| Literature DB >> 32631369 |
Yingkai Zhang1, Cheng Li1, Lei Li2, Yanyan Sun3, Zeqing Li1, Yunli Mei1, Xinyuan Feng1.
Abstract
PURPOSE: To design a new type of screw for minimally invasive atlantoaxial anterior transarticular screw (AATS) fixation with a diameter that is significantly thicker than that of traditional screws, threaded structures at both ends, and a porous metal structure in the middle. The use of a porous metal structure can effectively promote bone fusion and compensate for the disadvantages of traditional AATSs in terms of insufficient fixation strength and difficulty of bone fusion. The biomechanical stability of this screw was verified through finite element analysis. This instrument may provide a new surgical option for the treatment of atlantoaxial disorders.Entities:
Keywords: Atlantoaxial instability; Atlantoaxial screw fixation; Atlas; Axis; Biomechanics; Finite element analysis; Transarticular screw fixation
Mesh:
Year: 2020 PMID: 32631369 PMCID: PMC7339419 DOI: 10.1186/s13018-020-01764-w
Source DB: PubMed Journal: J Orthop Surg Res ISSN: 1749-799X Impact factor: 2.359
Fig. 1Point (a) in the figure shows the screw entry region, which is 4 mm above the junction between the inferior edge of the lateral arch of the axis and the lateral edge of the vertebral body of the axis. Point (b) shows the implantation direction of the device and (b) is the midpoint of the posterior edge of the superior articular process of the atlas. Point (c) indicates the screw path, and point (d) is the 5 mm safety buffer zone
Fig. 2The cylinder was gradually thickened in the 3D reconstruction until it broke through the outer or inner wall of the superior articular process of the atlas (a, b), and this diameter of the cylinder was recorded. The implantation of the cylinder was simulated during the 3D reconstruction. The red portion is the length of the cylinder in the lateral mass of the axis, the yellow portion is the length of the cylinder in the atlantoaxial joint space, and the green portion is the length of the cylinder in the lateral mass of the atlas (c, d)
Material properties used for various components in the finite element model [14–17]
| Components | Poisson’s ratio | Young’s modulus (MPa) | cross-sectional area(mm2) | Reference |
|---|---|---|---|---|
| Cortical bone | 0.2 | 15000 | – | [ |
| Cancellous bone | 0.2 | 500 | – | [ |
| Anterior longitudinal ligament | 0.3 | 30 | 6 | [ |
| Posterior longitudinal ligament | 0.3 | 20 | 5 | [ |
| Inter spinous ligament | 0.3 | 10 | 5 | [ |
| Ligamentum flavum | 0.3 | 10 | 5 | [ |
| Alar ligament | 0.3 | 5 | 22 | [ |
| Transverse ligament | 0.2 | 20 | – | [ |
| Nuchal ligament | 0.2 | 20 | 10 | [ |
| Supraspinous ligament | 0.3 | 10 | 10 | [ |
| Capsular ligament | 0.3 | 10 | 46 | [ |
| Screw and rod | 0.3 | 110000 | – | [ |
Fig. 3Stable atlantoaxial complex
Fig. 4Development of an atlantoaxial fusion method model. a Traditional atlantoaxial anterior transarticular screw fixation. b Atlantoaxial posterior pedicle screw fixation. c New AATS
Measured atlantoaxial data (unit: mm)
| Left | Right | Left(FEA data) | Right(FEA data) | |
|---|---|---|---|---|
| Length A | 8.5 ± 0.7 | 8.6 ± 0.6 | 8.6 | 8.6 |
| Length B | 4.1 ± 0.3 | 4.2 ± 0.4 | 4.2 | 4.2 |
| Length C | 12.5 ± 0.6 | 12.6 ± 0.5 | 12.6 | 12.6 |
| Diameter | 8.1 ± 0.4 | 8.2 ± 0.4 | 8.2 | 8.2 |
Fig. 5A New AATS Model. a Threaded structures at both ends. b Porous metal structure in the middle. c Internal annular solid cylinder with an outer diameter of 3 mm and an inner diameter of 1 mm (for guide wire positioning). B New AATS. C New AATS in atlantoaxial model
New ATS design data used in finite element analysis
| Value (mm) | |
|---|---|
| Head | 10 |
| Middle | 8 |
| Tail | 8 |
| Diameter | 6 |
Comparison of the range of motion between the current finite element model and those of experimental studies (degree)
| Segment | Panjabi et al. [ | Model 1 | |
|---|---|---|---|
| Flexion | C0-C1 | 14.4 ± 3.2 | 15.21 |
| C1-C2 | 12.7 ± 3.2 | 13.12 | |
| Extension | C0-C1 | 14.4 ± 3.2 | 15.54 |
| C1-C2 | 10.5 ± 5.0 | 12.36 | |
| Lateral bending | C0-C1 | 5.6 ± 3.0 | 7.65 |
| C1-C2 | 12.6 ± 7.0 | 15.25 | |
| Axial rotation | C0-C1 | 3.3 ± 2.3 | 4.45 |
| C1-C2 | 37.4 ± 9.0 | 41.95 |
Fig. 6Graphical representation of the atlantoaxial fixation stiffness during flexion, extension, lateral bending, and axial rotation
Fig. 7Von Mises stress on pedicle screw