The present disclosure relates to spinal support systems and more particularly to reinforcement of spinal support systems and methods.
Spinal support systems utilizing pedicle screws and spinal rods disposed in rod receptacles or “tulips” have been used to support spinal vertebrae. The purpose of such systems vary. In some applications, the spinal support system is used in spinal fusion therapy to hold adjacent vertebrae stationary with respect to each other, enabling bone growth tissue to form. In some applications, the rods are placed in tension to correct spinal maladies (e.g., scoliosis).
The rod receptacles typically define diametrically oppose slots, with the spinal rod extending through the slots. The formation of the slots further define opposed wall segments that extend proximally on lateral sides of the spinal rod. The spinal rod is typically held within the slots with a set screw that threadably engages the wall segments.
Over time, creep stresses may cause the wall segments to deflect radially outward and away from the set screw, with an accompanying decrease the clamping force of the set screw against the spinal rod. This can cause loosening of the assembly and slippage of the resident spinal rod within the spinal rod receptacle. In some instances, torque requirements, particularly where the spinal rods are subject to high tension forces, can cause the set screw to slip within the spinal rod receptacle during implantation. A system that remedies these shortcomings of conventional spinal support systems would be welcomed.
In various embodiments of the disclosure, a spinal support system is disclosed where a unitary reinforcement cap threadably engages both the internal and the external surfaces of the wall segments of the rod receptacle. By doubling the number of threads that are engaged, additional strength and structural integrity are realized over standard set screw arrangements. Also, because of the unitary construction, wherein an internal set screw portion and an external skirt portion are integral to the reinforcement cap, lateral movement between the set screw portion and the skirt portion is limited.
In some embodiments, the unitary reinforcement cap does not threadably engage the external surface, but instead slidingly engages the external surface to provide support to the rod receptacle. Accordingly, such embodiments do not require the presence of threads on the external surface of the rod receptacle, and can be configured for a retrofit of conventional rod receptacles.
In some embodiments, the threads are of a canted cantilever construction, wherein the interfaces of threadably engaged components are tailored to generate reaction force vectors that prevent slippage at the interfaces.
Structurally, a reinforcement cap is disclosed for a spinal support system, comprising: a platform portion including a distal face and a proximal face separated by a perimeter portion; a skirt portion that extends from the distal face of the platform portion, the skirt portion including an interior surface, at least a portion of the interior surface including interior threads formed thereon; and a set screw portion that extends from the distal face of the platform portion, the set screw portion being surrounded by the skirt portion and including an exterior surface that faces radially outward, at least a portion of the exterior surface including exterior threads formed thereon, the set screw portion defining a rotation axis, the set screw portion and the skirt portion being concentric about the rotation axis to define an annular gap between the exterior threads of the set screw portion and the interior threads of the skirt portion. The skirt portion may include an exterior surface that is tangential with the perimeter portion. In some embodiments, the set screw portion extends distally beyond the skirt portion. The skirt portion may include an exterior surface that defines a plurality of flats, each of the plurality of flats being parallel to the rotation axis.
In some embodiments, the exterior threads of the set screw portion define a canted cantilever profile. Likewise, in some embodiments, the interior threads of the skirt portion define a canted cantilever profile. The canted cantilever profile of the set screw portion may slope in a distal direction and toward the rotation axis. The canted cantilever profile of the set screw portion may slope in a distal direction and away from the rotation axis.
In some embodiments, the platform portion defines a socket accessible from the proximal face, the socket being concentric with and extending along the rotation axis. The platform portion may also define a tapped center hole accessible from the proximal face, the tapped center hole being concentric with and extending along the rotation axis, the socket extending distally from the tapped center hole. The reinforcement cap may further define a center passage concentric with the rotation axis and extending from the socket through a distal end of the set screw portion.
In various embodiments of the disclosure, a spinal support system comprises the reinforcement cap as described above; and a spinal rod receptacle having a side wall that includes an interior surface and an exterior surface, the side wall defining a pair of diametrically opposed slots that extend axially along the side wall and are open at a proximal end of the spinal rod receptacle, the interior surface of the spinal rod receptacle defining interior threads, the exterior surface of the spinal rod receptacle defining first exterior threads, wherein the interior threads of the spinal rod receptacle are configured to mate with the exterior threads of the set screw portion of the reinforcement cap, and the exterior threads of the spinal rod receptacle are configured to mate with the interior threads of the skirt portion of the reinforcement cap. In various embodiments, a spinal rod is configured for insertion into the diametrically opposed slots. A pedicle screw may be disposed within the spinal rod receptacle, a shaft of the pedicle screw extending distally from the spinal rod receptacle.
In various embodiments of the disclosure, a method for securing a spinal support rod to a spinal rod receptacle is disclosed, comprising: (a) disposing a spinal support rod through diametrically opposed slots of a spinal rod receptacle; (b) threadably engaging interior threads of a skirt portion of a reinforcement cap with exterior threads of the spinal rod receptacle; (c) simultaneously with step (b), threadably engaging exterior threads of a set screw portion of the reinforcement cap with interior threads of the spinal rod receptacle; and (d) tightening the reinforcement cap against the spinal support rod. In some embodiments, step (d) includes driving the reinforcement cap with a tool that mates with a socket formed on the reinforcement cap. In some embodiments, step (d) includes driving the reinforcement cap with a tool that engages flats formed on the skirt portion of the reinforcement cap.
Referring to
The spinal rod receptacle 24 includes a side wall 82 having an interior surface 84 and an exterior surface 86 (
Referring to
The reinforcement cap 28a may define a socket 272 accessible from the proximal face 326 of the cap 28a. In the depicted embodiment, the socket 272 is hexagonal, but other geometries, such as a square, rectangle, octagon, cross, or star pattern may be utilized. In some embodiments, a center passage 276 extends from the socket 272 through a distal end 278 of the set screw portion 342. Herein, “proximal” refers to a direction 76 that is toward a surgeon during operation or implantation and away from a bone or patient (
Referring to
Referring to
Referring to
Functionally, the interior threads 94 of the spinal rod receptacle 24 are configured to mate with the exterior threads 344 of the set screw portion 342 of the reinforcement cap 28. For the reinforcement caps 28a and 28b, the exterior threads 96 of the spinal rod receptacle 24 are configured to mate with the interior threads 336 of the skirt portion 332 of the reinforcement cap 28, 28b. The socket 272 accommodates driving of the reinforcement cap 28, 28b with an appropriate mating wrench (e.g., hexagonal wrench for the depicted embodiment, or a square bit, rectangular bit, cross (PHILLIPS) bit, or star (TORX®) bit as appropriate). The flats 374, when implemented, provide an alternative way to apply torsion to the reinforcement cap 28, for example by use of socket tool that slides over and engages the flats 374. The flats 374 can also be used in so-called rescue situations, providing alternative gripping surfaces for removal of components of the spinal support system 20. The center passage 276 may be sized, for example, to accommodate sliding passage of a Kirschner wire or a guide rod.
The unitary structure of the set screw portion 342 with the platform portion 322 and skirt portion 344 provides additional structural strength and integrity relative to a separate cap and set screw arrangement. For example, the spinal support system 20 provides greater resistance to lateral forces because the set screw portions 342 is integrated with the platform portion 322, establishing a shear stress at a junction 368 of the screw portion 342 and the platform portion 322 that provides additional resistance to deformation relative to an assembly where the cap and set screw are separate components. The added strength and structural integrity provided by the integrated arrangement of the reinforcement cap 28 may be advantageous for high torque and high stress applications, such as scoliosis correction.
The tapped center hole 360 may function to facilitate mounting of an extension rod receptacle (not depicted). Arrangements for such extensible systems are disclosed at U.S. patent application Ser. No. 15/970,368, entitled “Extension Ready Spinal Support Systems”, filed on even date and owned by the owner of the present application, the disclosure of which is hereby incorporated by reference herein in its entirety.
Referring to
For configurations such as the depicted spinal support system 20, the wall segment 408 (e.g., wall segment 90 of the spinal support system 20) is, in some embodiments, not supported by any additional structure. In such embodiments, the wall segment 408 will tend to cause deflections 6o that deflect radially outward in response to the radial outward force FRO. As the wall segment 408 deflects radially outward, the overlap between the threads 406 and 408 at the interfaces 422 is reduced, thereby weakening the coupling between the set screw 404 and the wall segment 408. The tighter the draw on the set screw 404, the greater the radial outward force FRO and the greater the deflection of the wall segment 408, further decreasing the overlap at the interfaces 422. Accordingly, as the torque requirements of the conventional set screw 404 are increased, the coupling between the set screw 404 and the wall segment 408 becomes more tenuous. Over time, creep stresses may cause the deflection of the wall segment 408 and the attendant decrease in the overlap at the interfaces 422, causing the clamping force FC to reduce. This can cause loosening of the assembly and slippage of the resident spinal rod within the spinal rod receptacle 410. In some instances, torque requirements can cause the set screw 404 to slip within the spinal rod receptacle 410 during implantation.
A threaded arrangement utilizing threads having the canted cantilever profile arrangement 450 is schematically depicted at
However, unlike the conventional threaded arrangements 400, the contact interfaces 472 of the canted cantilever profiles 450 are sloped radially inward (i.e., toward the central axis 462) in the first direction 466. By this arrangement, the radial component FRR is vectored inward, toward the center axis 466. The forces so generated will tend to cause deflections 6i of the wall segment 458 that is radially inward in response to the radial inward force FRI. Because of the radial inward deflections 6i, the wall segments 458 tend to be supported by radial interference and friction with the set screw 454. Accordingly, the coupling between the set screw 454 and the spinal rod receptacle 460 provided by the canted cantilever profile arrangement 450 is stronger and can provide a greater clamping force FC than can the conventional threaded arrangement 400 of spinal rod receptacle 410.
For the spinal support system 20, the interior threads 94 of the rod receptacle 24 interact with the set screw portion 342 in the manner described attendant to the canted cantilever profile arrangement 450 of
Alternatively, the exterior threads 96 of the spinal rod receptacle 24 and the interior threads 336 of the skirt portion 332 may be of a conventional arrangement. Conventional threads, as described attendant to
Each of the additional figures and methods disclosed herein can be used separately, or in conjunction with other features and methods, to provide improved devices and methods for making and using the same. Therefore, combinations of features and methods disclosed herein may not be necessary to practice the disclosure in its broadest sense and are instead disclosed merely to particularly describe representative and preferred embodiments.
Various modifications to the embodiments may be apparent to one of skill in the art upon reading this disclosure. For example, persons of ordinary skill in the relevant arts will recognize that the various features described for the different embodiments can be suitably combined, un-combined, and re-combined with other features, alone, or in different combinations. Likewise, the various features described above should all be regarded as example embodiments, rather than limitations to the scope or spirit of the disclosure.
Persons of ordinary skill in the relevant arts will recognize that various embodiments can comprise fewer features than illustrated in any individual embodiment described above. The embodiments described herein are not meant to be an exhaustive presentation of the ways in which the various features may be combined. Accordingly, the embodiments are not mutually exclusive combinations of features; rather, the claims can comprise a combination of different individual features selected from different individual embodiments, as understood by persons of ordinary skill in the art.
Any incorporation by reference of documents above is limited such that no subject matter is incorporated that is contrary to the explicit disclosure herein. Any incorporation by reference of documents above is further limited such that no claims included in the documents are incorporated by reference herein. Any incorporation by reference of documents above is yet further limited such that any definitions provided in the documents are not incorporated by reference herein unless expressly included herein.
Unless indicated otherwise, references to “embodiment(s)”, “disclosure”, “present disclosure”, “embodiment(s) of the disclosure”, “disclosed embodiment(s)”, and the like contained herein refer to the specification (text, including the claims, and figures) of this patent application that are not admitted prior art.
For purposes of interpreting the claims, it is expressly intended that the provisions of 35 U.S.C. 112(f) are not to be invoked unless the specific terms “means for” or “step for” are recited in the respective claim.
This patent application claims the benefit of U.S. Provisional Patent Application No. 62/500,719, filed on May 3, 2017, and U.S. Provisional Patent Application No. 62/500,820, also filed May 3, 2017, the disclosures of which are hereby incorporated by reference in their entirety.
Number | Name | Date | Kind |
---|---|---|---|
5261912 | Frigg | Nov 1993 | A |
5520690 | Errico | May 1996 | A |
5669911 | Errico | Sep 1997 | A |
5672176 | Biedermann | Sep 1997 | A |
5782833 | Haider | Jul 1998 | A |
5882350 | Ralph | Mar 1999 | A |
5964760 | Richelsoph | Oct 1999 | A |
6074391 | Metz-Stavenhagen et al. | Jun 2000 | A |
6248105 | Schlapfer | Jun 2001 | B1 |
6296642 | Morrison et al. | Oct 2001 | B1 |
6440137 | Horvath | Aug 2002 | B1 |
6520963 | McKinley | Feb 2003 | B1 |
6585737 | Baccelli | Jul 2003 | B1 |
6835196 | Biedermann et al. | Dec 2004 | B2 |
6843791 | Serhan | Jan 2005 | B2 |
7156850 | Kim | Jan 2007 | B2 |
7291151 | Alvarez | Nov 2007 | B2 |
7445627 | Hawkes | Nov 2008 | B2 |
7896902 | Jeon | Mar 2011 | B2 |
RE42545 | Ralph et al. | Jul 2011 | E |
8083776 | Alvarez | Dec 2011 | B2 |
8257402 | Jackson | Sep 2012 | B2 |
8273109 | Jackson | Sep 2012 | B2 |
8337532 | McLean et al. | Dec 2012 | B1 |
8702758 | Wang et al. | Apr 2014 | B2 |
8747405 | Belliard | Jun 2014 | B2 |
8852241 | Datta | Oct 2014 | B2 |
8870928 | Jackson | Oct 2014 | B2 |
9023087 | Frankel et al. | May 2015 | B2 |
9277950 | Buttermann | Mar 2016 | B2 |
9427260 | Juchno | Aug 2016 | B2 |
9451994 | Whipple et al. | Sep 2016 | B1 |
9510867 | Garamszegi | Dec 2016 | B2 |
10149702 | Ewer | Dec 2018 | B2 |
20020082602 | Biedermann et al. | Jun 2002 | A1 |
20030125741 | Biedermann et al. | Jul 2003 | A1 |
20040249380 | Glascott | Dec 2004 | A1 |
20060079895 | McLeer | Apr 2006 | A1 |
20070055238 | Biedermann et al. | Mar 2007 | A1 |
20080287998 | Doubler et al. | Nov 2008 | A1 |
20100094353 | Shim et al. | Apr 2010 | A1 |
20100160981 | Butler et al. | Jun 2010 | A1 |
20110190821 | Chin et al. | Aug 2011 | A1 |
20120130436 | Haskins et al. | May 2012 | A1 |
20120215263 | Lee | Aug 2012 | A1 |
20120271365 | Daubs et al. | Oct 2012 | A1 |
20130345755 | Prajapati et al. | Dec 2013 | A1 |
20140094849 | Spratt et al. | Apr 2014 | A1 |
20140121703 | Jackson et al. | May 2014 | A1 |
20140135839 | Frankel et al. | May 2014 | A1 |
20140135854 | Dec et al. | May 2014 | A1 |
20140148858 | Dant et al. | May 2014 | A1 |
20140316475 | Parikh et al. | Oct 2014 | A1 |
20160242817 | Abbasi | Aug 2016 | A1 |
20180228518 | Carruth et al. | Aug 2018 | A1 |
Number | Date | Country |
---|---|---|
10-2010-0119303 | Nov 2010 | KR |
WO 2010028287 | Mar 2010 | WO |
WO 2010037098 | Apr 2010 | WO |
WO 2014052117 | Apr 2014 | WO |
WO 2014138736 | Sep 2014 | WO |
Entry |
---|
International Search Report for Application No. PCT/US2018/030928 dated Sep. 27, 2018 (3 pages). |
Number | Date | Country | |
---|---|---|---|
20180317973 A1 | Nov 2018 | US |
Number | Date | Country | |
---|---|---|---|
62500719 | May 2017 | US | |
62500820 | May 2017 | US |