A Thermo-Structural Analysis of Die-Sinking Electrical Discharge Machining (EDM) of a Haynes-25 Super Alloy Using Deep-Learning-Based Methodologies

Author:

Aneesh T.1ORCID,Mohanty Chinmaya Prasad1,Tripathy Asis Kumar2,Chauhan Alok Singh3ORCID,Gupta Manoj4ORCID,Annamalai A. Raja5ORCID

Affiliation:

1. School of Mechanical Engineering, Vellore Institute of Technology, Vellore 632014, India

2. School of Computer Science Engineering and Information System, Vellore Institute of Technology, Vellore 632014, India

3. Defence Metallurgical Research Laboratory, Defence Research and Development Organisation, Hyderabad 500058, India

4. Department of Mechanical Engineering, National University of Singapore, Singapore 119077, Singapore

5. Centre for Innovative Manufacturing Research, Vellore Institute of Technology, Vellore 632014, India

Abstract

The most effective and cutting-edge method for achieving a 0.004 mm precision on a typical material is to employ die-sinking electrical discharge machining (EDM). The material removal rate (MRR), tool wear rate (TWR), residual stresses, and crater depth were analyzed in the current study in an effort to increase the productivity and comprehension of the die-sinking EDM process. A parametric design was employed to construct a two-dimensional model, and the accuracy of the findings was verified by comparing them to prior research. Experiments were conducted utilizing the EDM machine, and the outcomes were assessed in relation to numerical simulations of the MRR and TWR. A significant temperature disparity that arises among different sections of the workpiece may result in the formation of residual strains throughout. As a consequence, a structural model was developed in order to examine the impacts of various stress responses. The primary innovations of this paper are its parametric investigation of residual stresses and its use of Haynes 25, a workpiece material that has received limited attention despite its numerous benefits and variety of applications. In order to accurately forecast the output parameters, a deep neural network model, more precisely, a multilayer perceptron (MLP) regressor, was utilized. In order to improve the precision of the outcomes and guarantee stability during convergence, the L-BFGS solver, an adaptive learning rate, and the Rectified Linear Unit (ReLU) activation function were integrated. Extensive parametric studies allowed us to determine the connection between key inputs, including the discharge current, voltage, and spark-on time, and the output parameters, namely, the MRR, TWR, and crater depth.

Funder

Aeronautics Research and Development Board, Defense Research and Development Organization, Government of India

Publisher

MDPI AG

Subject

Industrial and Manufacturing Engineering,Mechanical Engineering,Mechanics of Materials

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