| Literature DB >> 30420962 |
Jason Coquim1, Joseph Clemenzi1, Mohsen Salahi1, Abdurahman Sherif1, Pouria Tavakkoli Avval2, Suraj Shah3, Emil H Schemitsch4,5, Z Shaghayegh Bagheri6, Habiba Bougherara1, Radovan Zdero1,4,5,7.
Abstract
This investigation assessed the biomechanical performance of the metal plate and bone strut technique for fixing recalcitrant nonunions of femur midshaft segmental defects, which has not been systematically done before. A finite element (FE) model was developed and then validated by experiments with the femur in 15 deg of adduction at a subclinical hip force of 1 kN. Then, FE analysis was done with the femur in 15 deg of adduction at a hip force of 3 kN representing about 4 x body weight for a 75 kg person to examine clinically relevant cases, such as an intact femur plus 8 different combinations of a lateral metal plate of fixed length, a medial bone strut of varying length, and varying numbers and locations of screws to secure the plate and strut around a midshaft defect. Using the traditional "high stiffness" femur-implant construct criterion, the repair technique using both a lateral plate and a medial strut fixed with the maximum possible number of screws would be the most desirable since it had the highest stiffness (1948 N/mm); moreover, this produced a peak femur cortical Von Mises stress (92 MPa) which was below the ultimate tensile strength of cortical bone. Conversely, using the more modern "low stiffness" femur-implant construct criterion, the repair technique using only a lateral plate but no medial strut provided the lowest stiffness (606 N/mm), which could potentially permit more in-line interfragmentary motion (i.e., perpendicular to the fracture gap, but in the direction of the femur shaft long axis) to enhance callus formation for secondary-type fracture healing; however, this also generated a peak femur cortical Von Mises stress (171 MPa) which was above the ultimate tensile strength of cortical bone.Entities:
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Year: 2018 PMID: 30420962 PMCID: PMC6211160 DOI: 10.1155/2018/4650308
Source DB: PubMed Journal: Biomed Res Int Impact factor: 3.411
Figure 1FE CAD model of the artificial femur showing Cases 1 to 9. Geometries, relative positions, and material properties replicated the experiments exactly. Anterior views are shown.
Figure 2Experimental methods showing (a) a repaired artificial femur for Case 5 with plate, strut, screws, and strain gages and (b) the test setup for applying load via the mechanical tester for Case 1 specimen.
Figure 3FEA versus experimental strains used for FE model validation at 1 kN and from similar previous femur fracture repair configurations studied by the current senior authors [17–19]. Data from Cases 1 to 9 are combined in a single graph because the same basic FE model was used for each case. Positive and negative values indicate, respectively, tensile and compressive strains. Equivalent elastic (Von Mises) strains are shown. Perfect agreement would be indicated by a slope =1 and a correlation coefficient R = 1.
Figure 4FEA axial stiffnesses at 3 kN of axial force for Cases 1 to 9.
FEA Von Mises peak surface stresses for a 3 kN axial force for all components of Cases 1 to 9. The location of each peak stress occurred at a particular screw or screw hole “level”.
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| 1 | 40 (inferior neck) | --- | --- | --- |
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| 2 | 113 (level #8) | 318 (level #8) | 378 (level #2) | 1033 (level #8) |
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| 3 | 96 (level #1) | 124 (level #7) | 325 (level #1) | 454 (level #7) |
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| 4 | 42 (level #1) | 89 (level #6) | 257 (level #1) | 293 (level #6) |
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| 5 | 92 (level #1) | 75 (level #5) | 122 (level #3) | 256 (level #4) |
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| 6 | 66 (level #2) | 70 (level #7) | 283 (level #3) | 227 (level #4) |
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| 7 | 86 (level #3) | 18 (level #4) | 313 (level #3) | 288 (level #4) |
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| 8 | 112 (level #4) | 127 (level #5) | 341 (level #3) | 388 (level #4) |
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| 9 | 171 (level #4) | --- | 1039 (level #3) | 1680 (level #4) |
Figure 5FEA stress maps of the femur cortical bone for an axial force of 3 kN for Case 1 (i.e., intact), Case 5 (i.e., stiffest), and Case 9 (i.e., softest). Equivalent elastic (Von Mises) stresses are shown. Red arrows are peak stresses. Internal stresses are not shown. Stress levels are not shown on the colour scale to avoid figure clutter, but the same colour scale applies to all FE cases.