| Literature DB >> 33836709 |
Xing Guo1,2, Jiaming Zhou1,2, Yueyang Tian1,2, Liang Kang1,2, Yuan Xue3,4.
Abstract
BACKGROUND: The plate-to-disc distance (PDD) is an important factor affecting the degeneration of adjacent segments after anterior cervical discectomy and fusion (ACDF). However, the most suitable PDD is controversial. This study examined the adjacent intervertebral disc stress, bone graft stress, titanium plate stress and screw stress to evaluate the biomechanical effect of different PDD on surgical segment and adjacent segment following C5/C6 ACDF.Entities:
Keywords: Adjacent segment degeneration; Biomechanical effect; Cervical vertebrae; Complication; Degenerative disc disease; Finite element analysis; Plate-to-disc distance; Spinal fusion; Spine surgery
Year: 2021 PMID: 33836709 PMCID: PMC8035773 DOI: 10.1186/s12891-021-04218-4
Source DB: PubMed Journal: BMC Musculoskelet Disord ISSN: 1471-2474 Impact factor: 2.362
Fig. 1Finite element models of C4–C7 cervical spine and other structures and details. a Frontal view of preoperative model; b Lateral view of preoperative model; c Loading and boundary condition; d Intervertebral disc details; e Vertebral body details
Demographics of study participants (n = 10)
| Variables | Median (Q1, Q3) | Range |
|---|---|---|
| Age (years) | 26.00 (24.75,27.25) | (23.00–29.00) |
| Height (cm) | 169.50 (162.25,173.50) | (160.00–177.00) |
| Weight (kg) | 63.75 (56.88,73.13) | (54.00–80.00) |
| BMI (kg/m2) | 22.30 (21.51,24.49) | (21.09–25.54) |
BMI Body mass index
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 | 3-noded triangular shell | 12,000 | 0.3 |
| Cancellous bone | 4-noded tetrahedron | 100 | 0.2 |
| Posterior elements | 4-noded tetrahedron | 3500 | 0.25 |
| Facet cartilage | 4-noded tetrahedron | 10.4 | 0.4 |
| End plate | 4-noded tetrahedron | 600 | 0.3 |
| Nucleus pulposus | 8-noded brick | 1 | 0.49 |
| Annulus ground substance | 8-noded brick | 3.4 | 0.4 |
| Annulus fibers | Truss (tension-only) | 450 | 0.45 |
| Titanium plate | 4-noded tetrahedron | 120,000 | 0.3 |
| Titanium screw | 4-noded tetrahedron | 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 | 62,340 | 146,282 |
| Mesh 2 | 129,770 | 282,016 |
| Mesh 3 | 186,736 | 396,958 |
Fig. 2a and b Frontal and lateral view of postoperative model with long PDD titanium plate; c and d Frontal and lateral view of postoperative model with middle PDD titanium plate; e and f Frontal and lateral view of postoperative model with short PDD titanium plate. PDD plate-to-disc distance
Fig. 3The predicted percentage differences of von Mises stress between Mesh 1 and Mesh 2 and between Mesh 2 and Mesh 3 in different structures for Volunteer 1 in the axial rotation
ROM (°) of each segment under different loading conditions
| Load scheme | Experiment data (mean ± SD) | Current model [median (min, max)] | ||||
|---|---|---|---|---|---|---|
| C4/5 | C5/6 | C6/7 | C4/5 | C5/6 | C6/7 | |
| Flexion | 5.3 ± 3.0 | 5.5 ± 2.6 | 3.7 ± 2.1 | 5.9 (4.9, 7.6) | 6.0 (4.8, 7.3) | 3.9 (2.6, 5.0) |
| Extension | 4.8 ± 1.9 | 4.4 ± 2.8 | 3.4 ± 1.9 | 5.3 (3.8, 6.3) | 5.8 (3.7, 6.6) | 4.3 (3.1, 5.0) |
| Rotation | 6.8 ± 1.3 | 5.0 ± 1.0 | 2.9 ± 0.8 | 6.7 (5.6, 7.4) | 5.4 (4.1, 6.0) | 2.9 (2.2, 3.6) |
| Lateral bending | 9.3 ± 1.7 | 6.5 ± 1.5 | 5.4 ± 1.5 | 8.9 (7.9, 10.6) | 6.6 (5.2, 7.6) | 5.8 (4.6, 6.6) |
ROM Range of motion, SD Standard deviation
Fig. 4The predicted ROM of the preoperative model was validated by previous published study. All the predicted data in our study occurred within the standard deviation of the mean values of the previous literature. ROM range of motion
The von Mises stress of the structures in different lengths of titanium plates
| von Mises stress (MPa) | PDD = 0 mm | PDD = 5 mm | PDD = 10 mm | F | η2 | ||
|---|---|---|---|---|---|---|---|
| Flexion | C4/C5 disc | 1.417 ± 0.297 | 1.411 ± 0.257 | 1.422 ± 0.271 | 0.406 | 0.671 | 0.029 |
| C6/C7 disc | 1.483 ± 0.036 | 1.476 ± 0.045 | 1.455 ± 0.030 | 1.495 | 0.242 | 0.100 | |
| Bone graft | 0.255 ± 0.040 * # | 0.307 ± 0.025 # | 0.400 ± 0.031 | 49.897 | < 0.001 | 0.787 | |
| Titanium plate | 57.886 ± 3.374 * # | 48.363 ± 4.237 # | 36.822 ± 1.049 | 109.670 | < 0.001 | 0.890 | |
| Screw | 32.983 ± 1.238 * # | 42.075 ± 3.569 # | 58.018 ± 3.083 | 202.663 | < 0.001 | 0.938 | |
| Extension | C4/C5 disc | 1.337 ± 0.027 | 1.333 ± 0.019 | 1.346 ± 0.032 | 0.619 | 0.546 | 0.044 |
| C6/C7 disc | 1.425 ± 0.027 | 1.419 ± 0.016 | 1.413 ± 0.018 | 0.751 | 0.482 | 0.053 | |
| Bone graft | 1.527 ± 0.051 * # | 1.668 ± 0.042 # | 1.812 ± 0.053 | 84.109 | < 0.001 | 0.862 | |
| Titanium plate | 58.069 ± 6.173 * # | 41.552 ± 3.822 # | 24.791 ± 1.740 | 148.985 | < 0.001 | 0.917 | |
| Screw | 34.820 ± 1.386 * # | 58.166 ± 3.206 # | 95.603 ± 2.204 | 1653.432 | < 0.001 | 0.992 | |
| Bending | C4/C5 disc | 1.382 ± 0.038 | 1.426 ± 0.119 | 1.388 ± 0.041 | 0.957 | 0.397 | 0.066 |
| C6/C7 disc | 1.402 ± 0.030 | 1.415 ± 0.032 | 1.398 ± 0.020 | 0.960 | 0.395 | 0.066 | |
| Bone graft | 1.522 ± 0.084 * # | 1.868 ± 0.057 # | 2.308 ± 0.055 | 349.902 | < 0.001 | 0.963 | |
| Titanium plate | 94.691 ± 1.859 * # | 83.956 ± 2.769 # | 73.790 ± 1.708 | 233.352 | < 0.001 | 0.945 | |
| Screw | 55.388 ± 1.090 * # | 60.705 ± 1.258 # | 66.406 ± 0.647 | 285.569 | < 0.001 | 0.955 | |
| Rotation | C4/C5 disc | 1.384 ± 0.047 | 1.378 ± 0.036 | 1.387 ± 0.038 | 0.112 | 0.895 | 0.008 |
| C6/C7 disc | 1.351 ± 0.170 | 1.292 ± 0.170 | 1.224 ± 0.080 | 1.912 | 0.167 | 0.124 | |
| Bone graft | 1.620 ± 0.026 * # | 1.714 ± 0.053 # | 1.945 ± 0.041 | 161.710 | < 0.001 | 0.923 | |
| Titanium plate | 68.463 ± 2.529 * # | 62.311 ± 2.526 # | 57.824 ± 0.929 | 62.751 | < 0.001 | 0.823 | |
| Screw | 56.617 ± 1.467 * # | 64.038 ± 1.663 # | 75.025 ± 2.727 | 208.241 | < 0.001 | 0.939 | |
PDD Plate-to-disc distance
P<0.05:Compared with titanium plates of 5 mm PDD
# P<0.05:Compared with titanium plates of 10 mm PDD
Fig. 5The von Mises stress distribution diagram of adjacent intervertebral discs with different PDD titanium plates under different loading conditions (a C4/C5; b C6/C7). PDD plate-to-disc distance
Fig. 6The von Mises stress distribution diagram of bone graft with different PDD titanium plates under different loading conditions. PDD plate-to-disc distance
Fig. 7The von Mises stress distribution diagram of titanium plate and screw with different PDD titanium plates under different loading conditions. PDD plate-to-disc distance