scholarly journals Study of the Stress-Strain State of the "Spine-Implant" System in Different Types of Tumor Lesions

2020 ◽  
Vol 5 (6) ◽  
pp. 241-246
Author(s):  
A. Popov ◽  
◽  
D. Petrenko ◽  
O. Yaresko ◽  
◽  
...  

Lesions resulting from the oncological process disrupt the structural stability of the spine and lead to pathological fractures and compression of the spinal cord structures. Surgical interventions used for spinal neoplasms can be both palliative and radical. Any of these surgical procedures significantly changes the biomechanical conditions of the spine functioning, and the wrong choice of surgical tactics can lead to fatal errors. The purpose of the study was to investigate the stress-strain state of the spine and the "spine-implant" system in various types of tumor lesions before and after stabilization surgical interventions. Material and methods. The model was built in the SolidWorks software. The calculations based on the finite element method and the analysis of the results were carried out in the ANSYS Workbench program. In the course of the study, a comparison was made between the character of stress-strain state distribution in the intact model and in models where the following changes were modeled: lesion of the T12 vertebral body by a tumor process by 30% of its volume (model 1) and cement augmentation of the created defect (model 2), and also lesions of the vertebral body by 60% with concomitant local kyphosis L5 (model 3) and stabilization with a transpedicular construction T10-L2 (model 4). Results and discussion. Based on the results of the calculations, it was determined that the presence of a T12 vertebral body defect by up to 30% leads to an increase in the absolute values of stresses in the vertebral body and the posterior supporting complex, while cement augmentation leads to the restoration of stress values close to the intact spine. Consequently, the presence of a pathological lesion in the vertebral body, occupying up to 60% of its volume, leads to disturbances in the supporting function of not only the affected segment, but also the segments adjacent to it. Placement of a transpedicular implant and restoration of the support of the anterior column of the affected vertebra makes it possible to bring the state of load distribution of the affected area of the spine closer to normal values. Conclusion. The study of the stress-strain state of the "spine-implant" system in the presence of a pathological lesion occupying 30% of the volume of the vertebral body leads to a violation of the supporting function of the affected vertebra, and an increase in the defect to 60% of the volume of the vertebral body and the presence of local kyphotic deformity of the spine negatively affects the distribution stresses in the segments that are adjacent to it. The use of cement augmentation and transpedicular construction allows the support function of the spine to be restored in accordance with normal parameters of load distribution. Indications for the use of cement vertebroplasty is the presence of a defect up to 30% of the volume of the vertebral body. In the case of the volume increase of the vertebra defect up to 60% and the occurrence of kyphotic deformity, it is necessary to supplement the cement vertebroplasty with transpedicular fixation of the spine

2020 ◽  
Vol 73 (4) ◽  
pp. 722-727
Author(s):  
Mykola O. Korzh ◽  
Vasyl B. Makarov ◽  
Volodymyr I. Lipovsky ◽  
Dmytro V. Morozenko ◽  
Svitlana I. Danylchenko

The aim: To study was to use mathematical modeling in assessing the stress-strain state of the bone-implant system during plate osteosynthesis with a PHILOS plate of a proximal humerus fracture with polylactic acid implants. Materials and methods: Two bone-implant systems with a three-fragment humerus fracture according to the Neer classification (type 11-C1 according to the AO / ASIF classification) were selected for the study, one of which was with additional reinforcement of the head fragment with two polylactic acid implants (PLA – polylactide Ingeo™ Biopolymer 4032D). Sawbones (Europe AB, Malmö, Sweden) built the humeral model on 3D scanning of the composite model № 3404 of the left humerus. Results: A comparative analysis of the obtained results of mathematical modeling of the stress-strain state of the bone-implant systems showed that with given constraints (hand abduction to 90°), the use of two polylactic acid implants can reduce the stress in the plate and screws, respectively, by 11% and 6% . Conclusions: The use of polylactic acid implants during osteosynthesis of three- and four-fragment fractures of the proximal humerus, especially in the case of osteoporosis, allows providing for the reinforcement of metal structures and supporting of the articular surface without deterioration of fixation rigidity.


Author(s):  
А. Г. Гребеников ◽  
И. В. Малков ◽  
В. А. Урбанович ◽  
Н. И. Москаленко ◽  
Д. С. Колодийчик

The analysis of the design and technological features of the tail boom (ТB) of a helicopter made of polymer composite materials (PCM) is carried out.Three structural and technological concepts are distinguished - semi-monocoque (reinforced metal structure), monocoque (three-layer structure) and mesh-type structure. The high weight and economic efficiency of mesh structures is shown, which allows them to be used in aerospace engineering. The physicomechanical characteristics of the network structures are estimated and their uniqueness is shown. The use of mesh structures can reduce the weight of the product by a factor of two or more.The stress-strain state (SSS) of the proposed tail boom design is determined. The analysis of methods for calculating the characteristics of the total SSS of conical mesh shells is carried out. The design of the tail boom is presented, the design diagram of the tail boom of the transport category rotorcraft is developed. A finite element model was created using the Siemens NX 7.5 system. The calculation of the stress-strain state (SSS) of the HC of the helicopter was carried out on the basis of the developed structural scheme using the Advanced Simulation module of the Siemens NX 7.5 system. The main zones of probable fatigue failure of tail booms are determined. Finite Element Analysis (FEA) provides a theoretical basis for design decisions.Shown is the effect of the type of technological process selected for the production of the tail boom on the strength of the HB structure. The stability of the characteristics of the PCM tail boom largely depends on the extent to which its design is suitable for the use of mechanized and automated production processes.A method for the manufacture of a helicopter tail boom from PCM by the automated winding method is proposed. A variant of computer modeling of the tail boom of a mesh structure made of PCM is shown.The automated winding technology can be recommended for implementation in the design of the composite tail boom of the Mi-2 and Mi-8 helicopters.


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