- Open Access
Scoliosis corrective force estimation from the implanted rod deformation using 3D-FEM analysis
© Abe et al; licensee BioMed Central Ltd. 2015
- Published: 11 February 2015
Improvement of material property in spinal instrumentation has brought better deformity correction in scoliosis surgery in recent years. The increase of mechanical strength in instruments directly means the increase of force, which acts on bone-implant interface during scoliosis surgery. However, the actual correction force during the correction maneuver and safety margin of pull out force on each screw were not well known. In the present study, estimated corrective forces and pull out forces were analyzed using a novel method based on Finite Element Analysis (FEA).
Twenty adolescent idiopathic scoliosis patients (1 boy and 19 girls) who underwent reconstructive scoliosis surgery between June 2009 and Jun 2011 were included in this study. Scoliosis correction was performed with 6mm diameter titanium rod (Ti6Al7Nb) using the simultaneous double rod rotation technique (SDRRT) in all cases. The pre-maneuver and post-maneuver rod geometry was collected from intraoperative tracing and postoperative 3D-CT images, and 3D-FEA was performed with ANSYS. Cobb angle of major curve, correction rate and thoracic kyphosis were measured on X-ray images.
Average age at surgery was 14.8, and average fusion length was 8.9 segments. Major curve was corrected from 63.1 to 18.1 degrees in average and correction rate was 71.4%. Rod geometry showed significant change on the concave side. Curvature of the rod on concave and convex sides decreased from 33.6 to 17.8 degrees, and from 25.9 to 23.8 degrees, respectively. Estimated pull out forces at apical vertebrae were 160.0N in the concave side screw and 35.6N in the convex side screw. Estimated push in force at LIV and UIV were 305.1N in the concave side screw and 86.4N in the convex side screw.
Corrective force during scoliosis surgery was demonstrated to be about four times greater in the concave side than in convex side. Averaged pull out and push in force fell below previously reported safety margin. Therefore, the SDRRT maneuver was safe for correcting moderate magnitude curves. To prevent implant breakage or pedicle fracture during the maneuver in a severe curve correction, mobilization of spinal segment by releasing soft tissue or facet joint could be more important than using a stronger correction maneuver with a rigid implant.
- Pedicle Screw
- Thoracic Kyphosis
- Concave Side
- Adolescent Idiopathic Scoliosis Patient
- Major Curve
Development of novel correction maneuvers and improvement of material property in spinal instrumentation have resulted in better deformity correction in scoliosis surgery in recent years [1, 2]. Rod rotation maneuver and direct vertebral rotation technique using thoracic pedicle screw have provided better scoliosis correction, and use of rigid instruments such as cobalt-chromium alloy rod have also accelerated these trends of aggressive correction. The use of these aggressive correction maneuver could induce the increase of force exerted on bone-implant interface during scoliosis surgery. There were many biomechanical studies about holding strength of spinal instruments [3–6]. As regards corrective force exerted on the spinal instruments, several biomechanical models were developed to simulate scoliosis correction in-vitro [7–9]. However, there were only few reports which estimated the actual corrective force during correction maneuver in vivo [10, 11]. We have developed a novel method for estimating corrective force acting on the spine by investigating the geometrical change of implanted rod in scoliosis surgery [12, 13]. In the present study, estimated corrective forces and pull out forces exerted on the pedicle screw were analyzed using a novel method based on finite element analysis.
3D-CAD model of rod geometry was generated and Finite Element Analysis (FEA) was performed using ANSYS 11.0 according to the previously developed method reported by Salmingo et al [12, 13]. Material properties of this rod are Young's Modulus (E), yield stress (σY), yield strain (εY) and hardening coefficient (H) equal to105 GPa, 900 MPa, 8.57×10−3 and 2.41 GPa, respectively.
Push out or push in forces exerted on each screw on the bilateral side were estimated using FEA. The calculated forces represent also to the pullout and push-in forces acting at the vertebrae of the scoliosis patient since the implant is directly connected to the vertebra. The magnitudes of pullout and push-in forces were also estimated from the applied forces. The pullout or push-in force was defined as the pulling or pushing force acting normal to the implant curvature at the local coordinate plane (y-x plane since the rod is bent at one plane), Fig. 1. The pullout or push-in force was computed using the reaction force (i.e. opposite force acting at the spine) of the computed corrective force that deformed the rod during scoliosis surgery. The rod geometry was used to define the direction of the pullout or push-in force because its curvature constitutes the spine curvature after the surgical treatment of scoliosis. The rod geometry was approximated by quintic polynomial function using the previous method . A tangent angle β that is orthogonal to the pullout or push-in force axis was computed by evaluating the derivative of quintic polynomial function evaluated for location of each screw. The reaction force vector was resolved into component (Reaction force x Cosβ), equal to the magnitude of pullout or push-in force acting at the corresponding fixation level.
1. Measurement of radiological parameters
Essentially, corrective force cannot be exerted on the spinal implant beyond the limit of anchor holding strength during scoliosis surgery. If corrective force reaches the limit of anchor strength, implant breakage or bony fracture reported as “screw plowing” could occur . According to the results of the present study, averaged pull out and push in force exerted on each screw during SDRRT fell below previously reported safety margin , and therefore this maneuver was demonstrated to be safe for correcting a moderate magnitude curve. To prevent implant breakage or pedicle fracture during maneuver in more severe curve correction, destabilization of spinal segment by releasing soft tissue or facet joint could be more important rather than the use of excessive correction maneuver with rigid implant.
Less screws tend to be used in scoliosis surgery for economical reasons in recent years, and correction rates have been reported as not significantly different between the less density (1.0-1.25) group and the high density (1.75-2.0) group . Reduction of the implant density, however, also means the load exerted on each anchor is increased. Our simulation study showed that pull out force exerted on the screw in the apical vertebra increased 2.5 fold when screw density decreased from 2.0 to 1.0. To solve these problems, we can use the current simulation technology to estimate in-vivo forces on each spinal implant, to find out the safety margin of implant forces and to determine the best settings of anchors and correction maneuvers for scoliosis correction.
Corrective force during correction maneuver in scoliosis surgery and pull out forces acting on each pedicle screw were analyzed using a novel method based on Finite Element Analysis. Computational simulation based on in-vivo data makes difficult scoliosis surgery scientifically validated, which can improve safety and effectiveness of deformity correction.
This is the extended abstract of IRSSD 2014 program book .
Consent to publish for the article’s content and images provided as well as consent to participate was obtained from the patients and patient’s parents for this study
Publication charges for this collection were funded by IRSSD 2014 Sapporo.
This article has been published as part of Scoliosis Volume 10 Supplement 2, 2015: Research into Spinal Deformities 9: Short Papers from the IRSSD 2014 Meeting. The full contents of the supplement are available online at http://www.scoliosisjournal.com/supplements/10/S2.
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