| Literature DB >> 35898687 |
Kavita Gunasekaran1, Khairul Salleh Basaruddin1,2, Nor Amalina Muhayudin1, Abdul Razak Sulaiman3.
Abstract
This paper presents a systematic study in reviewing the application of finite element method for the analysis of correction mechanism of spine deformity due to scoliosis. The study is aimed at systematically (1) reviewing the use of finite element analysis in spine deformity case, (2) reviewing the modelling of pedicle screw and rod system in scoliosis surgery, and (3) analysing and discussing gap between the studies. Using the restricted key phrases, the review gathered studies from 2001 to 2021 from various electronic databases (Scopus, ScienceDirect, PubMed, Medline, and WorldCAT). Studies were included if they reported a finite element study on spine deformity. Studies that did not fully disclose their methodology and results had significant discrepancies, not published in English or not yet published were all disqualified. Regardless of inconsistencies in the methodological design of the studies, the quality of all papers was above the acceptable level. A total of fifteen manuscripts were considered for inclusion and were given a comprehensive review. This study indicates that analysing the forces acting on the spine, as well as the interrelationship between the force, stress, and degree of correction (which measured as the Cobb angle), could help to improve the corrective mechanism procedure of spine deformity. Pedicle screws and its placement strategies are also important as it influence the corrective forces for scoliosis treatment. Hence, the findings of this study could potentially be used as a guidance to develop a reliable finite element analysis that can predict the biomechanics responses during the corrective spine deformity treatment.Entities:
Mesh:
Year: 2022 PMID: 35898687 PMCID: PMC9314159 DOI: 10.1155/2022/5147221
Source DB: PubMed Journal: Biomed Res Int Impact factor: 3.246
Figure 1Sample of spine radiographs, (a) preoperatively and (b) postoperatively with having a single rod (anterior procedure) [3].
Figure 2The research selection procedure from the reviewed articles.
Overall score based on the articles that were reviewed.
| Authors and years | Questions | Overall score | Overall % | ||||||||||||
|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|---|
| 1 | 2 | 3 | 4 | 5 | 6 | 7 | 8 | 9 | 10 | 11 | 12 | 13 | |||
| Dumas et al. [ | 2 | 2 | 1 | 1 | 1 | 2 | 0 | 0 | 1 | 2 | 2 | 0 | 2 | 16/20 | 80.0 |
| Abolaeha et al. [ | 2 | 2 | NA | 1 | 1 | 0 | 1 | 2 | 2 | 2 | 2 | 0 | 2 | 18/20 | 90.0 |
| Salmingo et al. [ | 2 | 2 | 2 | 2 | 1 | 1 | 2 | 2 | 2 | 2 | 2 | 2 | 1 | 23/26 | 88.5 |
| Wang et al. [ | 2 | 2 | 0 | 0 | 1 | 0 | 0 | 2 | 2 | 2 | 2 | 2 | 2 | 17/18 | 94.4 |
| Driscoll et al. [ | 2 | 1 | 0 | 0 | NA | 0 | 1 | 2 | 2 | 2 | 2 | 0 | 2 | 14/16 | 87.5 |
| Salmingo et al. [ |
| 2 | 1 | 1 | 1 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 23/26 | 88.5 |
| Little et al. [ |
| 2 | 1 | 1 | 2 | 2 | 2 | 1 | 2 | 2 | 2 | 2 | 2 | 23/26 | 88.5 |
| Abe et al. [ | 2 | 2 | 2 | 2 | NA | 0 | 2 | 1 | 2 | 2 | 2 | 1 | 2 | 20/22 | 91.0 |
| Wang et al. [ | 2 | 2 | 2 | 2 | 1 | 0 | 1 | 2 | 2 | 2 | 2 | 2 | 1 | 21/24 | 87.5 |
| Clin et al. [ | 2 | 2 | 2 | 2 | NA | 0 | 2 | 1 | 2 | 2 | 2 | 2 | 2 | 21/22 | 95.5 |
| Balamurugan et al. [ | 2 | 2 | 0 | 0 | NA | 0 | 2 | 2 | 2 | 1 | 2 | 0 | 2 | 14/16 | 87.5 |
| Guan et al. [ | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 1 | 0 | 23/24 | 95.8 |
| Zhang et al. [ | 2 | 2 | 2 | 2 | 1 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 2 | 25/26 | 96.0 |
| He et al. [ | 2 | 2 | 2 | 2 | 0 | 1 | 2 | 2 | 2 | 2 | 2 | 1 | 1 | 21/24 | 87.5 |
| Chen et al. [ | 2 | 2 | 2 | 2 | 0 | 0 | 2 | 2 | 2 | 2 | 2 | 1 | 1 | 20/22 | 90.1 |
∗Note: significance evaluation: 2—yes; 1—limited detail; 0—no; NA: not applicable.
Participants' or models' characteristic.
| Authors | Condition/category | Number of participants/models | Gender | Anthropometric data | |
|---|---|---|---|---|---|
| Male | Female | ||||
| Dumas et al. [ | Postsurgical patients | 2 | NM | NM | Age: 30 and 35 |
| Abolaeha et al. [ | Postsurgical patients | NM | NM | NM | NM |
| Salmingo et al. [ | Postsurgical patients | 3 | 3 | 0 | Age: 16, 15 and 14 |
| Wang et al. [ | Postsurgical patients | 10 | 10 | 0 | Age: adolescent |
| Driscoll et al. [ | Spine finite element model | 1 | NM | NM | NM |
| Salmingo et al. [ | Pre- and postsurgical patients | 6 | NM | NM | Age: adolescent |
| Little et al. [ | Postsurgical patients | 8 | NM | NM | Age: adolescent |
| Abe et al. [ | Postsurgical patients | 20 | 1 | 19 | Age: adolescent |
| Wang et al. [ | Presurgical patient | 1 | 1 | 0 | Age: NM |
| Clin et al. [ | Postsurgical patients | 5 | 0 | 5 | Age: adolescent |
| Balamurugan et al. [ | Spine finite element model | 1 | NM | NM | NM |
| Guan et al. [ | Postsurgical patients | 1 | NM | NM | Age: 11 |
| Zhang et al. [ | Presurgical patients | 1 | 0 | 1 | Age: 14 |
| He et al. [ | Normal spine | 1 | 1 | 0 | Age: 40 |
| Chen et al. [ | Postsurgical patients | 1 | 0 | 1 | Age:15 |
Note: NM-not mentioned.
Variables of FEA studies on the corrective mechanism of spine deformity.
| Authors | Software(s) | Element type | Geometrical model | Loading and boundary conditions | Type of material | Mechanical properties |
|---|---|---|---|---|---|---|
| Dumas et al. [ | Ansys 6.0. | (i) Vertebra: beam element (ii) pelvic: beam element (iii) ligament: tension-only cable elements (iv) articular facets: surface contact element | A patient-specific FE model of interverbal disc constructed from CT image. | Displacement: between the bending test measurements and the standing position measurements, 3D motion of T1 in relation to the pelvis was estimated. | Screws and rod: elastoplastic materials | (i) Augmented bending stiffness (about |
| Abolaeha et al. [ | Abaqus 6.11-1 | (v) Vertebral and intervertebral disc: linear hexahedral | A previous patient-specific FE model of vertebral and interverbal disc constructed from X-ray image and CT scan | During the loading and spine growth simulation processes, the inferior extremity of L5 was constrained in all degrees of freedom. Each vertebra is subjected to a dispersed load. | Rod: stainless steel |
|
| Salmingo et al. [ | Computed tomography (CT), Solidworks 2010, ANSYS 11.0 | 10 node tetrahedral solid elements | A patient-specific FE model of spine constructed from CT image. | Forces, | Rod: titanium alloy (JIS T 7401-3) | E = 105 GPa yield stress ( |
| Wang et al. [ | Radiographic software, ADAMS 2005 software (Mechanical Dynamics) | NM | Previously developed FE model of thoracic spine. | NM | Pedicle screw: titanium rod: titanium |
|
| Driscoll et al. [ | ANSYS 130.0 APDL | NM | A patient-specific FE model of vertebral and interverbal disc constructed from CT image. | To regulate and measure movement, all bodies assigned multiple coordinate systems centred on their geometric centre of mass. | Screw: titanium (Ti 6Al-4 V, grade 5) rod: cobalt chrome | Pedicle screw: |
| Salmingo et al. [ | Solidworks 2010, ANSYS 11.0 | 10 node tetrahedral solid elements | Three-dimensional FE model of rod geometries before surgery. | Before surgery. Zero force | Polyaxially pedicle screws and implant rods: titanium |
|
| Little et al. [ | Computed tomography (CT), ABAQUS 6.9-1, Python 2.5 | (i) Screw: 8 node brick | A patient-specific FE model with ribcage and Osseo ligamentous spine | A “no separation” normal contact and frictionless tangential contact definition were defined between the both surface of the rod and the screw head. | Screw: titanium alloy | Screw: |
| Abe et al. [ | Solidworks 2010, Aquilion 64 CT scanner, ANSYS 11.0 | 10 node tetrahedral solid elements | A patient-specific model of rod geometry constructed from CT image. | NM | Rod: titanium rod (Ti6Al7Nb) |
|
| Wang et al. [ | Computed tomography (CT), ANSYS ICEM-CFD | Hexahedron element | A patient-specific FE model of the spine constructed from CT image. | The upper lamina terminals of T1 were subjected to a fixed loading force of 300 N, which simulated upper body gravity. | Pedicle screw and rod elastoplastic materials | Ligaments elasticity coefficient |
| Anterior longitudinal, | ||||||
| Clin et al. [ | ANSYS 14.5 | NM | A patient-specific FE model of the spine to pelvis | NM | Screw: titanium alloy |
|
| Balamurugan et al. [ | MIMICS 14.0 software, ANSYS 18.0 | NM | A patient-specific FE model of thoracolumbar constructed from CT image | All degrees of freedom were limited in the L5 vertebra. Assuming the patient's weight is 800 N (80 kg), apply a compressive force of 50 N all along | Rod: titanium | Cortical bone: |
| Guan et al. [ | Materialise mimics 19.0, Leuven, Abaqus, | Hexahedral elastic elements | A patient-specific FE model of the thoracic spine lumbar vertebrae constructed from CT image | T1 was limited to transverse plan movements. | Elastoplastic spine model | Posterior structure: |
| Zhang et al. [ | Solidworks 2020, Ansys Workbench 19.0 | Tetrahedral elements | A patient-specific FE model of the lumbar spine constructed from CT image | Apply a moment of 10 nm in the planes on the upper surface of the L1 vertebral body to simulate flexion, extension, left and right bending, left and right rotation. | Elastoplastic spine model | Cortical bone: |
| He et al. [ | Mimics 19.0, ANSYS 15.0 | Solid 187 tetrahedral elements | Three-dimensional finite element (FE) model of intervertebral disc and pedicle screw & rod system (PSRS). | 500 N applied to the models for directions of flexion, extension, lateral bending, and axial rotation | Screw and rod: titanium alloy | Cortical bone: |
| Chen et al. [ | CT scan, Solidworks | NM | Three-dimensional finite element (FE) model of the spine from CT, pedicle screw, and rod system. | NM | Rod: titanium alloy | Cortical bone |
∗Note: E: Young modulus; ν: Poisson ratio; K: the strength coefficient; NM: Not mentioned.
Data extraction on the effect of Cobb angles from the reviewed articles.
| Authors | Category | Plane | Situation/ Zone | Cobb Angle | Outcome Measures | Parameter Output | Findings | |||
|---|---|---|---|---|---|---|---|---|---|---|
| Dumas et al. [ | Simulation of clinical data and post-operative measurements comparison & rod rotation analysis | Lateral, Sagittal, Axial | Scheuermann hyper kyphosis | 50° | Rod rotation (°) | Lateral rotation= - | The surgeon's experience was consistent with models of two clinical situations of hypokyphosis and scoliosis. | |||
| Abolaeha et al. [ | Spinal growing rod analysis | Sagittal & Axial | Cycle of Adjustment period | Before | After | Magnitude of force | Compressive force (N) | Rod Displacement(mm) | The rod length was changed until the desired Cobb angle was achieved, which was decreased from an initial value of 37° to 28°. This necessitated a 5 mm lengthening of the rod, resulting in a correction force of 362 N. | |
| Salmingo et al. [ | The three-dimensional corrective forces analysis | Frontal (x-z plane) | Patient 1 | Before | After | 3D Forces(N), Stress, Strain Distribution | Only the rod geometry before and after the surgical treatment was used to analyse the distributions of forces that distorted the implant rod. | The highest force acting on each patient's screw ranged from 198 to 439 N. The force magnitude was clinically acceptable. The maximal forces were generated at each patient's lowest fixation level of vertebra. | ||
| Wang et al. [ | The corrective forces & bone-screw forces analysis | Sagittal & Axial | NA | Sagittal curve: 5.3° | Resultant Screw force(N) | TCF magnitudes vs resultant screw force magnitudes associated with monoaxial, dorsoaxial and polyaxial pedicle screw. | True corrective forces were 50±30N on average. For monoaxial, dorsoaxial and polyaxial screws, the average bone-screw forces were 229±140N, 141±99N, and 103±42N, respectively; the average EF magnitudes were 205±136N, 125±93N, & 65±39N respectively. | |||
| Driscoll et al. [ | The three-dimensional corrective force analysis | Transverse, Axial, & Sagittal | NA | Right thoracic: 73° | Screw pull-out force | T3 | 0 | Over the course of the surgical process simulation, stress in intervertebral discs discovered between instrumented vertebrae averaged 3.95MPa. | ||
| Salmingo et al. [ | The three-dimensional corrective forces analysis | Sagittal | Patient 1 | Before | After | Pull-out and push-in force | The screw density and implant implantation arrangement all contributed to a higher degree of correction. This shows that if more implants are put closer together, vertebrae can be easily altered. | Forces of correction are unrelated. Although increasing the number of implant screws reduced the magnitude of corrective forces, it did not result in a higher degree of correction. | ||
| Little et al.[ | The three-dimensional corrective forces analysis | Coronal | Patient 1 | Before | After | Degree of deformity correction, Compressive force profile | -3 | 400N | Endplate-to-endplate contact was seen on adjacent endplates of one or more intervertebral disc spaces in the instrumented curve after the surgical loading procedures, according to patient model predictions. | |
| Abe et al. [ | The corrective force estimation | NM | NA | Thoracic: 53°- 74° | Push out or push in forces | Convex | F1 | 113N | The concave side corrective force is four times greater than in convex side. | |
| Concave | F1 | 424N | ||||||||
| Flexion | L2-L3 | 3.28°-.4° | Axial compression- The rod was the part that was subjected to the most stress | |||||||
| Extension | L2-L3 | 2.3°-3.3° | ||||||||
| Wang et al. [ | The stress-strain analysis | Coronal | NA | Thoracolumbar: 53° | The ranges of motion (ROM) | Lateral Bending | L2-L3 | 3.31°-5.0° | ||
| Clin et al. [ | Pedicle screw design & Load-Sharing Capacity analysis | Transverse & coronal | NA | Thoracic: 53°-85° | Derotation force, axial torque | The average post-instrumentation force sustained by high and low-density implant patterns with varied pedicle screw design configurations was recorded, as well as the peak force experienced during surgery simulation. | Increased degrees of freedom in the screw head limit the screw's ability to cure coronal deformity while lowering bone-screw forces. | |||
| Balamurugan et al. [ | Effect on spine deformity correction | NM | NA | NM | Stress distribution | T5 | <0.5MPa | After surgery, the stress concentration is highest near the end of the lumber area. | ||
| Guan et al. [ | The three-dimensional corrective forces analysis | Coronal, sagittal and horizontal | (i) Forward bend | Thoracic: 14°-36° | Stress | As the 3D corrective forces increased, the cobb angle of the thoracolumbar section reduced, as did the rotation angle of the vertebra. The combined force correction effects were higher. | The objective functions were each lowered by 58%, 52%, and 63 percent. On the convex side of the highest displacement of the vertebral body, the optimal corrective forces point was found. | |||
| Zhang et al.[ | Stress distribution | Coronal, sagittal and frontal | NA | Frontal: 43° Lumbar: 45° | Stress distribution | Stress is concentrated on the lumbar vertebral body during flexion loading, with an unequal stress distribution on the left anterior side of the vertebral body (concave side). Stress in the lumbar spine is localised primarily at the pedicle of the vertebral arch and the lamina of the vertebral arch during extension load. | Under all loads, the range of motion (ROM) is reduced. Flexion loads cause a greater distribution of vertebral concave stress. The stress is concentrated in the L3 vertebral arch. | |||
| He at al. [ | The three-dimensional corrective forces analysis | Coronal, sagittal and horizontal | NA | NM | Stress shielding rate | FEA analysis of the new improved spinal correction system ISCS to determine its stability and biomechanical features, as well as a comparison of the ISCS to the pedicle screw and rod system (PSRS). | Maximum stress L2 vertebral body & L1/2 and L2/3 discs in PSRS were smaller than in ISCS. PSRS and ISCS have identical maximum stress in lateral bending and axial rotation directions. | |||
| Chen at al [ | The pedicle screw placement strategies | Sagittal | (a) All segments have pedicle screws placed. | Thoracic: 43° | Interaction force | 113N | Densities of pedicle | |||
Figure 3A spine with scoliosis with coronal, sagittal, and axial plane views [5].