SASTech - Technical Journal of RUAS

  • Year: 2011
  • Volume: 10
  • Issue: 1

Design of connecting rod for heavy duty applications produced by different processes for enhanced fatigue life

  • Author:
  • Tony George Thomas1, S. Srikari2, M. L. J Suman3
  • Total Page Count: 7
  • DOI:
  • Page Number: 1 to 7

1M. Sc.[Engg.] Student, Department of AAE, M.S. Ramaiah School of Advanced Studies, Bangalore, 560 058

2Professor, Department of AAE, M.S. Ramaiah School of Advanced Studies, Bangalore, 560 058

3Senior Lecturer, Department of MME, M.S. Ramaiah School of Advanced Studies, Bangalore, 560 058

Abstract

The connecting rod forms an integral part of an internal combustion engine. The connecting rod is acted upon by different types of loads while undergoing its operation. One of the main reasons contributing to its failure is fatigue. The aim of this study is to redesign the connecting rod by incorporating the manufacturing process effects into the analysis and obtain a better fatigue performance. The redesign is aimed at reducing the weight of the component.

Heavy duty application's connecting rod was selected for the study. The analytically calculated loads acting on the small end of connecting rod were used to carry out the static analysis using ANSYS. A stress concentration was observed near the transition between small end and shank. A piston-crank-connecting rod assembly was simulated for one complete cycle (0.02 seconds) using ADAMS to obtain the loads acting on small end of connecting rod. This force vs. time graph was converted into an equivalent stress vs. time graph. This stress vs. time graph was used as loading graph for fe-safe. The fatigue life calculated using fe-safe is 6.94×106 cycles and these results are validated with the help of Palmgren-Miner linear damage rule.

The fatigue life of connecting rod can be further enhanced by incorporating manufacturing process effects in the analysis stage. Fatigue life was estimated by incorporating the shot peening process effects. An in-plane residual stress for the selected surface elements were applied for obtaining the beneficial effect of shot peening. There was an increment of 72% in fatigue life cycles). We concude that shot peening can significantly increase the fatigue life of a connecting rod component

Keywords

Fatigue Analysis, Compressive Residual Stress, Shot Peening, Surface Cracks