Numerical Simulation of Fatigue Crack Growth in Titanium Alloy Orthopaedic Plates
Filip Vučetić*
orcid.org/0000-0002-7194-4880
; Innovation Center of Faculty of Mechanical Engineering, Belgrade, Kraljice Marije 16, 11120 Belgrade, Republic of Serbia
Katarina Čolić
; Innovation Center of Faculty of Mechanical Engineering, Belgrade, Kraljice Marije 16, 11120 Belgrade, Republic of Serbia
Aleksandar Grbović
; University of Belgrade, Faculty of Mechanical Engineering, Kraljice Marije 16, 11120 Belgrade, Republic of Serbia
Ana Petrović
; University of Belgrade, Faculty of Mechanical Engineering, Kraljice Marije 16, 11120 Belgrade, Republic of Serbia
Aleksandar Sedmak
; University of Belgrade, Faculty of Mechanical Engineering, Kraljice Marije 16, 11120 Belgrade, Republic of Serbia
Dražan Kozak
; Mechanical Engineering Faculty in Slavonski Brod, University of Slavonski Brod, Trg Ivane Brlic Mazuranic 2, HR-35000 Slavonski Brod, Croatia
Simon Sedmak
; Innovation Center of Faculty of Mechanical Engineering, Belgrade, Kraljice Marije 16, 11120 Belgrade, Republic of Serbia
APA 6th Edition Vučetić*, F., Čolić, K., Grbović, A., Petrović, A., Sedmak, A., Kozak, D. i Sedmak, S. (2020). Numerical Simulation of Fatigue Crack Growth in Titanium Alloy Orthopaedic Plates. Tehnički vjesnik, 27 (6), 1917-1922. https://doi.org/10.17559/TV-20200617192027
MLA 8th Edition Vučetić*, Filip, et al. "Numerical Simulation of Fatigue Crack Growth in Titanium Alloy Orthopaedic Plates." Tehnički vjesnik, vol. 27, br. 6, 2020, str. 1917-1922. https://doi.org/10.17559/TV-20200617192027. Citirano 18.01.2021.
Chicago 17th Edition Vučetić*, Filip, Katarina Čolić, Aleksandar Grbović, Ana Petrović, Aleksandar Sedmak, Dražan Kozak i Simon Sedmak. "Numerical Simulation of Fatigue Crack Growth in Titanium Alloy Orthopaedic Plates." Tehnički vjesnik 27, br. 6 (2020): 1917-1922. https://doi.org/10.17559/TV-20200617192027
Harvard Vučetić*, F., et al. (2020). 'Numerical Simulation of Fatigue Crack Growth in Titanium Alloy Orthopaedic Plates', Tehnički vjesnik, 27(6), str. 1917-1922. https://doi.org/10.17559/TV-20200617192027
Vancouver Vučetić* F, Čolić K, Grbović A, Petrović A, Sedmak A, Kozak D i sur. Numerical Simulation of Fatigue Crack Growth in Titanium Alloy Orthopaedic Plates. Tehnički vjesnik [Internet]. 2020 [pristupljeno 18.01.2021.];27(6):1917-1922. https://doi.org/10.17559/TV-20200617192027
IEEE F. Vučetić*, et al., "Numerical Simulation of Fatigue Crack Growth in Titanium Alloy Orthopaedic Plates", Tehnički vjesnik, vol.27, br. 6, str. 1917-1922, 2020. [Online]. https://doi.org/10.17559/TV-20200617192027
Sažetak Biomaterials intended for orthopaedic plates manufacturing have much higher mechanical properties relative to the bone itself and still there are many cases where those plates fracture in service, with fatigue as the main failure mode. This causes problem with the healing process and requires that the patient undergoes another surgery. Experience and knowledge of the orthopaedic surgeon is one of the most important factors contributing to the frequency of fatigue failures. If incorrectly implanted, plates will be subjected to overloading from the start, which is convenient for crack initiation. One of the most commonly used biocompatible materials for internal bone fixation is α + β titanium alloy Ti-6Al-4V. Focus of this study was to simulate the behaviour of titanium alloy orthopaedic plates in the presence of cracks under four-point bending. The extended finite element method (XFEM) in ANSYS was employed for this purpose. Loads correspond to the ones occurring in human tibia during gait cycle for different body weights. Experimental investigation of tensile and fracture mechanics parameters of Ti-6Al-4V alloy was conducted on tensile testing machine and fractomate. Numerical simulation established the optimal geometry from remaining life point of view, indicating large differences between different geometries. Results also have shown that the remaining life of orthopaedic plates is strongly dependant on patient's body weight (load) and that the relative differences in remaining life between compared plate geometries stay the same under different loads. Influence of corrosive environment of the human body was not taken into consideration.