 700, thereby preventing the drill tip 702 from extending beyond the attached liner 14.

[0055] The removal tool 704 includes an elongated shaft 714 and a threaded tip 716 extending from the shaft 714. The threaded tip 716 is sized to be inserted into the pilot hole 718 formed by the pilot hole drill tip 702 to remove the attached liner 14 from the implanted acetabular shell 312.

[0056] The removal tool 704 includes a rounded end 720 distal to the threaded tip 716 to minimize damage to the inner surface of the implanted acetabular shell 312 .

[0057] The thread pitch of threaded tip 716 is finer than the thread pitch of pilot hole drill tip 702. The threaded portion of pilot hole drill tip 702 has a smaller diameter than the diameter of threaded tip 716 of removal tool 704.

[0058] FIG. 30 illustrates a method of removing the liner 14 attached to the implanted acetabular shell 312. In step 722, the user accesses the surgical site where the acetabular shell 312 will be implanted in the patient. In step 724, the user places the rim plate 700 having the openings 708 over the implanted acetabular shell 312 such that the tabs 706 interlock with the corresponding recesses 60 in the acetabular shell 312. In step 726, pilot holes 718 are drilled in the attached liner 14 through the openings 708 in the placed rim plate 700 until the drill stops 712 reach the bottom of the rim plate 700. In step 728, once the pilot holes 718 are drilled in the liner 14, the placed rim plate 700 is removed to expose the drilled holes.

[0059] In step 730 , the removal tool 704 is inserted into the drilled pilot hole 718 by threading the threaded tip 716 into the pilot hole 718 until the distal end of the threaded tip 716 contacts the acetabular shell 312 .

[0060] At step 732, the attached liner 14 is disengaged from the implanted acetabular shell 312 with the inserted removal tool 704. In one aspect, the threaded tip 716 of the removal tool 704 continues to thread into the attached liner 14 until it is disengaged from the acetabular shell 312. In the illustrated embodiment, the liner 14 is disengaged from the acetabular shell 312 when the circumferential lip 54 pops out of the circumferential recess 52.

[0061] FIG. 31 illustrates another embodiment of a device for removing a liner 14 attached to an acetabular shell 312 implanted in a patient. The device is similar to the device of FIG. 29, but also includes a modular dome 734 that can accommodate a particular size of liner. For example, there may be four modular domes 734 with outer diameters of 28, 32, 36, and 40 mm. In one aspect, the domes 734 are made of a plastic material. The rim plate 701 of FIG. 31 differs from the rim plate of FIG. 29 in that it does not include tabs 706, but includes a downwardly extending central projection 736 having male threads through its central axis. The male threads of the projection are adapted to be threadably received in a central threaded recess 738 of the modular dome 734. The spherical dome 734 is shaped to fit inside the liner 14 such that when the dome 734 is threaded onto the rim plate 701, the rim plate 701 seats onto the liner 14 and acetabular shell 312 to properly align the opening 708 with the liner 14. The angle of the opening 708 in Figure 31 is the same as in Figure 29.

[0062] The liner removal step is the same as that shown in Figure 30, except for the step of placing the rim plate. Instead of interlocking the tabs 706 with the corresponding recesses 60, the rim plate 701 with the attached domes 734 is placed onto the acetabular shell 312.

[0063] 32-34 show another embodiment of an apparatus 740 for removing a liner 14 attached to an acetabular shell 312 implanted in a patient. The apparatus 740 includes a rim plate 700 and a lever-type removal tool 742 centrally located on the rim plate.

[0064] The rim plate 700 is identical to the rim plate of FIG. 29 and has a gap so that when the attached liner 14 is disengaged from the acetabular shell 312, the liner 14 can move upwardly away from the shell 312.

[0065] The lever removal tool 742 is somewhat similar to the insertion tool 200 of FIG. 23 in that it includes a cannulated shaft 202 having a square key 764 that fits into the square anti-rotation recess 258. However, unlike the shaft 202 of FIG. 23, the shaft 202 also includes two pairs of lateral extensions 744, 746 with holes 748, 750 for rotatably coupling two gears 756, 758 of the lever arms 752, 754. The removal tool 742 also includes an inner shaft 760 that is received within the outer shaft 202 and has a screw tip front end 762 and a Hudson-type attachment 763 at its proximal end. Just behind the screw tip 762, the inner shaft 760 has a flat stop 763 to prevent the screw tip from being inserted into the liner 14 beyond a predetermined distance. An intermediate portion 768 of the inner shaft 760 has threads that threadably couple to the spur gears 756, 758 of the lever-action arms 752, 754. Two hexagonal cap screws 770 are inserted into the laterally extending holes 748, 750 to rotatably couple the two lever-action arms 752, 754 to the outer shaft 202, with the spur gears 756, 758 engaging the threads 768 of the inner shaft 760.

[0066] The outer shaft 202 is placed into the rim plate's anti-rotation control feature 258 (see FIG. 34A). The threaded tip inner shaft 760 is then advanced through the outer shaft 202 and threaded into the liner 14 approximately 6.5 mm when a flat stop 763 engages the liner 14, preventing the threaded tip 762 from being inserted further into the liner 14 (see FIG. 34B). As the inner shaft 760 advances downward, the lever-type arms 752, 754 rotate away from the acetabular shell 312 via the spur gears 756, 758. The user then rotates the arms 752, 754 toward the shell 312 just enough to overcome the engagement features 54, 52 of the liner 14 and shell 312 (see FIG. 34C). In the embodiment shown in FIGS. 34A-34C, the liner 14 disengages from the acetabular shell 312 when the circumferential lip 54 pops out of the circumferential recess 52.

[0067] The embodiment of Figures 32 and 33 may be advantageous to use as it does not require the additional pilot hole drill tip 702. The openings 708 are still present on the rim plate 700; however, they are not used in the embodiment of Figures 32 and 33. However, the openings 708 allow the rim plate 700 to be shared between different embodiments if they are both provided in the removal kit.

[0068] 35A-38B show an instrument removal system 772, and in particular a system for removing the trial femoral head from the trial DM mobile insert. The system 772 includes a trial femoral head 776, a trial mobile insert 774, a removal instrument 778, and an impactor 780 for removing the trial femoral head 776 from the trial mobile insert 774.

[0069] Prior to final implantation of a total hip arthroplasty implant, the surgeon will often try different implants to assess stability and leg length, and subject the leg to a full trial reduction, which verifies the final implant selection, including stem offset and head offset.

[0070] As previously discussed with reference to Figures 16-18, dual mobility (DM) constructs 110 are a growing market for at-risk patients. Many surgeons require a DM mobile insert trial to assess range of motion, stability, and leg length. The trial should represent an implant product that matches the inner and outer diameters of the DM mobile insert 180. The DM mobile insert and femoral head implant are sterile packaged separately and must be assembled using a press on a back table prior to implantation. The DM mobile insert holds the femoral head to prevent intra-prosthetic dislocation. The trial requires easy assembly and disassembly to determine the appropriate head offset of the final implant. The trial mobile insert 774 should still hold the trial femoral head 776 to allow for evaluation of the trial reduction.

[0071] Figures 35A and 35B show an exemplary DM trial mobile insert 774. The DM trial femoral head 776 is shown in Figures 38A and 38B. Both the trial femoral head 776 and the trial mobile insert 774 are made of a sulfone polymer material, in particular PPSU (Polyphenylsulfone), which has high resistance to impaction and high autoclave temperatures. PPSU material is available, for example, under the trade name Radel from Solvay SA (Brussels, Belgium).

[0072] In terms of shape, the trial mobile insert 774 is similar to the mobile insert 180 of FIG. 18. However, the trial mobile insert 774 includes a central through hole 782 and six V-shaped cuts 784 from its face that are uniformly spaced apart circumferentially to allow the mobile insert 774 to flex and be assembled with the trial femoral head 776 simply by the force of the user's hands. The six cuts 784 define six legs 786 that extend toward the face of the mobile insert 774.

[0073] In terms of shape, the trial femoral head 776 is similar to the femoral head 116 of Figure 17 for attachment to a femoral stem. Once the trial femoral head 776 is snapped into the trial mobile insert 774, the femoral head can be rotated in any direction.

[0074] 36 shows an exemplary removal tool 778 shaped to receive the trial mobile insert 774 with the trial mobile insert 774 attached. The removal tool 778 has six teeth 779 that fit into corresponding V-cuts 784. The bottom of the legs 786 rest on the wide recessed area defined by the teeth of the removal tool 778.

[0075] 38A-B, the removal tool 778 includes a through opening 794 that includes a first opening 796 having a larger diameter and a second opening 798 having a smaller diameter with a circumferentially tapered region 800 therebetween. When the trial mobile insert 774 is placed on the removal tool 778, the face of the trial femoral head 776 rests over the tapered region 800 (approximately midway between the proximal and distal ends of the first opening), as shown in FIG.

[0076] 37 illustrates an exemplary impactor 780. At its proximal portion, impactor 780 includes an impaction head 802, a shaft 804 extending distally from the impaction head, a smaller diameter impaction tip 806 adapted for insertion into central throughbore 782, and an impaction stop 808 disposed between the shaft and the impaction tip.

[0077] 38B , when a light force is applied to the impaction head 802, the distal end of the impaction tip 806 pushes the attached trial femoral head 776 downward until it disengages from the trial mobile insert 774 and rests on the tapered region 800. As shown, the impactor stop 808 is positioned to bottom out on the outer surface of the mobile insert 774 above the through opening 782 when the femoral head 776 is not present. However, in an alternative design, the impactor stop 808 can be positioned closer to the distal end of the impactor 780 such that when the trial femoral head 776 is disengaged from the trial mobile insert 774 and rests on the tapered region 800, the impactor stop 808 bottoms out on the mobile insert before it can exert any force on the trial femoral head 776 on which its distal end rests. This prevents the trial femoral head 776 from potentially being damaged by the force applied from the impactor 780 while the trial femoral head 776 is resting on the tapered region 800 .

[0078] It is clear and understood that the elements, features, and / or teachings described in each embodiment disclosed herein are not limited to the particular embodiment to which the elements, features, and / or teachings are described. Thus, it is clear and understood that elements, features, and / or teachings described in one embodiment may be applied to one or more of the other embodiments disclosed herein. For example, it is understood that any of the shells disclosed herein may have a configuration of fastener openings 30 in the shell 12.

[0079] Modifications and variations of the disclosed embodiments are possible without departing from the scope of the present disclosure, which is defined in the following claims.

[0080] When introducing elements of the disclosure or embodiments thereof, the articles "a," "an," "the," and "said" are intended to mean that there are one or more of the elements. The terms "comprising," "including," and "having" are intended to be inclusive and mean that there may be additional elements other than the listed elements.

[0081] Since various changes can be made in the above structures, products, and methods without departing from the scope of the present disclosure, all material contained in the above description and shown in the accompanying drawings is intended to be interpreted as illustrative.

Claims

1. 1. An apparatus for removing a liner attached to an implanted acetabular shell, comprising: a rim plate having an opening and adapted to be placed over the acetabular shell; a pilot hole drill tip sized to be inserted into the opening to create a pilot hole in the installed liner; a removal tool having an elongate shaft and a threaded tip extending from the shaft, the threaded tip sized to be inserted into the pilot hole to remove the attached liner from the implanted acetabular shell; the opening in the rim plate includes a plurality of circumferentially spaced openings, each of the openings angled to guide the pilot hole drill tip into the attached liner; The device is capable of replacing the rim plate with a rim plate having an opening whose respective angle is substantially the same as the taper angle of the liner to be removed, depending on a taper angle, which is the angle of a tapered liner section extending from a proximal end of the liner toward a distal end, relative to a central axis of the liner to be removed.

2. 2. The apparatus of claim 1, wherein the pilot hole drill tip includes a threaded portion and a drill stop disposed a predetermined distance proximal to the threaded portion configured to contact an upper surface of the rim plate, thereby preventing the pilot hole drill tip from extending beyond the attached liner.

3. The apparatus of claim 1 , wherein the opening in the rim plate is angled inwardly to guide the pilot hole drill tip into the installed liner.

4. The apparatus of claim 1 , wherein the rim plate includes a plurality of teeth adapted to be received in corresponding recesses in the implanted acetabular shell.

5. The device of claim 4 , wherein each tooth has a conical outer surface that mates with a conical inner surface of a corresponding recess in the implanted acetabular shell.

6. the pilot hole drill tip includes a threaded portion having a first diameter; The device of claim 1 , wherein the threaded tip of the removal tool has an outer diameter greater than the first diameter.

7. The apparatus of claim 6 , wherein a diameter of the opening in the rim plate is smaller than the outer diameter of the threaded tip.

Images