Total artificial spino-laminar prosthetic replacement

• US 10,022,238 B1
• Filed: 02/26/2018
• Issued: 07/17/2018
• Est. Priority Date: 11/25/2009
• Status: Active Grant

• Current Assignee: Moskowitz Family LLC
• Original Assignee: Moskowitz Family LLC
• Inventors: Moskowitz, Nathan C., Moskowitz, Mosheh T., Sugalski, Eric, Moskowitz, Ahmnon D.
• Primary Examiner(s): Robert, Eduardo C
• Assistant Examiner(s): ECKMAN, MICHELLE CHRISTINE
• Application Number:
  US15/904,617
• Publication Number:
  US 20180185161A1
• Time in Patent Office: 141 Days
• CPC Class Codes: A61B 17/7071 Implants for expanding or repairing the vertebral arch or wedged between laminae or pedicles; Tools therefor
• CPC Class Codes: A61F 2/4405 for apophyseal or facet joints, i.e. between adjacent spinous or transverse processes devices implanted between spinous or transverse processes A61B17/7062
• CPC Class Codes: A61F 2002/30471 connected by a hinged linkage mechanism, e.g. of the single-bar or multi-bar linkage type
• CPC Class Codes: A61F 2002/30563 having elastic means or damping means, different from springs, e.g. including an elastomeric core or shock absorbers
• CPC Class Codes: A61F 2002/30578 having apertures, e.g. for receiving fixation screws
• CPC Class Codes: A61F 2002/30604 modular
• CPC Class Codes: A61F 2002/30616 Sets comprising a plurality of prosthetic parts of different sizes or orientations
• CPC Class Codes: A61F 2002/30624 Hinged joint, e.g. with transverse axle restricting the movement
• CPC Class Codes: A61F 2002/30649 Ball-and-socket joints
• CPC Class Codes: A61F 2002/30948 using computerized tomography, i.e. CT scans
• CPC Class Codes: A61F 2002/30952 using CAD-CAM techniques or NC-techniques
• CPC Class Codes: A61F 2002/449 comprising multiple spinal implants located in different intervertebral spaces or in different vertebrae
• CPC Class Codes: A61F 2310/00023 Titanium or titanium-based alloys, e.g. Ti-Ni alloys

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).