| Literature DB >> 27601934 |
Leonard I Voronov1, Krzysztof B Siemionow2, Robert M Havey1, Gerard Carandang3, Avinash G Patwardhan1.
Abstract
INTRODUCTION: Lateral mass screw (LMS) fixation with plates or rods is the current standard procedure for posterior cervical fusion. Recently, implants placed between the facet joints have become available as an alternative to LMS or transfacet screws for patients with cervical spondylotic radiculopathy. The purpose of this study was to evaluate the biomechanical stability of the DTRAX(®) cervical cage for single- and two-level fusion and compare this to the stability achieved with LMS fixation with rods in a two-level construct.Entities:
Keywords: DTRAX cervical cage; biomechanics; cervical facets; cervical spine; lateral mass screw; posterior fusion
Year: 2016 PMID: 27601934 PMCID: PMC5003555 DOI: 10.2147/MDER.S111031
Source DB: PubMed Journal: Med Devices (Auckl) ISSN: 1179-1470
Figure 1DTRAX® (Providence Medical Technology, Walnut Creek, CA, USA) cervical cage with bone screw.
Note: Cage dimensions are 10 mm × 5.5 mm × 2.5 mm. The bone screw extends 3.5 mm through the fenestration at the superior aspect of the cage.
Figure 2Experimental setup during flexion–extension testing.
Note: Angular motions of the C2–C7 vertebrae relative to T1 were measured using an optoelectronic motion measurement system.
Figure 3Testing protocol.
Notes: (A) Intact, (B) C4–C6 LMS construct, (C) C5–C6 bilateral posterior cages, (D) C4–C6 bilateral posterior cages, (E) C4–C6 LMS construct with supplemental bilateral posterior cages.
Abbreviation: LMS, lateral mass screw.
Mean (SD) segmental ranges of motion (degree) for each condition under 0 N follower preload and 1.5 Nm load for each test condition
| Motion segment/testing mode | Intact | C4–C6 LMS fusion | C5–C6 posterior cages | C4–C6 posterior cages | C4–C6 posterior cages + LMS fusion |
|---|---|---|---|---|---|
| Flexion–extension | 9.0±2.5 | 10.1±2.5 | 10.1±2.6 | 10.2±2.5 | 10.1±2.5 |
| Lateral bending | 11.2±3.0 | 10.6±2.2 | 11.1±2.5 | 10.4±2.5 | 10.5±2.3 |
| Axial rotation | 6.9±2.4 | 8.0±2.5 | 8.1±2.7 | 8.9±2.7 | 8.8±2.6 |
| Flexion–extension | 8.6±2.0 | 1.4±0.7 | 9.8±1.8 | 2.0±1.1 | 1.2±0.7 |
| Lateral bending | 9.8±1.2 | 0.5±0.2 | 9.3±1.5 | 0.1±0.3 | 0.3±0.2 |
| Axial rotation | 9.3±3.2 | 1.0±0.6 | 10.0±3.3 | 0.5±0.3 | 0.5±3.3 |
| Flexion-extension | 11.5±3.5 | 1.6±0.7 | 3.4±1.8 | 3.1±1.7 | 1.1±0.6 |
| Lateral bending | 10.0±2.1 | 0.7±0.3 | 0.7±0.5 | 0.5±0.5 | 0.4±0.3 |
| Axial rotation | 8.5±2.1 | 1.2±0.4 | 0.8±0.5 | 0.8±0.6 | 0.5±0.2 |
| Flexion–extension | 9.3±1.6 | 8.7±2.9 | 8.5±3.2 | 8.8±2.9 | 8.8±3.2 |
| Lateral bending | 6.7±2.1 | 6.1±3.2 | 6.1±3.3 | 6.4±3.3 | 6.4±3.3 |
| Axial rotation | 4.7±1.8 | 4.2±2.4 | 4.5±2.3 | 4.7±2.3 | 4.6±2.6 |
| Flexion–extension | 20.2±5.2 | 3.1±1.3 | 12.5±3.5 | 5.0±2.6 | 2.2±1.2 |
| Lateral bending | 10.8±2.6 | 1.2±0.4 | 10.0±1.6 | 0.6±0.3 | 0.7±0.3 |
| Axial rotation | 17.8±5.1 | 2.2±0.9 | 10.8±3.6 | 1.3±1.0 | 1.0±0.5 |
Note:
Significance from intact at P<0.05.
Abbreviations: LMS, lateral mass screw; SD, standard deviation.
Differences across conditions at C4–C6 using one-way ANOVA with Bonferroni correction
| C4–C6 ROM – Paired | |||
|---|---|---|---|
| Intact vs posterior cages | Posterior cages vs LMS | LMS vs LMS with posterior cages | |
| Flexion–extension | 0.000 | 0.014 | 0.030 |
| Lateral bending | 0.000 | 0.867 | 0.076 |
| Axial rotation | 0.001 | 0.784 | 0.016 |
Abbreviations: ANOVA, analysis of variance; LMS, lateral mass screw; ROM, range of motion.