Interspinous spacer
An implantable spacer for placement between adjacent spinous processes is provided. The spacer includes a body and a wing rotatably connected to the body. The wing includes two U-shaped configurations that together define a substantially H-shaped configuration for retaining the spacer between adjacent spinous processes. An actuator assembly is connected to the body and to the wing with the proximal end of the spacer being connectable to a removable driver that is configured to engage the actuator assembly. While connected to the spacer, the driver is rotatable in one direction to deploy the wing from an undeployed to a deployed configuration and in an opposite direction to undeploy the wing. In the deployed configuration, the spacer acts as a space holder opening up the area of the spinal canal, maintaining foraminal height, reducing stress on the facet joints and relieving pain for the patient.
1. A method for treating a subject, comprising:
cutting a supraspinous ligament of the subject to provide access to an interspinous space between a superior spinous process and an inferior spinous process;
moving an interspinous implant toward the interspinous space such that the interspinous implant passes directly between a superior section of the supraspinous ligament and an inferior section of the supraspinous ligament;
positioning a central portion of the interspinous implant at the interspinous space, the interspinous implant is in a delivery configuration for keeping first and second members of the interspinous implant spaced apart from the superior and inferior spinous processes; and
while the central portion of the interspinous implant is positioned at the interspinous space, moving the interspinous implant from the delivery configuration to a locked deployed configuration by rotating the first and second members about a single transverse axis perpendicular to a longitudinal axis of the central portion for holding the superior and inferior spinous processes between the first and second members.
2. The method of claim 1 , wherein when the interspinous implant is in the locked deployed configuration, a superior portion of the first member is positioned alongside a first side of the superior spinous process and an inferior portion of the first member is positioned alongside a first side of the inferior spinous process and a superior portion of the second member is positioned alongside a second side of the superior spinous process and an inferior portion of the second member is positioned alongside a second side of the inferior spinous process.
3. The method of claim 1 , wherein after positioning the central portion at the interspinous space, driving an actuator of the central portion using a delivery instrument connected to the interspinous implant to cause the rotation of the first and second members.
4. The method of claim 1 , further comprising mechanically moving self-locking components of the interspinous implant to move the interspinous spacer toward the locked deployed configuration.
5. The method of claim 1 , wherein moving the interspinous implant from the delivery configuration to the locked deployed configuration comprises simultaneously rotating the first and second members to the locked deployed configuration.
6. The method of claim 1 , wherein moving the interspinous implant from the delivery configuration to the locked deployed configuration comprises rotating each of the first and second members by about 90 degrees.
7. The method of claim 1 , wherein, in the delivery configuration, the first and second members are parallel to each other.
8. The method of claim 1 , wherein, in the delivery configuration, the first and second members are parallel to the longitudinal axis of the central portion.
9. A method for treating a subject, comprising:
moving an interspinous spacer between portions of a supraspinous ligament of the subject;
delivering the interspinous spacer to an interspinous space in the subject; and
moving a wing assembly of the interspinous spacer relative to the interspinous space while at least a portion of the interspinous spacer is located at the interspinous space such that
first and second superior extensions of the wing assembly rotate toward a superior spinous process about a single transverse axis perpendicular to a longitudinal axis of a central portion of the interspinous spacer,
first and second inferior extensions of the wing assembly rotate toward an inferior spinous process about the single transverse axis perpendicular to the longitudinal axis of the central portion of the interspinous spacer, and
the interspinous spacer automatically locks the wing assembly in a deployed configuration, wherein the superior spinous process is held between the first and second superior extensions and the inferior spinous process is held between the first and second inferior extensions.
10. The method of claim 9 , wherein after the interspinous spacer is locked, the first superior extension is positioned alongside a first side of the superior spinous process and the first inferior extension is positioned alongside a first side of the inferior spinous process and the second superior extension is positioned alongside a second side of the superior spinous process and the second inferior extension is positioned alongside a second side of the inferior spinous process.
11. The method of claim 9 , further comprising mechanically driving an actuator of the interspinous spacer using a delivery instrument connected to the interspinous spacer to cause the rotation of the wing assembly.
12. The method of claim 9 , further comprising mechanically moving self-locking components of the interspinous spacer to cause automatic locking.
13. The method of claim 9 , further comprising mechanically operating an actuator mechanism of the interspinous spacer to cause rotation of the wing assembly while a main body of the interspinous spacer is positioned at the interspinous space, wherein the main body contains the actuator mechanism and is rotatably coupled to the wing assembly.
14. The method of claim 9 , wherein delivering the interspinous spacer comprises delivering the interspinous spacer with the wing assembly parallel to the longitudinal axis of the central portion of the interspinous spacer.
15. A method for treating a subject, comprising:
forming an access path between portions of a supraspinous ligament of the subject;
moving an interspinous spacer in a delivery configuration to an interspinous space via the access path, the interspinous spacer including a main body, a locking assembly, a first elongate member, and a second elongate member; and
moving the interspinous spacer by rotation of the first and second elongate members about a single transverse axis perpendicular to a longitudinal axis of the main body to a deployed configuration such that a superior spinous process is located directly between the first and second elongate members and an inferior spinous process is located directly between the first and second elongate members, wherein the locking assembly locks the interspinous spacer in the deployed configuration.
16. The method of claim 15 , wherein the locking assembly is driven by an instrument detachably coupled to the main body of the interspinous spacer.
17. The method of claim 15 , wherein moving the interspinous spacer by rotation of the first and second elongate members comprises simultaneously rotating the first and second elongate members to the deployed configuration.
18. The method of claim 15 , wherein moving the interspinous spacer by rotation of the first and second elongate members comprises rotating each of the first and second members by about 90 degrees.
19. The method of claim 15 , wherein, in the delivery configuration, the first and second elongate members are parallel to each other.
20. The method of claim 15 , wherein, in the delivery configuration, the first and second elongate members are parallel to the longitudinal axis of the main body.