Articles
  • Investigation of sparking electro discharge machining for fabricating silicon carbide reinforced Al7050 alloy-based composite through stir casting
  • B.R. Senthil Kumara,*, R. Sivakumarb, M. Chrispin Dasc and V. Muthuramand

  • aProfessor, Department of Aeronautical Engineering, Nehru Institute of Engineering and Technology, Coimbatore, 641105
    bProfessor, Department of Civil Engineering, E.G.S. Pillay Engineering College, Nagapattinam 611002, Tamilnadu, India
    cAssociate Professor, Department of Mechanical Engineering, St. Joseph’s Institute of Technology, OMR, Chennai
    dProfessor, Department of Mechanical Engineering, Vels Institute of Science, Technology and Advanced Studies (VISTAS), Chennai

  • This article is an open access article distributed under the terms of the Creative Commons Attribution Non-Commercial License (http://creativecommons.org/licenses/by-nc/4.0) which permits unrestricted non-commercial use, distribution, and reproduction in any medium, provided the original work is properly cited.

Abstract

This research investigates the application of spark electro-discharge machining for fabricating a stir-cast composite reinforced with silicon carbide, based on the Al7050 alloy. Employing a response surface methodology with a central composite design, the study explores 20 combinations of control parameters to investigate their collective influence. Specifically, it focuses on understanding how three key machining parameters—current, pulse-on time, and pulse-off time—affect material removal rates, electrode wear, and surface roughness. A novel teaching-learning-based optimization strategy, integrating response surface methodology with grey relational analysis, is utilized to optimize multiple responses. The optimized parameters derived through response surface methodology are a current of 10 amps, a pulse-on time of 6 µsec, and a pulse-off time of 5 µsec, resulting in significant improvements. These optimized settings correspond to material removal rates, electrode wear rates, and surface roughness values of 0.01074 g/min, 0.0040 g/min, and 4.9395 µm, respectively. Additionally, the teaching-learning-based optimization method employs grey relational analysis initially to rank the input factors. With the optimized process variables obtained using GRA-TLBO—8.48 amps for current, 6.22 µsec for pulse-on time, and 3.34 µsec for pulse-off time—the material removal rate, electrode wear rate, and surface roughness are further enhanced to 0.01159 g/min, 0.00408 g/min, and 3.7202 µm, respectively


Keywords: Al7050, Ceramics processing, RSM, MCDM, GRA-TLBO.

This Article

  • 2025; 26(2): 323-341

    Published on Apr 30, 2025

  • 10.36410/jcpr.2025.26.2.323
  • Received on Mar 25, 2024
  • Revised on Jun 22, 2024
  • Accepted on Jul 4, 2024

Correspondence to

  • B.R. Senthil Kumar
  • Professor, Department of Aeronautical Engineering, Nehru Institute of Engineering and Technology, Coimbatore, 641105
    Tel : 9345451066 Fax: 9345451066

  • E-mail: senthilramanseetha60@gmail.com