Alilakbari, K., Imanparast, M., Masoudi Nejad, R. (2018). Microstructure and fatigue fracture mechanism for a heavy-duty truck diesel engine crankshaft. Scientia Iranica, (), -. doi: 10.24200/sci.2018.50964.1939
Karim Alilakbari; Mohammad Imanparast; Reza Masoudi Nejad. "Microstructure and fatigue fracture mechanism for a heavy-duty truck diesel engine crankshaft". Scientia Iranica, , , 2018, -. doi: 10.24200/sci.2018.50964.1939
Alilakbari, K., Imanparast, M., Masoudi Nejad, R. (2018). 'Microstructure and fatigue fracture mechanism for a heavy-duty truck diesel engine crankshaft', Scientia Iranica, (), pp. -. doi: 10.24200/sci.2018.50964.1939
Alilakbari, K., Imanparast, M., Masoudi Nejad, R. Microstructure and fatigue fracture mechanism for a heavy-duty truck diesel engine crankshaft. Scientia Iranica, 2018; (): -. doi: 10.24200/sci.2018.50964.1939
Microstructure and fatigue fracture mechanism for a heavy-duty truck diesel engine crankshaft
1Department of Mechanical Engineering, Faculty of Montazeri, Khorasan Razavi Branch, Technical and Vocational University (TVU), Mashhad, Iran
2Department of Mechanical Engineering, University of Sistan and Baluchestan, Zahedan, Iran
3Department of Mechanical Engineering, Foolad Institute of Technology, Fooladshahr, Isfahan, 84916-63763, Iran
Abstract
The main goal of this research is the experimental and numerical study on the fatigue function and failure of the crankshaft of diesel engine of a heavy truck. To do this, a crankshaft of the diesel engine of a heavy truck that has gone under failure after traveling 955000 km, has been used. To examine the sources of this failure, several experimental studies have been carried out including chemical composition, the strength of the material, determining the hardness and the microstructure of the material. Besides, using an elastic–plastic three dimensional finite element method (FEM) model, the location of the maximum stress in the crankshaft was determined using the ‘‘complete crankshaft model’’ and ‘‘one crank model’’. Using the results of stress analysis, was a basis for the three-dimensional crack growth model and fatigue life estimation to determine the stress intensity factor and fatigue life considering the related parameters and boundary conditions method. At the final stage, using the results gotten from the given model for the fatigue crack growth, comparing it with experimental results, and examining the whole process, it was concluded that the scratches in crankpin region, was the main reason for the fatigue failure got from bending-torsional load-combination.
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