Interspinous process spacer instrument system with deployment indicator

• US 8,945,183 B2
• Filed: 03/09/2009
• Issued: 02/03/2015
• Est. Priority Date: 10/20/2004
• Status: Active Grant

• Current Assignee: Boston Scientific Neuromodulation Corporation (Boston Scientific Corporation)
• Original Assignee: Vertiflex, Inc. (Boston Scientific Corporation)
• Inventors: Altarac, Moti, Tebbe, Shawn, Kim, Daniel H.
• Primary Examiner(s): Prone, Christopher D
• Application Number:
  US12/400,601
• Publication Number:
  US 20090222043A1
• Time in Patent Office: 2,157 Days
• Field of Search: 623 1711- 1716, 606247-253, 600/309, 600/505
• US Class Current: 606/249
• CPC Class Codes: A61B 17/7062 Devices acting on, attached to, or simulating the effect of, vertebral processes, vertebral facets or ribs rib fixation devices A61B17/8076; Tools for such devices
• CPC Class Codes: A61B 17/7065 Devices with changeable shape, e.g. collapsible or having retractable arms to aid implantation; Tools therefor
• CPC Class Codes: A61B 17/861 specially shaped for gripping driver
• CPC Class Codes: A61B 17/8877 characterised by the cross-section of the driver bit
• CPC Class Codes: A61B 17/8888 at its central region

Abstract

A percutaneous and minimally invasive instrument system for implanting an interspinous process spacer into a patient is disclosed. The insertion instrument system includes an inserter and a driver. The inserter is configured to releasably clamp to an interspinous process spacer for its delivery, implantation and deployment. The driver is configured for removable insertion into a proximal end of a passageway of the inserter. The driver has a distal spacer engaging portion configured to engage that part of the spacer requiring activation for the deployment of the spacer from at least one undeployed configuration to at least one deployed configuration and vice versa. As the spacer goes from the undeployed to the deployed configuration and vice versa, the system advantageously provides a degree of deployment information to the user via at least one deployment indicator.

Claims

1. An instrument system comprising:

a spacer configured to be arranged from at least one undeployed configuration to at least one deployed configuration;

an inserter connectable to the spacer;

a driver configured to arrange the spacer from the at least one undeployed configuration to the at least one deployed configuration; and

a deployment indicator including a spring loaded shaft biased against a movable portion of the spacer at one end;

wherein movement of the movable portion of the spacer moves the shaft;

said movement of said shaft being visible at a second end to provide at least one information pertaining to a degree of deployment of the spacer.

2. The instrument system of claim 1 wherein the driver is insertable into a passageway of the inserter and configured at one end to engage the spacer when the spacer is connected to the inserter.

3. The instrument system of claim 1 wherein at least a portion of the deployment indicator is configured to be resident outside a patient.

4. The instrument system of claim 1 wherein when one end of the inserter is connected to the spacer and said end is inserted into a patient, the instrument is configured such that the deployment indicator is resident outside the patient.

5. The instrument system of claim 1 wherein the deployment indicator is connectable to the spacer.

6. The instrument system of claim 1 wherein the shaft includes an indicator line that is configured to indicate at least one deployed configuration of the spacer.

7. The instrument system of claim 6 wherein the indicator line is configured to be visible through a window;

the system further including at least one alignment line adjacent to said window and configured such that alignment of the indicator line with the alignment line indicates a fully deployed configuration of the spacer.

8. The instrument system of claim 1 wherein the shaft has a first position to indicate a first deployment information and has a second position to indicate a second deployment information.

9. The instrument system of claim 8 wherein the first position is characterized by the shaft projecting at the second end and the second position characterized by the shaft being substantially flush with respect to at least one surface.

10. The instrument system of claim 1 wherein the deployment indicator provides a visual indication of the configuration of the spacer as the spacer moves from the at least one undeployed configuration to the at least one deployed configuration.

11. The instrument system of claim 1 wherein the spacer includes a first wing and a second wing, the first wing is movable between a first undeployed position and a first deployed position, the second wing is movable between a second undeployed position and a second deployed position, and wherein the deployment indicator informs the operator of both a position of the first wing as the first wing moves between the first undeployed position and the first deployed position and a position of the second wing as the second wing moves between the second undeployed position and the second deployed position.

12. The instrument system of claim 1 wherein the spacer includes a first wing and a second wing, the first wing and the second wing are movable between an undeployed position and a spinous process received position, and wherein the deployment indicator provides a visual indication of a position of the first wing and a position of the second wing as the first wing and the second wing move from the undeployed position to the spinous process received position.

13. The instrument system of claim 1 wherein

the spacer includes a body portion, a first wing configured to receive a first spinous process, and a second wing configured to receive a second spinous process;

and

the deployment indicator is configured to inform the operator of an amount of rotation of at least one of the first and second wings when the driver causes the first wing to rotate relative to the body portion to receive the first spinous process and causes the second wing to rotate relative to the body portion to receive the second spinous process.

14. An instrument system comprising:

a spacer having engaging portions movable between an undeployed position and a deployed position;

an inserter releasably coupled to the spacer, the inserter having a central bore extending therethrough;

a driver having a first end portion opposite a second end portion, wherein the first end portion is movably positioned within at least a section of the central bore of the inserter and includes projections that contact corresponding engaging portions of the spacer to move the engaging portions from the undeployed position to the deployed position in response to movement of the second end portion; and

a deployment indicator including a spring loaded shaft biased against a movable portion of the spacer at one end, wherein movement of the movable portion of the spacer moves the shaft, wherein movement of the shaft is visible at a second end to provide at least one information pertaining to the degree of deployment of the spacer.

15. The instrument system of claim 14 wherein deployment indicator is a first deployment indicator, and wherein the instrument system further includes a second deployment indicator that provides a second visual indication of the positions of the engaging portions of the spacer, the central bore of the inserter is a first central bore, and wherein the driver includes a second central bore extending therethrough, and wherein the spring loaded shaft extends through at least a portion of the second central bore.

16. The instrument system of claim 14 wherein the shaft is biased towards the spacer and includes a first end portion opposite a second end portion, wherein the first end portion of the shaft contacts the spacer and a position of the second end portion of the shaft relative to the second end portion of the driver provides the visual indication of the positions of the engaging portions of the spacer.

17. The instrument system of claim 14, further comprising:

an indicator window;

an alignment line adjacent to the window; and

an indicator line movable with the driver, wherein when the indicator line is at least generally aligned with the alignment line the engaging portions of the spacer are in the deployed position.

18. The instrument system of claim 14 wherein the spacer includes a first wing and a second wing, the first wing is movable between a first undeployed position and a first deployed position, the second wing is movable between a second undeployed position and a second deployed position, and wherein the deployment indicator visually informs an operator of both a position of the first wing moving between the first undeployed position and the first deployed position and a position of the second wing moving between the second undeployed position and the second deployed position.

19. The instrument system of claim 14 wherein the spacer includes a first wing configured to receive a first spinous process and a second wing configured to receive a second spinous process, and wherein the deployment indicator is configured to inform the operator of both a position of the first wing when the driver mechanically moves the first wing between a first undeployed position and a first deployed position and a position of the second wing when the driver mechanically moves the second wing between a second undeployed position and a second deployed position.

20. The instrument system of claim 14 wherein the deployment indicator informs the operator of the position of at least one wing of the spacer independent of physical contact between the at least one wing and the subject'"'"'s body.