Spinal repair

• US 20060265077A1
• Filed: 12/09/2005
• Published: 11/23/2006
• Est. Priority Date: 02/23/2005
• Status: Abandoned Application

• Current Assignee: Spinal Ventures, LLC
• Original Assignee: Spinal Ventures, LLC
• Inventors: Zwirkoski, Paul A.
• Application Number:
  US11/298,138
• Publication Number:
  US 20060265077A1
• Time in Patent Office: Days
• US Class Current: 623/17.160
• CPC Class Codes: A61B 17/7094 Solid vertebral fillers; devices for inserting such fillers
• CPC Class Codes: A61F 2/442 Intervertebral or spinal discs, e.g. resilient non-disc-shaped intervertebral inflatable pockets A61F2/441; non-disc-shaped intervertebral fusion implants A61F2/4455
• CPC Class Codes: A61F 2/4425 made of articulated components
• CPC Class Codes: A61F 2/4611 of spinal prostheses
• CPC Class Codes: A61F 2002/2835 Bone graft implants for filling a bony defect or an endoprosthesis cavity, e.g. by synthetic material or biological material
• CPC Class Codes: A61F 2002/302 toroidal, e.g. rings
• CPC Class Codes: A61F 2002/30331 made by longitudinally pushing a protrusion into a complementarily-shaped recess, e.g. held by friction fit
• CPC Class Codes: A61F 2002/30383 made by laterally inserting a protrusion, e.g. a rib into a complementarily-shaped groove
• CPC Class Codes: A61F 2002/30462 retained or tied with a rope, string, thread, wire or cable
• CPC Class Codes: A61F 2002/30495 using a locking ring
• CPC Class Codes: A61F 2002/30604 modular
• CPC Class Codes: A61F 2002/30662 with rotation-limiting means
• CPC Class Codes: A61F 2002/30663 multiaxial, e.g. biaxial; multipolar, e.g. bipolar or having an intermediate shell articulating between the ball and the socket
• CPC Class Codes: A61F 2002/4415 elements of the prosthesis being arranged in a chain like manner
• CPC Class Codes: A61F 2002/443 having two transversal endplates and at least one intermediate component
• CPC Class Codes: A61F 2002/444 for replacing the nucleus pulposus
• CPC Class Codes: A61F 2220/0025 Connections or couplings between prosthetic parts, e.g. between modular parts; Connecting elements
• CPC Class Codes: A61F 2220/0033 made by longitudinally pushing a protrusion into a complementary-shaped recess, e.g. held by friction fit
• CPC Class Codes: A61F 2220/0075 sutured, ligatured or stitched, retained or tied with a rope, string, thread, wire or cable
• CPC Class Codes: A61F 2230/0065 toroidal, e.g. ring-shaped, doughnut-shaped

Abstract

A spinal implant for repairing a region of a subject'"'"'s spine may have a plurality of interlockable segments that can be deployed from a delivery configuration (e.g., a linear array) into a deployed configuration. When the implant is in the delivery configuration, the implant comprises a linear array of the segments that are flexibly connected, and when the implant is in the deployed configuration, the segments are interlocked into a stable structure so that each segment is adjacent to and interlocked with at least two other segments. in the deployed configuration, the implants may have a greater strength (e.g., crush strength) and may help maintain the stability of the body region. The implant may be inserted into the spinal region by an applicator from the posterior region of the subject in the delivery configuration and assembled within the body to form the deployed configuration.

Claims

1. An implant for insertion into the spinal region of a subject, comprising:

a plurality of interlockable segments, deployable from a delivery configuration into a deployed configuration;

wherein, when the implant is in the delivery configuration, the implant comprises a linear array of the segments that are flexibly connected, and when the implant is in the deployed configuration, the segments are interlocked into a stable structure so that each segment is adjacent to and interlocked with at least two other segments.

2. The implant of claim 1, further comprising a filament connecting the segments.

3. The implant of claim 2, wherein at least some of the segments are slideably coupled to the filament.

4. The implant of claim 1, wherein the segments interlock by mating with adjacent segments in the deployed configuration.

5. The implant of claim 1, further comprising a holdfast to secure the implant in the deployed configuration.

6. The implant of claim 1, wherein the deployed configuration is configured as a ring.

7. The implant of claim 1, wherein the deployed configuration is configured as a disc.

8. A method of inserting an interlockable implant comprising:

positioning an applicator adjacent to a target tissue site;

delivering an implant to the target tissue site, wherein the implant comprises a linear array of flexibly connected interlockable segments; and

securing the implant into a deployed configuration wherein the interlockable segments are interlocked so that each segment is adjacent to and interlocked with two other segments.

9. The method of claim 8, further comprising deploying the implant from a delivery configuration in which the implant comprises a linear array of flexibly connected segments to a deployed configuration in which the segments are interlocked into a stable structure so that the interlocked segments do not move with respect to adjacent segments.

10. The method of claim 9, wherein the step of deploying comprises tensioning the connection between the segments.

11. An interbody fusion device for insertion into the spinal region of a subject, comprising:

a plurality of interlockable segments, deployable from a delivery configuration into a deployed configuration;

wherein, when the implant is in the delivery configuration, the implant comprises a linear array of the segments that are flexibly connected, and when the implant is in the deployed configuration, the segments are interlocked into a ring wherein each segment is adjacent to and interlocked with at least two other segments.

12. The interbody fusion device of claim 11, wherein at least some of the segments comprise voids configured to allow ingrowth.

13. The interbody fusion device of claim 11, wherein the segments are slideably coupled to a filament passing though one or more passages within each segment.

14. The interbody fusion device of claim 11 further comprising an orientation guide configured to maintain the orientation of the segments with respect to each other in the delivery configuration.

15. The interbody fusion device of claim 11, wherein each segment comprises two faces offset by between about 30 and about 60 degrees, and wherein each face is configured to interlock with an adjacent face of a another segment.

16. A method of inserting an interbody fusion device comprising:

positioning an applicator adjacent to a target tissue site;

delivering an interbody fusion device to the target tissue site, wherein the device comprises a linear array of flexibly connected interlockable segments; and

securing the device into a deployed configuration wherein the interlockable segments are interlocked so that each segment is adjacent to and interlocked with two other segments to form a ring.

17. An nuclear replacement device for insertion into a subject'"'"'s spine, comprising:

a plurality of pie-shaped interlockable segments, deployable from a delivery configuration into a deployed configuration;

wherein, when the implant is in the delivery configuration, the implant comprises a linear array of the segments that are flexibly connected, and when the implant is in the deployed configuration, the segments are interlocked into a disc wherein each segment is adjacent to and interlocked with at least two other segments.

18. The nuclear replacement device of claim 17, wherein at least a region of the segments comprises an elastic material.

19. The nuclear replacement device of claim 17, wherein the segments are slideably coupled to a filament passing though one or more passages within each segment.

20. The nuclear replacement device of claim 17, further comprising an orientation guide configured to maintain the orientation of the segments with respect to each other in the delivery configuration.

21. The nuclear replacement device of claim 17, wherein each segment comprises two faces offset by between about 30 and about 60 degrees, and wherein each face is configured to interlock with an adjacent face of a another segment.

22. A method of inserting a nuclear replacement device comprising:

positioning an applicator adjacent to a target tissue site;

delivering a nuclear replacement device to the target tissue site, wherein the device comprises a linear array of flexibly connected interlockable segments; and

securing the device into a deployed configuration wherein the interlockable segments are interlocked so that each segment is adjacent to and interlocked with two other segments to form a disc.

23. A total disc replacement device for insertion into a subject'"'"'s spine, comprising:

a plurality of interconnecting segments, deployable from a delivery configuration into a deployed configuration;

wherein the segments comprise;

a central endplate; and

a plurality of wing segments;

further wherein, when the device is in the delivery configuration, the device comprises a central endplate and a linear array of the wing segments that are flexibly connected, and when the device is in the deployed configuration, the segments are interlocked around the central endplate into an articulating endplate.

24. The total disc replacement device of claim 23, further comprising a central inner bead configured to abut at least the central endplate region of the articulating endplate.

25. The total disc replacement device of claim 23, further comprising a second plurality of interconnecting segments, deployable from a delivery configuration into a deployed configuration;

wherein the second plurality of segments of comprise;

a second central endplate; and

a second plurality of wing segments;

further wherein, when the device is in the delivery configuration, the device comprises a second central endplate and a linear array of the second wing segments that are flexibly connected, and when the device is in the deployed configuration, the second plurality of segments are interlocked around the second central endplate into a second articulating endplate.

26. The total disc replacement device of claim 25, wherein the central inner bead is further configured to abut a second articulating endplate.

27. The total disc replacement device of claim 25, wherein the central endplate comprises a disc having a channel for mating with the wing segments.

28. The total disc replacement device of claim 25, wherein at least a region of the central endplate comprises a smooth surface for mating with a central inner bead.

29. The total disc replacement device of claim 25, wherein the annular endplate comprises a concave surface for coupling with the central inner bead.

30. The total disc replacement device of claim 25, wherein the segments are slideably coupled to a filament passing though one or more passages within each segment.

31. The total disc replacement device of claim 25, further comprising an orientation guide configured to maintain the orientation of the segments with respect to each other in the delivery configuration.

32. The total disc replacement device of claim 25, wherein the orientation guide comprise a filament connecting the segments.

33. A method of inserting a total disc replacement device comprising:

positioning an applicator adjacent to a target tissue site;

delivering an articulating endplate to the target tissue site, wherein the articulating endplate comprises a linear array of flexibly connected interlockable segments comprising a plurality of wing segments for mating with a central endplate; and

securing the articulating endplate into a deployed configuration wherein the wing segments and the central endplate are interlocked.

34. The method of claim 33, further comprising delivering a central inner bead to the target tissue site.

35. The method of claim 34, further comprising delivery a second articulating endplate to the target tissue site, wherein the second articulating endplate comprises a linear array of flexibly connected interlockable segments comprising a plurality of wing segments for mating with a central endplate.