Structural Analysis of Compressor Blades for Turbocharger by Using the Different Materials

Authors

  • Ni Ni Hlaing
  • Htay Htay Win
  • Myint Thein
  • Aung Ko Latt

DOI:

https://doi.org/10.31695/IJASRE.2019.33643

Keywords:

Compressor Blades, Effective Strain, Total Deformation, Turbocharger, Stress Analysis, Material

Abstract

A structural analysis has been carried out to investigate the Von-Mises stresses, effective strains and total deformation of the
compressor blades of the turbocharger in locomotive diesel engines. An investigation in the usage of new materials is required. In
this research, compressor blades are designed with three different materials. The modeling of the compressor is drawn by using
SolidWorks (2016) software and analysis is done in ANSYS (17.0). The design speed of the compressor is considered 68,000 rpm.
An attempt is also made to suggest the suitable material for the compressor blades of a turbocharger by comparing the results
obtained for three different materials (Aluminum Alloy (7050-T7651), AISI 4340 Steel and Inconel Alloy (718)) for the compressor. The Aluminum Alloy (7050-T7651) for the compressor blades of a turbocharger is recommended on the suitable results than the other two materials

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How to Cite

Ni Ni Hlaing, Htay Htay Win, Myint Thein, & Aung Ko Latt. (2019). Structural Analysis of Compressor Blades for Turbocharger by Using the Different Materials. International Journal of Advances in Scientific Research and Engineering (IJASRE), ISSN:2454-8006, DOI: 10.31695/IJASRE, 5(12), 94–104. https://doi.org/10.31695/IJASRE.2019.33643

Issue

Vol. 5 No. 12 (2019): Volume 5 Issue 12 Dec (2019)

Section

Articles

License

Copyright (c) 2019 Ni Ni Hlaing, Htay Htay Win, Myint Thein, Aung Ko Latt

Creative Commons License

This work is licensed under a Creative Commons Attribution-NonCommercial 4.0 International License.