Total artificial spino-laminar prosthetic replacement
10022238 ยท 2018-07-17
Assignee
Inventors
- Nathan C. Moskowitz (Rockville, MD, US)
- Mosheh T. Moskowitz (Rockville, MD, US)
- Eric Sugalski (Arlington, MA, US)
- Ahmnon D. Moskowitz (Rockville, MD, US)
Cpc classification
A61F2/4405
HUMAN NECESSITIES
A61F2002/30578
HUMAN NECESSITIES
A61F2002/30563
HUMAN NECESSITIES
A61F2310/00023
HUMAN NECESSITIES
A61F2002/449
HUMAN NECESSITIES
A61B17/7071
HUMAN NECESSITIES
A61F2002/30616
HUMAN NECESSITIES
A61F2002/30948
HUMAN NECESSITIES
A61F2002/30471
HUMAN NECESSITIES
International classification
Abstract
A total artificial spinous process (spino)-laminar prosthesis (TASP-LP) including a body having a portion forming a spinous process extending away from the body, a first lamina portion extending from a first side of the body, and a second lamina portion extending from a second side of the body, wherein the first lamina portion and the second lamina portion are disposed on opposite sides of the spinous process.
Claims
1. A total artificial spinous process (spino)-laminar prosthesis (TASP-LP) comprising: a hinge pin having a first end, a second end, and a pin body between the first end and the second end; a body comprising: a first winged spinous process-laminar hinged portion on a first side of the body, wherein the first winged spinous process-laminar hinged portion has a first wing extension and a first hinge connection, wherein the first winged spinous process-laminar hinged portion defines a first plurality of holes through the first winged spinous process-laminar hinged portion including at least one first screw hole defined through the first wing extension at an angle configured to allow a first screw to pass through and into natural lamina and at least one first hinge hole extending through the first hinge connection that is sized and configured to receive the hinge pin; and a second winged spinous process-laminar hinged portion on a second side of the body, wherein the second winged spinous process-laminar hinged portion has a second wing extension and a second hinge connection, wherein the second winged spinous process-laminar hinged portion defines a second plurality of holes through the second winged spinous process-laminar hinged portion including at least one second screw hole defined through the second wing extension at an angle configured to allow a second screw to pass through and into natural lamina and at least one second hinge hole extending through the second hinge connection that is sized and configured to receive the hinge pin, wherein the first winged spinous process-laminar hinged portion and the second winged spinous process-laminar hinged portion are disposed on opposite sides of the hinge pin with the hinge pin extending through at least part of the first and second pin holes of the first and second hinge connections so as to allow the first winged spinous process-laminar hinged portion to pivot with respect to the second winged spinous process-laminar hinged portion to vary a distance between the first and second wing extensions.
2. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first and second winged spinous process-laminar hinged portions define a spinous process that includes an opening for muscle or fascia suture attachment.
3. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first and second winged spinous process-laminar hinged portions define a spinous process that includes a plurality of openings for muscle or fascia suture attachment.
4. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first and second winged spinous process-laminar hinged portions define a spinous process that includes two lobes mimicking a natural anatomy of a spinal element.
5. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 4, wherein each of the two lobes includes an opening for muscle or fascia suture attachment.
6. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first and second winged spinous process-laminar hinged portions define a spinous process that includes a single lobe mimicking a natural anatomy of a spinal element.
7. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, further comprising: the first and second screws.
8. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 7, wherein each of the first and second screws comprises one of a translaminar screw, a flathead screw, and a self-tapping screw.
9. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 7, wherein a surface of each of the first winged spinous process-laminar hinged portion and the second winged spinous process-laminar hinged portion includes a recess surrounding the opening for receiving a head of the attachment device such that the head of the attachment device is countersunk into or flush with the surface.
10. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 7, wherein a surface of each of the first winged spinous process-laminar hinged portion and the second winged spinous process-laminar hinged portion engages the attachment device to lock the attachment device with the surface.
11. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein each of the first winged spinous process-laminar hinged portion and the second winged spinous process-laminar hinged portion includes a relief opening or groove that permits each of the first winged spinous process-laminar hinged portion and the second winged spinous process-laminar hinged portion to flex.
12. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein each of the first winged spinous process-laminar hinged portion and the second winged spinous process-laminar hinged portion includes a thinned portion having a thickness that is less than a thickness of an adjacent portion, thereby permitting each of the first winged spinous process-laminar hinged portion and the second winged spinous process-laminar hinged portion to flex at the thinned portion.
13. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, and further comprising means for muscle suture attachment.
14. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first winged spinous process-laminar hinged portion defines two screw holes in addition to the first screw hole and the second winged spinous process-laminar hinged portion defines two screw holes in addition to the second screw hole, and further comprising: six screws configured for attaching the total artificial spinous process (spino)-laminar prosthesis (TASP-LP) to natural lamina.
15. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first winged spinous process-laminar hinged portion extends from the first wing extension to the first hinge connection without an additional hinge pin in-between and the second winged spinous process-laminar hinged portion extends from the second wing extension to the second hinge connection without an additional hinge pin in-between.
16. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein first wing extension has a flat bottom surface and wherein the first winged spinous process-laminar hinged portion has a curved portion between the first wing extension and the first hinge portion.
17. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first hinge hole, the second hinge hole, and the hinge pin are axially aligned about a hinge axis and wherein the first and second screw holes have axes that are substantially perpendicular to the hinge axis in neutral, elevated, and depressed positions of the total artificial spinous process (spino)-laminar prosthesis (TASP-LP).
18. The total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, wherein the first hinge hole, the second hinge hole, and the hinge pin are axially aligned about a hinge axis, wherein a first surface of the first hinge connection and a second surface of the second hinge connection each extend in a plane perpendicular to the hinge axis, and wherein the first surface faces the second surface and abuts the second surface.
19. A method of operating the total artificial spinous process (spino)-laminar prosthesis (TASP-LP) of claim 1, the method comprising: pivoting the first winged spinous process-laminar hinged portion with respect to the second winged spinous process-laminar hinged portion about the hinge pin to achieve an appropriate distance between the first and second wing extensions prior to securing the first and second wing extensions to the natural lamina; and securing the first wing extension to a left side of natural lamina via at least one first screw and securing the second wing extension to a right side of natural lamina via at least one second screw.
20. The method of claim 19, and further comprising: passing a suture through muscle and one or more spinous process perforations defined by the total artificial spinous process (spino)-laminar prosthesis (TASP-LP) to anatomically connect the muscle to the total artificial spinous process (spino)-laminar prosthesis (TASP-LP).
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) These and other aspects and features of embodiments of the present invention will be better understood after a reading of the following detailed description, together with the attached drawings, wherein:
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DETAILED DESCRIPTION OF THE EXEMPLARY EMBODIMENTS OF THE INVENTION
(45) The present invention now is described more fully hereinafter with reference to the accompanying drawings, in which embodiments of the invention are shown. This invention may, however, be embodied in many different forms and should not be construed as limited to the embodiments set forth herein; rather, these embodiments are provided so that this disclosure will be thorough and complete, and will fully convey the scope of the invention to those skilled in the art.
(46) Referring now to the drawings,
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(48) The total prosthetic module 10 can include, for example, a prosthetic spinous process 12 and left prosthetic lamina 14 and right prosthetic lamina 16. The prosthetic spinous process 12 can include perforations 20 for muscle suture attachment. The left prosthetic lamina 14 and right prosthetic lamina 16 can include screw attachments 18 for receiving translaminar screws 22.
(49) An exemplary embodiment of a cervical TASP-LP construction can be based on a 3-D CT computer rendition which very closely recreates the natural geometric anatomy of the healthy human cervical spine. Hence, an exemplary embodiment of a cervical prosthetic spinous process 12 of the TASP-LP 10 can be bifid (i.e., divided into two lobes), just like the predominant bifid spinous process anatomy of the natural cervical spine 30.
(50) Likewise, using 3-D computer modeling software, in an exemplary embodiment, the slope and angulations of the prosthetic spinous process 12, and of left and right prosthetic lamina 14, 16, can be rendered in accord with the natural spinous process 34 and of left and right natural lamina 30, 32 of the healthy natural cervical spine 30. Hence, as illustrated in the exemplary embodiment of
(51) With reference to
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(54) The exemplary embodiments of the prosthetic spinous process 12 can include perforations 20 on either side of the bifid process 12 to enable suturing of cervical muscles and fascia to the prosthetic spinous process 12, to reconstruct the normal cervical muscular architecture. The left and right prosthetic lamina 14, 16 can include, for example, two perforations 18 on its extensions, thereby enabling the fixation of the TASP-LP to the natural lamina (
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(57) In other exemplary embodiments, the different modules can be manufactured in different heights, lengths, and widths so that the surgeon can select from the properly sized one to integrate with the selective anatomy of different patients.
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(61) An exemplary prosthetic spinous process 12 can include perforations to enable suturing of Thoracic/Lumbar muscles and fascia to the prosthesis, to reconstruct the normal muscle orientation and architecture. The left and right prosthetic lamina can include, for example, three perforations on its extensions, which can enable the fixation of the TASP-LP to the natural lamina by trans-laminar screws as exemplarily illustrated in
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(65) The different modules 100a, 100b, 100c can be manufactured in different heights, lengths, and widths so that the surgeon can select from different sizes to accommodate for differences in patient anatomy.
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(71) For example,
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(75) The exemplary embodiments of a TASP-LP can be made of any bio-compatible material including, for example, polyether ether ketone (PEEK) (e.g., a colourless organic polymer thermoplastic), titanium steel, allograft bone, or other suitable materials, etc.
(76) The exemplary embodiments of a TASP-LP can include pins as well as screws, or other suitable fasteners. The pins can be, for example, flat or round. The pins can include, for example, fish hooks or ridges. The pins can be part of the device or a separate attachment for slots. For example, an apparatus can be used to hold the pin in place while it is being hammered or stapled into the prosthesis.
(77) An exemplary embodiment of the TASP-LP can look like a lamina/spinous process or occupy the space of a lamina/spinous process, or be of any variant shape. The TASP-LP can include, for example, one piece, or two or more pieces assembled together. The pieces can include curves or be straight. The device can have different shapes, such as rectangular, triangular, curved or arch shaped, including for example: triangular arch, round arch, segmental arch, rampant round arch, lancet arc, equilateral pointed arch, shouldered flat arch, cusped arch, horseshoe arch, three centered arch, jack arch, inflexed arch, ogee arch, reverse ogee arch, a parabolic arch, or similar such arcs.
(78) Other exemplary embodiments of the prosthesis can include a joint in the center or the sides for moveability. The exemplary prosthesis can include a ball joint, screw joint, revolute joint, cylindrical joint, gliding joint, mechanical linkage joints, hinges, or any other suitable joint or feature which accomplishes the same function.
(79) Other exemplary embodiments of the prosthesis can comprise bearings, for example, such as a bushing for absorbing shock.
(80) In other exemplary embodiments, the prosthesis can be movable like a clip or hinge. The exemplary prosthesis can be made of flexible material and/or can be spring like.
(81) In another exemplary embodiment, a set or kit of a plurality of prostheses can be provided, each having different standard sizes, such that a surgeon easily can select one or more appropriately sized prostheses. The selected prosthesis each can have the same size or different sizes depending on the dimensions of the natural spinal portions of a given recipient.
The Exemplary Surgical Methods
(82) With reference again to
(83) In an exemplary embodiment, after performing a posterior cervical laminectomy executed by standard surgical technique, the spinous process-bilaminar unit(s) of the cervical post-laminectomy spine can be artificially replaced with a single or multiple cervical TASP-LP modules. Based on a width and length (i.e., number of levels) of the laminectomy, the surgeon selects either a single, multiple, or hybrid number of TASP-LP modules according to one or more of embodiments IA, IB, IC, II, III or IV.
(84) The TASP-LP modules can be secured to the natural lamina on both right and left sides, for example, by screwing in trans-laminar screws through the prosthesis' laminar extension perforations and into the natural remaining lamina. This step can immobilize the construct onto the natural cervical spine. The cervical fascia and muscles then can be reattached to the prosthetic spinous process(es) by passing a suture through the spinous process perforations thereby anatomically reconnecting the muscles to the prosthetic spine thereby mimicking the natural spinal anatomy.
(85) In an exemplary embodiment, after performing a posterior thoracic or lumbar laminectomy executed by standard surgical technique, the spinous process-bilaminar unit(s) of the Thoracic/Lumbar postlaminectomy spine can be artificially replaced with a single or multiple Thoracic/Lumbar TASPLP modules. Based on the width and length (i.e., number of levels) of the laminectomy, the surgeon can select either a single, multiple, or hybrid number of TASP-LP modules according to one or more of embodiments IA, IB, IC, II, III or IV.
(86) The Thoracic/Lumbar TASP-LP modules can be secured to the natural lamina on both right and left sides, for example, by screwing in trans-laminar screws through the prosthesis' laminar extension perforations and into the natural remaining lamina. This can immobilize the construct onto the natural thoracic or lumbar spine. The cervical fascia and muscles can then be reattached to the prosthetic spinous process(es) by passing a suture through the spinous process perforations thereby anatomically reconnecting the muscles to the prosthetic spine thereby mimicking the natural spinal anatomy.
(87) The present invention has been described herein in terms of several preferred embodiments. However, modifications and additions to these embodiments will become apparent to those of ordinary skill in the art upon a reading of the foregoing description.
(88) For example, the exemplary embodiments can include a total artificial spinous process (spino)-laminar prosthesis (TASP-LP) comprising one or more of the features of the cervical and Lumbar embodiments illustrated in embodiments IA, IB, IC, II, III, and IV.
(89) The exemplary embodiments can include a method of replacing the spinous process-bilaminar unit(s) of the cervical postlaminectomy spine with a single or multiple cervical TASP-LP modules according to one or more of embodiments IA, IB, IC, II, III, and IV.
(90) The exemplary embodiments can include a single total artificial spinous process (spino)-laminar prosthesis (TASP-LP) having varying lengths and widths.
(91) The exemplary embodiments can include a plurality of total artificial spinous process (spino)-laminar prosthesis (TASP-LP) having varying lengths and widths.
(92) The exemplary embodiments can include a total artificial spinous process (spino)-laminar prosthesis (TASP-LP) comprising expandable hinged spino-laminar wings to accommodate different laminectomy widths. 6. A total artificial spinous process (spino)-laminar prosthesis (TASP-LP) comprising hinged laminar extensions which can accommodate individualized laminar inclines.
(93) The exemplary embodiments can include a total artificial spinous process (spino)-laminar prosthesis (TASP-LP) comprising both hinged expandable spinous process-laminar wings and hinged laminar extensions.
(94) The exemplary embodiments can include a method of replacing the spinous process-bilaminar unit(s) of the Thoracic/Lumbar post-laminectomy spine with a single or multiple Thoracic/Lumbar TASP-LP modules according to one or more of embodiments IA, IB, IC, II, III, and IV.
(95) The exemplary embodiments can include a total artificial spinous process (spino)-laminar prosthesis (TASP-LP) comprising a biocompatible material.
(96) The exemplary embodiments can include a method of manufacturing tailor made individualized prosthetics using 3-D computerized modeling reconstructions of patients' specific geometric anatomy measured on their CT/Mills.
(97) The exemplary embodiments can include a TASP-LP having two or three screws, as exemplarily illustrated, or with fewer or more screws.
(98) The exemplary embodiments can include a mounting area that can be expanded or have its shape changed to any variety of shapes to cover different areas of the bone for attachment or fixation.
(99) The exemplary embodiments can include a prosthesis having areas for addition or incorporation of bone if a surgeon wishes to include a fusion.
(100) The exemplary embodiments can include screws that are countersunk into the prosthetic surface for fixed locking. Variations of locking mechanisms for fixed or variable angled screws can be applied. Either external or internal locking mechanisms can be employed.
(101) The exemplary embodiments can include a prosthesis that is flexible or expandable in any area.
(102) In other exemplary embodiment, pins and staples can be used instead of screws. Such pin or stapler fixtures can be pounded into the device. Other alternative fixture devices or bonding materials can be used to fixate the prosthesis.
(103) In the exemplary embodiments, the muscle suture attachment can be within the spinous process. This perforation can be a single perforation, or in other embodiments, the prosthesis can include a plurality of perforations, or no perforations. The perforations are not limited to the locations illustrated in the exemplary embodiments and can be located anywhere on the prosthesis.
(104) The exemplary embodiments, the prosthesis can be, for example, manufactured in multiple parts which can come in different sizes accommodating intra-patient and multiple patient anatomical variations, and the prosthesis can be assembled intra-operatively by the surgeon using multiple assembly techniques creating tailor made products individualized for the patient.
(105) In another exemplary embodiment, the method can include selecting one or more appropriately sized prostheses from a set or kit of a plurality of prostheses, wherein the set or kit includes prosthesis having different standard sizes. The selected prosthesis each can have the same size or different sizes depending on the dimensions of the natural spinal portions of a given recipient.
(106) The exemplary embodiments can include a current laminar prosthesis that is arch shaped to mimic the natural spinal, anatomy and to protect the intra-spinal neural elements. However other shapes can also be used which include, but at not limited to, circular, polygonal, pyramidal, flat, cornered, rounded, or any combination, variation, or permutation of the above.
(107) It is intended that all such modifications and additions comprise a part of the present invention to the extent that they fall within the scope of the several claims appended hereto.
(108) Like numbers refer to like elements throughout. In the figures, the thickness of certain lines, layers, components, elements or features may be exaggerated for clarity.
(109) The terminology used herein is for the purpose of describing particular embodiments only and is not intended to be limiting of the invention. Unless otherwise defined, all terms (including technical and scientific terms) used herein have the same meaning as commonly understood by one of ordinary skill in the art to which this invention belongs. It will be further understood that terms, such as those defined in commonly used dictionaries, should be interpreted as having a meaning that is consistent with their meaning in the context of the specification and relevant art and should not be interpreted in an idealized or overly formal sense unless expressly so defined herein. Well-known functions or constructions may not be described in detail for brevity and/or clarity.
(110) As used herein, the singular forms a, an and the are intended to include the plural forms as well, unless the context clearly indicates otherwise. It will be further understood that the terms comprises and/or comprising, when used in this specification, specify the presence of stated features, integers, steps, operations, elements, and/or components, but do not preclude the presence or addition of one or more other features, integers, steps, operations, elements, components, and/or groups thereof. As used herein, the term and/or includes any and all combinations of one or more of the associated listed items. As used herein, phrases such as between X and Y and between about X and Y should be interpreted to include X and Y. As used herein, phrases such as between about X and Y mean between about X and about Y. As used herein, phrases such as from about X to Y mean from about X to about Y.
(111) It will be understood that when an element is referred to as being on, attached to, connected to, coupled with, contacting, etc., another element, it can be directly on, attached to, connected to, coupled with or contacting the other element or intervening elements may also be present. In contrast, when an element is referred to as being, for example, directly on, directly attached to, directly connected to, directly coupled with or directly contacting another element, there are no intervening elements present. It will also be appreciated by those of skill in the art that references to a structure or feature that is disposed adjacent another feature may have portions that overlap or underlie the adjacent feature.
(112) Spatially relative terms, such as under, below, lower, over, upper, lateral, left, right and the like, may be used herein for ease of description to describe one element or feature's relationship to another element(s) or feature(s) as illustrated in the figures. It will be understood that the spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation depicted in the figures. For example, if the device in the figures is inverted, elements described as under or beneath other elements or features would then be oriented over the other elements or features. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the descriptors of relative spatial relationships used herein interpreted accordingly.