The device and method relates to instrumentation for the mammalian spine and is particularly directed to a device for correction of degenerative, congenital, or traumatic deformity, and a method of placement of the device.
There is a need for a cage system capable of effecting rigid intervertebral fusion placed in a minimally invasive manner through a posterior-lateral approach without requiring laminectomy to effect placement.
There is a need for a cage system that may be placed in a minimally invasive manner that is capable of effecting dynamic stabilization to intervertebral segments.
There is a need for a cage fusion or dynamic stabilization device that may be placed into an intervertebral osteotomy through a posterior-lateral approach without utilization of a rigid tube access device.
There is a need for a cage fusion type device that may be utilized in the cervical region through an anterior-lateral approach with a minimally invasive technique for placement that does not require the use of rigid tube placement instrumentation.
There is a need for a cage fusion or dynamic stabilization device that may be placed at all spinal levels utilizing a minimally invasive technique for placement having small access requirements and instrumentation that is flexible in nature allowing for adaptation to anatomic and placement route variation.
There is a need for a cage type fusion/stabilization device that can be placed between vertebral bodies with minimal disruption of endogenous structures, thus maximizing retention of endogenous structure and stability, with little or no disruption of the annular ligament.
There is a need for a minimally invasive cage type device that may be placed utilizing a true lateral access technique with the cage device placed transversely across the vertebral bodies and without material disruption of muscular structures and without associated morbidity at the time of surgery.
There is a need for a device that can effect dynamic stabilization between vertebral segments.
There is a need for devices effecting dynamic stabilization between vertebral segments having adaptive structural capabilities that permit dynamic movement of a load axis mimicking the structural capabilities of a native intervertebral disc.
There is a need for a dynamic stabilization device that has a capability of avoiding failure through design of redundant load carrying members.
A thermally active member comprises a shape memory material. The method of placement of the thermally active member facilitates transition of shape memory material between a simple undefined geometry, such as a substantially linear shape, to a complex predetermined shape memory form, such as a coiled shape. The preferred complex geometry may be described as an intervertebral cage or cage fusion device. The device may be placed into a space surgically created between two vertebrae through an access channel that is less than one third of its final deployed cross sectional dimension.
The device of the preferred embodiments may be classified as a “cage fusion” type device. The device may comprise one or more structural components comprised of a shape memory material.
In pre-deployment form, the device components exist as simple elements that are malleable and capable of adopting an essentially linear form 12.
The transitioned final form
The device is constructed to maintain a super-elastic form at body temperature, and may assume this shape at slightly below body temperature. This final deployed form of the device has a shape and size that may be a cage type structure, with the cage providing a framework for support. The structural properties of the device, when maintained at temperatures at or above the transition temperature, which is preferred to be at, or slightly below, body temperature is able to correct or assist in correcting anatomic deformity between vertebral segments. The device can effect a rigid fusion between adjacent vertebral bodies, and is preferred to have a high degree of rigidity.
A further embodiment of the device provides structural scaling of material and cross-sections, and allows for design of a device with a predictable degree of compressibility, and creation of a dynamic stabilization construct. This embodiment may function as a prosthetic disc accommodating a controlled degree of motion between vertebral bodies. The geometry of this embodiment is capable of motion in six planes, and can emulate mechanical characteristics of native disc structures.
Parallel coiled or helical designs may be utilized. Two or more equivalent coils or helices possess the geometric property of deployment generally parallel to the central axis of a deployment means, such as a deployment lumen or catheter. The multiple parallel helices may be joined at proximal and/or distal ends, structurally maintaining register between the helices through the deployment process. A single helix structure may deploy tangentially across the central axis of the deployment catheter, and not yield a symmetric deployment process. A three parallel helix embodiment 34 allows for a fully structurally symmetric process of deployment, wherein the forces of transition between the three elements are radially balanced, yielding a geometric relationship that tends towards deployment parallel 32 to the catheters central axis.
A thermal element comprises a thermally active shape memory material having super-elastic properties at body temperature. The design transition temperature may be specified below body temperature, such as 2 to 3 degrees Celsius below body temperature of the vertebrate into which the device is placed. Currently available materials meeting desirable specifications are various alloys of nitinol or nitinol like alloys. Alloy composition may be adjusted, creating shape memory materials having super-elastic and shape set characteristics (austenite state) near body temperature, while retaining those shape characteristics at body temperature and higher temperatures. These alloys exist at lower temperatures in martensite state wherein the material is relatively malleable and has no shape set or super-elastic properties, the shape may be expressed as “indeterminate” at these temperatures. When the shape of the device is indeterminate, if a dynamic force is placed upon the device and the dynamic force changes the shape, the shape into which the device is changed is retained when the dynamic force is removed. This martensite state corresponds to the pre-deployment malleable form, or indeterminate form, of the device. In this state, the device may be linear, like a wire, and may be bent 42 or shaped like a wire. In a preferred embodiment, the wire may be shaped manually by a physician installing the device.
When heat is applied to the device, the device assumes its predetermined super-elastic austenite “shape memory” form with high strength structural capabilities 44. The device will retain this shape as long as the temperature is maintained above the predetermined temperature, which is preferred to be just below body temperature of the human or other vertebrate into which the device is to be positioned. When a dynamic force is not being actively applied to the device at this higher temperature, the device assumes and retains a predetermined shape, which may be summarily referred to as a determinate shape. The device is shown in various embodiments of determinate shape in the drawing Figures.
In one embodiment, the device is a wire 40 having a substantially round cross section. The determinate form of the device is shape set to a coiled or helical form.
The device may be repositioned during the placement process by terminating heat introduction, and pulling the device in the opposite direction and into the catheter, where the temperature environment is less than Mf. Stated otherwise, the transition process is reversed.
The final shape set form of the device is designed to substantially match the geometry of the osteotomy 52 formed for its placement in a vertebral body 54 (or usually, two vertebral bodies.
Geometric configurations of the device are not limited to simple cylindrical shapes. A specified final design shape may be reduced to a single or multiple linear components, and the device is amenable to placement utilizing the technique described herein. At a low temperature state the device has no intrinsic shape beyond its cross section and no super-elastic properties. The device at the low temperature state may be characterized as shape indeterminate or indefinite. In this temperature state, the shape of the device is indeterminate and may be formed into a linear shape having a cross section that is considerably smaller than the cross section of the deployed device.
This process permits low temperature martensite states to be utilized having non-complex geometry, and simple linear or substantially linear shapes, like a wire. The cross-section shape of these elements may be of any imaginable design, and especially those which may be extruded. The structural cross-section may likewise be varied along the length of a component to meet varied structural requirements for different portions of the component in its final “shape memory” or determinate form. Cross section variation allows not only for the device to meet structural requirements in its final deployed “shape memory” or determinate form, but permits design of the individual helical elements in interdigitating configurations 72, preferably yielding a small cross section of the device in its low temperature pre-deployment or indeterminate form.
The design of the device may be specifically tailored to meet structural requirements for dynamic stabilization. Portions of the device may be so designed to allow compression between vertebral bodies and a limited degree of rotation between vertebral bodies; an essentially cylindrical geometry device with bent side wall segments 82 is shown which accommodate limited motion between vertebral segments.
Further, the device may be so designed that specified portions of the structure are attenuated to allow a controlled degree of deformation to occur.
The surfaces of the fully deployed device may be machined to produce a textured surface 112 that may increase the probability of boney fusion occurring.
The device may be of composite construction, utilizing polymer coating or applied sections that will enhance bone growth affecting a greater probability of fusion. Coatings may be selected that allow incorporation of bone growth stimulus factors. An additional property of composite construction may be the capability preventing the formation of wear debris or providing for the sequestration of wear debris from the immune system of the patient. This may be achieved by entirely coating each shape memory component 122 with a material is impermeable to the immune system.
This application is a continuation in part of application Ser. No. 11/196,891 filed Aug. 4, 2005. Applicant claims the benefit of provisional application Ser. No. 60/980,667 filed Oct. 17, 2007.
Number | Date | Country | |
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60980667 | Oct 2007 | US |
Number | Date | Country | |
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Parent | 11196891 | Aug 2005 | US |
Child | 12288272 | US |