| Literature DB >> 24772140 |
Zhou Jiang-Jun1, Zhao Min2, Yan Ya-Bo3, Lei Wei4, Lv Ren-Fa5, Zhu Zhi-Yu6, Chen Rong-Jian7, Yu Wei-Tao8, Du Cheng-Fei9.
Abstract
OBJECTIVE: Finite element analysis was used to compare preoperative and postoperative stress distribution of a bone healing model of femur fracture, to identify whether broken ends of fractured bone would break or not after fixation dislodgement one year after intramedullary nailing. Method s: Using fast, personalized imaging, bone healing models of femur fracture were constructed based on data from multi-slice spiral computed tomography using Mimics, Geomagic Studio, and Abaqus software packages. The intramedullary pin was removed by Boolean operations before fixation was dislodged. Loads were applied on each model to simulate a person standing on one leg. The von Mises stress distribution, maximum stress, and its location was observed. Results : According to 10 kinds of display groups based on material assignment, the nodes of maximum and minimum von Mises stress were the same before and after dislodgement, and all nodes of maximum von Mises stress were outside the fracture line. The maximum von Mises stress node was situated at the bottom quarter of the femur. The von Mises stress distribution was identical before and after surgery. Conclusion : Fast, personalized model establishment can simulate fixation dislodgement before operation, and personalized finite element analysis was performed to successfully predict whether nail dislodgement would disrupt femur fracture or not.Entities:
Keywords: Biomechanics; Bone healing model; Femur fracture; Finite element analysis; Intramedullary pin
Year: 2014 PMID: 24772140 PMCID: PMC3999007
Source DB: PubMed Journal: Pak J Med Sci ISSN: 1681-715X Impact factor: 1.088
The maximum and minimum von Mises stress for different materials before operation (Pa).
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| All | 1.059E+08 | 0.000E+00 | 3.178E+07 | 0.000E+00 |
| mat1 | 1.585E+01 | 1.145E+00 | 4.754E+00 | 3.434E+00 |
| mat2 | 2.198E+01 | 3.153E-01 | 6.594E+01 | 9.459E-01 |
| mat3 | 5.422E+06 | 0.000E+00 | 1.626E+07 | 0.000E+00 |
| mat4 | 7.892E+07 | 0.000E+00 | 2.368E+08 | 0.000E+00 |
| mat5 | 5.713E+07 | 0.000E+00 | 1.714E+08 | 0.000E+00 |
| mat6 | 8.612E+07 | 0.000E+00 | 2.584E+08 | 0.000E+00 |
| mat7 | 1.043E+08 | 8.080E+05 | 3.129E+08 | 2.424E+06 |
| mat8 | 1.059E+08 | 2.143E+06 | 3.178E+08 | 6.429E+06 |
| mat9 | 4.808E+07 | 3.053E+06 | 1.442E+08 | 9.160E+06 |
| mat10 | 4.747E+07 | 3.081E+06 | 1.424E+08 | 9.243E+06 |
The maximum von Mises stress.
The maximum and minimum von Mises stress for different materials after operation (Pa).
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| All | 7.122E+07 | 0.000E+00 | 2.137E+08 | 0.000E+00 |
| mat1 | 4.233E+00 | 5.879E-01 | 1.270E+01 | 1.764E+00 |
| mat2 | 4.716E+00 | 1.281E+00 | 1.415E+01 | 3.843E+00 |
| mat3 | 6.195E+00 | 1.168E+00 | 1.859E+01 | 3.504E+00 |
| mat4 | 1.181E+02 | 0.000E+00 | 3.544E+02 | 0.000E+00 |
| mat5 | 4.211E+07 | 0.000E+00 | 1.263E+08 | 0.000E+00 |
| mat6 | 5.114E+07 | 0.000E+00 | 1.534E+08 | 0.000E+00 |
| mat7 | 6.283E+07 | 0.000E+00 | 1.885E+08 | 0.000E+00 |
| mat8 | 7.122E+07 | 4.254E-21 | 2.137E+08 | 1.276E-20 |
| mat9 | 6.696E+07 | 6.496E+05 | 2.009E+08 | 1.949E+06 |
| mat10 | 5.894E+07 | 1.346E+06 | 1.768E+08 | 4.038E+06 |
The maximum von Mises stress.
The material properties before and after operation
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| mat1 | -8.186E+05 | 1.000E+03 | 0.3 | -8.989E+05 | 1.000E+03 | 0.3 |
| mat2 | -4.047E+05 | 1.000E+03 | 0.3 | -6.139E+05 | 1.000E+03 | 0.3 |
| mat3 | 9.191E+03 | 5.446E+07 | 0.3 | -3.290E+05 | 1.000E+03 | 0.3 |
| mat4 | 4.231E+05 | 2.507E+09 | 0.3 | -4.398E+04 | 1.000E+03 | 0.3 |
| mat5 | 8.370E+05 | 4.959E+09 | 0.3 | 2.410E+05 | 1.428E+09 | 0.3 |
| mat6 | 1.251E+06 | 7.411E+09 | 0.3 | 5.260E+05 | 3.116E+09 | 0.3 |
| mat7 | 1.665E+06 | 9.864E+09 | 0.3 | 8.110E+05 | 4.850E+08 | 0.3 |
| mat8 | 2.079E+06 | 1.232E+10 | 0.3 | 1.096E+06 | 6.494E+09 | 0.3 |
| mat9 | 2.493E+06 | 1.470E+02 | 0.3 | 1.381E+06 | 8.182E+09 | 0.3 |
| mat10 | 2.906E+06 | 1.722E+10 | 0.3 | 1.666E+06 | 9.871E+09 | 0.3 |
Fig.1The maximum and minimum von Mises stress of material all and material 08 under nine times weight load before operation
Fig.2The maximum and minimum von Mises stress of material all and material 08 under nine times weight load after operation