2022
DOI: 10.1155/2022/7976691
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Web Optimization of Compression Ignition Aviation Engine Crankshaft

Abstract: The focus of this study was the weight reduction of crankshaft web regions of an inline 4 cylinder, 250 HP compression ignition engine with a combustion chamber volume of 2499 cm3 intended for use in aircraft. Iteration #0 model was generated by manual reduction of a reference model. According to the results of the analyses, the stresses were compared. Since the increase in stress values of weight reduced model over the reference model exceeded the targeted upper limit of 15.0%, three geometric parameters have… Show more

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Cited by 3 publications
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