| Literature DB >> 33942538 |
Jia-Ming Zhou1,2, Xing Guo1,2, Liang Kang1,2, Rui Zhao1,2, Xiao-Tian Yang1,2, Yi-Bin Fu3, Yuan Xue1,2.
Abstract
OBJECTIVE: To investigate the biomechanical effect of different intervertebral reconstructive heights on adjacent segments following C5 /C6 anterior cervical discectomy and fusion (ACDF) through finite element analysis.Entities:
Keywords: Adjacent segment disease; Anterior cervical discectomy and fusion; Finite element analysis; Intervertebral reconstructive height
Year: 2021 PMID: 33942538 PMCID: PMC8274176 DOI: 10.1111/os.13010
Source DB: PubMed Journal: Orthop Surg ISSN: 1757-7853 Impact factor: 2.071
Fig. 1Finite element models of preoperative and postoperative C4–C7 cervical spine and other structures and details. (A) Frontal view of preoperative model; (B) Lateral view of preoperative model; (C) Intervertebral disc details; (D) Vertebral body details; (E) Lateral view of the cage; (F) Titanium plate and screws; (G) Frontal view of postoperative model; (H) Lateral view of postoperative model; (I) Loading and boundary condition.
The material properties of the spinal soft tissues and hard tissues used in the finite element model
| Description | Element type | Young's modulus (MPa) | Poisson's ratio |
|---|---|---|---|
| Cortical bone | C3D4 | 12,000 | 0.3 |
| Cancellous bone | C3D4 | 100 | 0.2 |
| Posterior elements | C3D4 | 3500 | 0.25 |
| Facet cartilage | C3D4 | 10.4 | 0.4 |
| End plate | C3D4 | 600 | 0.3 |
| Nucleus pulposus | C3D4 | 1 | 0.49 |
| Annulus ground substance | C3D4 | 3.4 | 0.4 |
| Annulus fibers | T3D2 | 450 | 0.45 |
| Titanium plate | C3D4 | 120,000 | 0.3 |
| Titanium screw | C3D4 | 120,000 | 0.3 |
The material properties of the ligaments
| ALL | PLL | LF | ISL | CL | |||||
|---|---|---|---|---|---|---|---|---|---|
| Displacement (mm) | Force (N) | Displacement (mm) | Force (N) | Displacement (mm) | Force (N) | Displacement (mm) | Force (N) | Displacement (mm) | Force (N) |
| 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 | 0 |
| 1 | 35.5 | 0.9 | 1.33 | 1.7 | 2.2 | 1.2 | 0.75 | 1.7 | 2.452 |
| 2 | 64.9 | 2 | 29.0 | 3.74 | 45.9 | 2.7 | 16.9 | 3.9 | 53.6 |
| 4 | 89.7 | 3 | 51.4 | 5.61 | 82.9 | 4.0 | 24.4 | 5.8 | 87.9 |
| 5 | 108.6 | 4 | 71.38 | 7.48 | 119.6 | 5.4 | 29.5 | 7.7 | 109.4 |
| 6 | 119.6 | 5 | 85.8 | 9.35 | 133.7 | 6.7 | 32.9 | 9.7 | 125.8 |
| 6 | 94.7 | 11.3 | 147.2 | 8.1 | 34.9 | 11.5 | 134.8 | ||
ALL, anterior longitudinal ligament; CL, capsular ligament; ISL, interspinous ligament; LF, ligamentum flavum; PLL, posterior longitudinal ligament.
Element and node numbers for three different mesh resolutions
| Element number | Node number | |
|---|---|---|
| Mesh 1 | 63218 | 148526 |
| Mesh 2 | 139672 | 299408 |
| Mesh 3 | 232536 | 452768 |
Fig. 2The predicted percentage differences of von Mises stress between Mesh 1 and Mesh 2 and between Mesh 2 and Mesh 3 in different structures in the axial rotation.
Fig. 3The predicted ranges of motion (ROM) of the preoperative model are validated by previous published study.
Fig. 4The intradiscal pressures distribution diagram of adjacent intervertebral discs. (A) C4/C5; (B) C6/C7.
Fig. 5The intradiscal pressure (IDP) of C4/C5 levels under different loading conditions.
The maximum von Mises stress (MPa) in C4/C5 segment under different loading conditions
| Baseline | 100% | 125% | 150% | 175% | 200% | |
|---|---|---|---|---|---|---|
| Flexion | 0.208 | 0.242 | 0.236 | 0.221 | 0.307 | 0.387 |
| Extension | 0.313 | 0.383 | 0.327 | 0.340 | 0.467 | 0.489 |
| Rotate | 0.253 | 0.463 | 0.435 | 0.423 | 0.459 | 0.491 |
| Lateral bending | 0.272 | 0.469 | 0.460 | 0.384 | 0.455 | 0.472 |
Fig. 6The intradiscal pressure (IDP) of C6/C7 levels under different loading conditions.
The maximum von Mises stress (MPa) in C6/C7 segment under different loading conditions
| Baseline | 100% | 125% | 150% | 175% | 200% | |
|---|---|---|---|---|---|---|
| Flexion | 0.215 | 0.289 | 0.283 | 0.239 | 0.275 | 0.402 |
| Extension | 0.263 | 0.393 | 0.372 | 0.351 | 0.369 | 0.411 |
| Rotate | 0.352 | 0.427 | 0.403 | 0.379 | 0.386 | 0.461 |
| Lateral bending | 0.363 | 0.483 | 0.475 | 0.401 | 0.479 | 0.497 |
Fig. 7The range of motion (ROM) of C4/C5 levels under different loading conditions.
The ROM (°) in C4/C5 segment under different loading conditions
| Baseline | 100% | 125 | 150% | 175% | 200% | |
|---|---|---|---|---|---|---|
| Flexion | 4.8 | 7.3 | 6.8 | 6.0 | 7.0 | 7.9 |
| Extension | 4.1 | 8.3 | 7.3 | 7.9 | 8.0 | 8.5 |
| Rotate | 6.6 | 8.1 | 7.9 | 7.5 | 8.1 | 8.5 |
| Lateral bending | 7.8 | 10.3 | 9.7 | 9.0 | 10.2 | 11.0 |
ROM, range of motion.
Fig. 8The range of motion (ROM) of C6/C7 levels under different loading conditions.
The ROM (°) in C6/C7 segment under different loading conditions
| Baseline | 100% | 125% | 150% | 175% | 200% | |
|---|---|---|---|---|---|---|
| Flexion | 3.7 | 6 | 5.6 | 5.1 | 6.1 | 6.5 |
| Extension | 4.8 | 8.3 | 7.7 | 7.3 | 7.9 | 9.1 |
| Rotate | 3 | 3.8 | 3.6 | 3.4 | 3.7 | 4 |
| Lateral bending | 4.8 | 5.7 | 6.3 | 5.5 | 6.1 | 7 |
ROM, range of motion.