| Literature DB >> 36225948 |
Jun Dong1, Baobao Liang2, Yuan Sun1, Xi Li1, Pei Han1, Chen Wang1, Yabing Song1, Hao Wu1, Ruoxi Liu1, Sihua Huang1, Sen Yu3, Lei Jin3, Zhentao Yu4, Liying Fan1, Huanjin Song1, Chun Zhang1, Xijing He1,5.
Abstract
Objective: Anterior cervical corpectomy and fusion (ACCF) has been widely used in the treatment of cervical spondylotic myelopathy (CSM) but is accompanied by unavoidable motion loss and destruction of vertebra. We aim to evaluate the range of motion (ROM) of caprine cervical spine constructs implanted with cervical artificial disc and vertebra system (ADVS). The purpose of this study was to investigate the biomechanical properties of the ADVS from an in vivo caprine cervical spine non-fusion model.Entities:
Keywords: Anterior cervical corpectomy and fusion; Biomechanics; Cervical artificial disc and vertebra system; Non-fusion; Range of motion
Year: 2022 PMID: 36225948 PMCID: PMC9523198 DOI: 10.1016/j.jot.2022.07.005
Source DB: PubMed Journal: J Orthop Translat ISSN: 2214-031X Impact factor: 4.889
Figure 1Photographs of ADVS. The artificial disc has an anterior plate (a, b). The angle between anterior plate and disc is 84° in upper artificial disc (A), 100° in lower artificial disc (b). A core (10 mm in diameter, 2 mm in height) is in the below-center of the disc surrounding with L-structure anteriorly & posteriorly for preventing the dislocation of disc from the vertebra (a, b). Two screw holes (3.5 mm in diameter) are designed in the middle of the anterior plate (c). Several zigzag crests are on the above surface of the disc (c). Four unicortical self-tapping screws (3.4 mm in diameter, 14–16 mm in length) are used for the fixation (d). The artificial vertebra is a quadrangular column (width: 14 mm; length: 35 mm; depth: 14 mm). Articular fovea matching to the core of the disc is designed cranially & caudally of the artificial vertebra (e, f, g). This hemisphere socket joint allows 18° ROM in flexion-extension and lateral bending, 360° ROM in rotation. Several tubes for bone graft are designed laterally (h).
Figure 2Process of implantation of ADVS. After sterilization, a right-sided anterolateral retropharyngeal approach to the cervical spine was used (a, b). C4 vertebral body was exposed following the incision and separation of soft tissue using high-frequency electrosurgical equipment (c, d). The median crests of C3 and C5 were localized by positioning needle, respectively (e). The C4 vertebra corpectomy was performed accompanied with the discectomy of C3-4 and C4-5 by using bone rongeur or nucleus pulposus forceps (f). A decompression groove (approximately width: 15 mm; length: 35 mm; depth: 15 mm) was made in the middle of C4 vertebra body (g). The assembled ADVS was filled with bone grafts and implanted into the decompression groove (h). Four unicortical self-tapping screws were fixed with a 20° trajectory in cranial and caudal direction, respectively (i).
Figure 3Photograph of biomechanics testing and radiological results. a: biomechanics testing of ADVS group; b: intact group; c: fixation group. Postoperative anteroposterior (d) and lateral (e) radiographs showed that ADVS was implanted at C4, no dislocation was observed. Postoperative CT of hardware enhanced model of 3D reconstruction anteroposterior (f) and laterally (g) images showed ADVS reconstructed the height of vertebra after corpectomy of C4. Screws were implanted into C3 vertebral body (h) and C5 vertebral body (i) respectively, no screw broke into the spinal canal. Sagittal (j) and axial (k) view of postoperative MRI T2 images showed that no compression to the spinal cord was observed.
Figure 4A typical load–displacement curve (a) and ROM curve (b) of C2-5 axial rotation.
Figure 5Average ROM of C2-3, C3-4, C4-5, C2-5 intervertebral space. a: flexion/extension; a1 C2-3 flexion/extension; a2: C3-4 flexion/extension; a3: C4-5 flexion/extension; a4: C2-5 flexion/extension. b: lateral bending; b1 C2-3 lateral bending; b2: C3-4 lateral bending; b3: C4-5 lateral bending; b4: C2-5 lateral bending. c: axial rotation; c1 C2-3 axial rotation; c2: C3-4 axial rotation; c3: C4-5 axial rotation; c4: C2-5 axial rotation. One asterisk means that there is statistically significant difference and p < 0.05. Two asterisks mean that there is statistically significant difference and p < 0.01.