| Literature DB >> 26222819 |
Jun Dong1, Meng Lu1, Teng Lu1, Baobao Liang2, Junkui Xu3, Jie Qin1, Xuan Cai1, Sihua Huang1, Dong Wang1, Haopeng Li1, Xijing He1.
Abstract
OBJECTIVE: To determine the range of motion and stability of the human cadaveric cervical spine after the implantation of a novel artificial disc and vertebra system by comparing an intact group and a fusion group.Entities:
Mesh:
Year: 2015 PMID: 26222819 PMCID: PMC4496753 DOI: 10.6061/clinics/2015(07)06
Source DB: PubMed Journal: Clinics (Sao Paulo) ISSN: 1807-5932 Impact factor: 2.365
Figure 1The ADVS is made of a titanium alloy (Ti6Al4V), which has three major parts, two discs and a vertebra. There is a hemisphere socket joint between the disc and vertebra that theoretically allow 12° in flexion, extension and lateral bending, 360° in axial rotation. A) ADVS in flexion; B) ADVS in extension; C) the artificial vertebra part; D) the artificial disc part; E) the lateral view of ADVS. 1) the base part of disc, it has a smooth surface on the top that fits the adjacent vertebra; 2) the front wing part; 3) the articular fossa; 4) bone graft tubes in different diameter; 5) the articular head; 6) the “L” structure, which was designed for dislocation between the disc part and the vertebra part; 7) the self-drilling trapping screw; F) upper, middle and lower sagittal diameters of C5 vertebra; G) anterior, media and posterior height from C4∼5 disc to C5∼6 disc. The ADVS was implanted after corpectomy was performed at C5 level, X-ray films of posteroanterior view H) and lateral I) views. The anterior plate fusion performed after cervical discectomy and vertebral corpectomy of C5 level, X-ray films of posteroanterior view J) and lateral K) views.
C5 Vertebrae and C4−5 and C5−6 Disc Measurements (mm).
| Variable | Measured Values | ||
|---|---|---|---|
| Upper | 11.6−17.1 | 14.24±1.21 | |
| Middle | 13.1−18.9 | 15.6±1.34 | |
| Lower | 14.2−19.4 | 16.63±1.22 | |
| Anterior | 21.4–23.7 | 22.73±0.51 | |
| Middle | 23.2–25.4 | 24.45±0.54 | |
| Posterior | 18.8–20.6 | 19.98±0.58 |
Figure 2ROM of C3∼C7, C3∼4, C4∼6, C6∼7. The ROM were measured under 2 N·m torque loading pressure. A) the fusion group showed a significantly restricted ROM of C3∼C7 regarding flexion, extension and axial rotation ROM of C3∼C7 compared to the intact group and non-fusion group. No significant difference of ROM in any direction was detected when compared the intact group and non-fusion group. B) the fusion group and non-fusion group showed a significantly increased ROM of C3∼4 regarding extension and lateral bending ROM of C3∼4 compared to the intact group. Significant difference of ROM of C3∼4 in axial rotation was detected when compared the intact group and non-fusion group. C) the fusion group showed a significantly restricted ROM of C4∼6 in all directions compared to the intact group and non-fusion group. Comparing with the intact group, the extension and lateral bending ROM of C4∼6 in non-fusion group increased significantly. D) the fusion group showed a significantly restricted ROM of C6∼7 in extension compared to the intact group and non-fusion group. The axial rotation ROM of C6∼7 in non-fusion group decreased significantly comparing with the fusion group. No significant difference of ROM of C6∼7 in any direction was detected when compared the intact group and non-fusion group. *p<0.05
Average Range of Motion of the Specimens in the Intact, Non-Fusion and Fusion Groups in Response to the Maximum Applied Moment of 2 N·m (in degrees).
| Motion (mean±SD) | ROM of C3−C7 | ROM of C3−4 | ROM of C4−6 | ROM of C6−7 | ||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|
| INT | NF | FU | INT | NF | FU | INT | NF | FU | INT | NF | FU | |
| FLE | 13.41±2.09 | 13.84±1.40 | 9.63±1.74 | 3.34±1.13 | 4.20±0.82 | 4.68±0.92 | 5.99±1.22 | 4.72±1.04 | 0.79±0.29 | 3.39±0.90 | 3.36±0.41 | 3.88±0.58 |
| EXT | 14.66±1.69 | 14.16±2.07 | 11.21±1.68 | 1.92±0.80 | 3.52±0.73 | 2.96±0.44 | 7.83±1.22 | 9.88±1.74 | 1.57±0.73 | 4.29±0.81 | 4.05±0.56 | 6.14±1.06 |
| LB | 26.47±5.06 | 28.87±5.85 | 24.20±3.00 | 5.27±1.83 | 7.72±1.51 | 7.64±0.95 | 12.40±1.79 | 15.12±1.9 | 6.67±1.03 | 8.35±1.84 | 7.78±0.84 | 8.24±1.35 |
| AR | 32.40±4.78 | 35.26±4.16 | 26.75±1.30 | 7.65±1.58 | 6.95±0.91 | 8.00±0.61 | 25.51±2.91 | 26.23±2.91 | 6.63±1.39 | 20.80±3.61 | 19.34±1.47 | 22.37±2.49 |
ROM (range of motion), INT (intact), NF (non-fusion), FU (fusion), FLE (flexion), EXT (extension), LB (lateral bending), AR (axial rotation).
The values for axial rotation and lateral bending are the sums of both the right and left sides.
Significantly different from the intact group (p<0.05).
Significantly different from the fusion group (p<0.05).
Stability Index of the Flexibility Test.
| Motion | Average SI-ROM of C3−7 | Average SI-ROM of C3−4 | Average SI-ROM of C4−6 | Average SI-ROM of C6−7 | ||||
|---|---|---|---|---|---|---|---|---|
| NF | FU | NF | FU | NF | FU | NF | FU | |
| FLE | 0.020±0.16 | 0.20±0.22 | −0.40±0.57 | −0.52±0.57 | 0.17±0.33 | 0.86±0.068 | −0.040±0.24 | −0.23±0.45 |
| EXT | 0.077±0.17 | 0.18±0.18 | −1.13±0.98 | −0.81±0.79 | −0.31±0.43 | 0.80±0.088 | 0.039±0.17 | −0.45±0.23 |
| LB | −0.031±0.14 | 0.0022±0.18 | −0.63±0.64 | −0.60±0.60 | −0.25±0.30 | 0.45±0.11 | 0.035±0.22 | −0.020±0.23 |
| AR | −0.0081±0.10 | 0.087±0.11 | 0.064±0.21 | −0.073±0.16 | −0.03±0.074 | 0.74±0.063 | 0.047±0.17 | −0.12±0.32 |
SI-ROM (stability index range of motion), INT (intact), NF (non-fusion), FU (fusion), FLE (flexion), EXT (extension), LB (lateral bending), AR (axial rotation).
The values for axial rotation and lateral bending are the sums of both the right and left sides.
Significantly different from the fusion group (p<0.05).