| Literature DB >> 32195235 |
Chia-En Wong1, Hsuan-Teh Hu2, Meng-Pu Hsieh2, Kuo-Yuan Huang3.
Abstract
Hybrid surgery (HS) allows surgeons to tailor fusion and arthroplasty in the treatment of multiple-level cervical disc degeneration. However, the decision making of selecting either ACDF or ADR for each level in three-level HS remains controversial and has not been fully investigated. This study was aimed to optimize three-level cervical hybrid constructs by systematically investigating their biomechanical properties and their effect on adjacent levels. A finite element model of cervical spine (C2-C7) was developed, and eight C3-C6 surgical models including six HS were constructed. The range of motion (ROM) in flexion, extension, lateral bending, and axial rotation under 2.0 Nm moments with 30 N follower load were simulated. The von Mises stress, strain energy at the adjacent intervertebral disc (IVD) and force at the adjacent facet were calculated. The ROM of the hybrid constructs and adjacent levels was close to that of the intact spine. HS with arthroplasty performed at C5-6 had better performance in terms of ROM reduction at the inferior adjacent level (C6-7). Moreover, C-D-D and 3ADR had best performance in reducing the von Mises stress and strain energy at C6-7. All HS reduced the facet burden at both C2-3 and C6-7 levels. However, the major drawback of HS revealed here is that the effect of C6-7 protection is at the cost of increased C2-3 IVD burden. In conclusion, we recommend C-D-D and 3ADR for patient with C3-C6 disc degeneration without predisposing C2-3 condition. C-C-D could be a good alternative with a lower medical cost. This analysis guides the decision making in three-level cervical HS before future cadaver studies or human clinical trials.Entities:
Keywords: ACDF; artificial disc replacement; biomechanics; cervical degenerative disc disease; finite element; hybrid surgery
Year: 2020 PMID: 32195235 PMCID: PMC7064443 DOI: 10.3389/fbioe.2020.00154
Source DB: PubMed Journal: Front Bioeng Biotechnol ISSN: 2296-4185
FIGURE 1Finite element model of intact C2–C7 and cervical discectomy.
Material property and mesh type of the cervical finite element model.
| Inner laminate: Inner layer | 360 | 0.30 |
| Inner laminate: Middle layer | 385 | 0.30 |
| Inner laminate: Outer layer | 420 | 0.30 |
| Outer laminate: Inner layer | 440 | 0.30 |
| Outer laminate: Middle layer | 495 | 0.30 |
| Outer laminate: Outer layer | 550 | 0.30 |
| Annulus ground substance | 4.2 | 0.45 |
| Cancellous bone | 100 | 0.20 |
| Cortical bone | 12000 | 0.30 |
| Posterior bony elements | 3500 | 0.25 |
| Endplate | 12000 | 0.30 |
| Nucleus pulposus | 1 | 0.49 |
| ALL/PLL/LF/ISL/SSL | 20/20/20/10/10 | 0.25 |
| CoCrMo | 200000 | 0.30 |
| Artificial disc inlay (UMHWPE) | 2400 | 0.30 |
| Graft bone | 100 | 0.20 |
| Cage (PEEK) | 3600 | 0.25 |
Properties of the ligaments in the present study.
| Elastic modulus (small strain) (MPa) | 7.8 | 10 | 15 | 10 | 8 |
| Transition strain (%) | 12 | 11 | 6.2 | 14 | 20 |
| Elastic modulus (large strain) (MPa) | 20 | 20 | 19.5 | 11.6 | 15 |
| Cross sectional area (mm2) | 63.7 | 20 | 40 | 40 | 30 |
Element type and number of element in the intact cervical spine finite element model.
| Cortical bone | S3R | 2580 | 1991 | 2435 | 2732 | 2782 | 2485 |
| Cancellous bone | C3D4 | 12645 | 11369 | 14792 | 16634 | 17048 | 13470 |
| Endplate | S3R | 710 | 828 | 883 | 865 | 960 | 867 |
| Posterior bony elements | C3D4 | 16211 | 11427 | 12514 | 14259 | 11829 | 14782 |
| Nucleus pulposus | C3D4 | 2017 | 2061 | 2130 | 2372 | 3273 | |
| Annulus ground substance | C3D4 | 3120 | 2756 | 3442 | 3483 | 4330 | |
| Annulus fiber | STRI3 | 1209 | 1044 | 1295 | 1419 | 1649 | |
| Ligament | |||||||
| No. of elements | T3D2 | 25 | 20 | 20 | 15 | 10 | |
FIGURE 2Finite element model of cervical surgical implants.
FIGURE 3Comparison of C2–C7 cervical ROM and IVD stress with the literature.
Facet contact force in the intact cervical segments.
| Preload (N) | 30 | 73.6 | 73.6 |
| Facet contact force (N) | 4.64 | 11 | 8.4 |
| Contact force/preload (%) | 15.5 | 14.9 | 11.4 |
FIGURE 4Range of motion and distribution in different cervical constructs.
FIGURE 5Comparison of adjacent level ROM in different cervical constructs.
FIGURE 6Maximal von Mises stress and strain energy at adjacent level in different cervical constructs.
FIGURE 7Total force at adjacent level facets during extension in different cervical constructs.