However, intraoperative flipping of a patient may aggravate cervical spinal cord injury. To solve this problem, some (1,28) have adopted the transoropharyngeal atlantoaxial reduction plate (TARP); however, this fusion technique restricts normal physiological range of motion (ROM) of the upper cervical spine. Several prospective studies of artificial atlantoodontoid joint (AAOJ) replacement have been reported (11-13,18) but finite element biomechanical analysis of AAOJ has not yet been reported to the authors knowledge. We reported a design of an AAOJ that can not only rebuild the stability of the atlanto-axial joint, but also reserve the rotation function █
INTRODUCTIONThe anterior high cervical spine fusion technique is often performed to relieve ventral compression and to improve the stability of the craniovertebral junction (CVJ) (8,10,17,24). Some of the indications include congenital atlanto-occipital fusion induced C1-C2 joint laxity and chronic dislocation; basilar invagination; congenital odontoid malformation caused C1-C2 dislocation; rheumatoid arthritis induced compression and C1-C2 dislocation; and brainstem and cord compression from CVJ tumors. These are typically treated by transoral decompression combined with posterior fusion (1,2,5).
AIM:To investigate the stress distribution on artificial atlantoaxial-odontoid joint (AAOJ) components during flexion, extension, lateral bending and rotation of AAOJ model constructed with the finite element (FE) method.
MATERIAL and METHODS:Human cadaver specimens of normal AAOJ were CT scanned with 1 mm -thickness and transferred into Mimics software to reconstruct the three-dimensional models of AAOJ. These data were imported into Freeform software to place a AAOJ into a atlantoaxial model. With Ansys software, a geometric model of AAOJ was built. Perpendicular downward pressure of 40 N was applied to simulate gravity of a skull, then 1.53 N• m torque was exerted separately to simulate the range of motion of the model.
RESULTS:An FE model of atlantoaxial joint after AAOJ replacement was constructed with a total of 103 053 units and 26 324 nodes. In flexion, extension, right lateral bending and right rotation, the AAOJ displacement was 1.109 mm, 3.31 mm, 0.528 mm, and 9.678 mm, respectively, and the range of motion was 1.6°, 5.1°, 4.6° and 22°.CONCLUSION: During all ROM, stress distribution of atlas-axis changed after AAOJ replacement indicating that AAOJ can offload stress. The stress distribution in the AAOJ can be successfully analyzed with the FE method.