| Literature DB >> 25880231 |
Chen-Sheng Chen1, Chang-Hung Huang2, Shih-Liang Shih3,4.
Abstract
BACKGROUND: Pedicle-screw-based posterior dynamic stabilization devices are designed to alleviate the rate of accelerated degeneration of the vertebral level adjacent to the level of spinal fusion. A new pedicle-screw-based posterior dynamic stabilization device- the Awesome Dynamic Rod System was designed with curve cuts on the rods to provide flexibility. The current study was conducted to evaluate the biomechanical properties of this new device.Entities:
Mesh:
Year: 2015 PMID: 25880231 PMCID: PMC4393882 DOI: 10.1186/s12891-015-0538-x
Source DB: PubMed Journal: BMC Musculoskelet Disord ISSN: 1471-2474 Impact factor: 2.362
Figure 1Spine and implant FE models used in this study. (A). The osseous structures, intervertebral discs, and ligaments of the intact spine. (B). The Awesome Dynamic Rod and Z-brace cage. (C). At the L4-L5 disc space, the Z-brace cage was placed obliquely with the left posterolateral corner of the annulus fibrosus removed as in PLIF procedures. (D). Four FE models used in this study.
ROM of four FE models at all motion segments
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| Flexion | INT | 3.63 (100%) | 3.74 (100%) | 3.71 (100%) | 5.22 (100%) | 3.8 (100%) | 0.23 (100%) |
| AWE | 4.85 (134%) | 4.79 (128%) | 4.72 (127%) | 1.84 (35%) | 8.4 (221%) | 0.52 (226%) | |
| FUS | 4.85 (134%) | 4.86 (130%) | 5.8 (156%) | 0.76 (15%) | 8.4 (221%) | 0.52 (226%) | |
| AWEFUS | 6.85 (189%) | 6.93 (185%) | 1.62 (44%) | 0.89 (17%) | 13.65 (359%) | 0.84 (365%) | |
| Extension | INT | 2.62 (100%) | 2.23 (100%) | 2.07 (100%) | 2.01 (100%) | 6.4 (100%) | 0.72 (100%) |
| AWE | 3.18 (121%) | 2.73 (122%) | 2.7 (130%) | 0.29 (14%) | 8.05 (126%) | 0.9 (125%) | |
| FUS | 3.08 (118%) | 2.63 (118%) | 2.57 (124%) | 0.55 (27%) | 7.7 (120%) | 0.87 (121%) | |
| AWEFUS | 4.14 (158%) | 3.56 (160%) | 0.5 (24%) | 0.74 (37%) | 11.55 (180%) | 1.29 (179%) | |
| Lateral Bending | INT | 7.11 (100%) | 5.2 (100%) | 5.07 (100%) | 5.01 (100%) | 8.2 (100%) | 0.37 (100%) |
| AWE | 9.42 (132%) | 6.18 (119%) | 5.73 (113%) | 1.18 (24%) | 11.9 (145%) | 0.53 (143%) | |
| FUS | 9.44 (133%) | 6.21 (119%) | 5.79 (114%) | 0.94 (19%) | 11.9 (145%) | 0.53 (143%) | |
| AWEFUS | 12.5 (176%) | 8.03 (154%) | 1.22 (24%) | 0.56 (11%) | 15.75 (192%) | 0.71 (192%) | |
| Torsion | INT | 5.58 (100%) | 2.9 (100%) | 3.4 (100%) | 4.74 (100%) | 9.7 (100%) | 0.58 (100%) |
| AWE | 7.86 (141%) | 3.14 (108%) | 3.43 (101%) | 2.18 (46%) | 15.05 (155%) | 0.91 (157%) | |
| FUS | 8.08 (145%) | 3.21 (111%) | 3.5 (103%) | 1.84 (39%) | 15.4 (159%) | 0.93 (160%) | |
| AWEFUS | 9.5 (170%) | 3.35 (116%) | 1.79 (53%) | 2.03 (43%) | 17.85 (184%) | 1.07 (184%) |
The percentages indicate the ROM of all models normalized by the ROM of INT.
Disc stresses at cephalic adjacent levels
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| Flexion | INT | 621 (100%) | 558 (100%) |
| AWE | 906 (146%) | 782 (140%) | |
| FUS | 915 (147%) | 944 (169%) | |
| AWEFUS | 1370 (221%) | 661 (118%) | |
| Extension | INT | 399 (100%) | 402 (100%) |
| AWE | 422 (106%) | 455 (113%) | |
| FUS | 410 (103%) | 437 (109%) | |
| AWEFUS | 525 (131%) | 184 (46%) | |
| Lateral Bending | INT | 1050 (100%) | 1040 (100%) |
| AWE | 1170 (111%) | 1090 (105%) | |
| FUS | 1180 (112%) | 1090 (105%) | |
| AWEFUS | 1840 (175%) | 405 (39%) | |
| Torsion | INT | 540 (100%) | 593 (100%) |
| AWE | 419 (78%) | 441 (74%) | |
| FUS | 436 (81%) | 454 (77%) | |
| AWEFUS | 488 (90%) | 322 (54%) |
The percentages indicate the disc stresses of all models normalized by the disc stresses of INT.
Facet joint forces in instrumented levels and cephalic adjacent levels
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| Extension | INT | 108 (100%) | 118 (100%) | 108 (100%) |
| AWE | 138 (128%) | 152 (129%) | 0 (0%) | |
| FUS | 132 (122%) | 145 (123%) | 0 (0%) | |
| AWEFUS | 208 (193%) | 0 (0%) | 0 (0%) | |
| Lateral Bending | INT | 40 (100%) | 15 (100%) | 21 (100%) |
| AWE | 51 (128%) | 44 (293%) | 0 (0%) | |
| FUS | 54 (135%) | 44 (293%) | 0 (0%) | |
| AWEFUS | 110 (275%) | 0 (0%) | 0 (0%) | |
| Torsion | INT | 141 (10%) | 143 (100%) | 135 (100%) |
| AWE | 196 (139%) | 204 (143%) | 3 (2%) | |
| FUS | 203 (144%) | 210 (147%) | 19 (14%) | |
| AWEFUS | 259 (184%) | 6 (4%) | 28 (21%) |
The percentages indicate the facet joint forces of all models normalized by the facet joint forces of INT.
Figure 2Comparison of disc annulus stress at the adjacent level L3-L4 in flexion. The maximum stress occurred at anterior edge of the annulus fibrosus. FUS showed the greatest stress. AWEFUS showed the lowest stress because levels L3-L4 were shielded by the Awesome Dynamic Rod System. AWE showed lower annulus stress than did FUS owing to its preservation of motion, which alleviated the effect of the adjacent level.