An experimental investigation on surface integrity and wire wear in rough and trim cut modes of WEDM for hybrid composite

IF 1.2 4区 工程技术 Q3 ENGINEERING, AEROSPACE
Nilesh Kumar, Jatinder Kumar
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Abstract

Purpose

The purpose of this paper is to investigate the surface integrity features, including surface roughness (SR), recast layer (RL), material migration, topography and wire wear pattern in rough and trim-cut wire electric discharge machine (WEDM) of hybrid composite (Al6061-90%/SiC-2.5%/TiB2-7.5%).

Design/methodology/approach

Effects of four important factors, namely, rough-cut history (RCH), pulse on time (Ton), peak current (IP) and wire offset (WO) have been assessed on the responses of interest for trim-cut WEDM. Box–Behnken design (RSM) was used to formulate the experimentation plan. Quantitative indices of surface integrity, namely, SR and RL, and selected samples have been investigated for qualitative analysis, namely, surface topography, material migration and wire wear pattern.

Findings

Ton and IP are found to be most significant, whereas RCH and WO are found insignificant for SR. Ton and WO were found to be the most significant factors affecting RL. After trim cut, an RL of thickness 8.26 µm is observed if the initial rough cut has been accomplished at high discharge energy setting. Whereas the best value of RL thickness, i.e. 5.36 µm, can be realized with low level of RCH. A significant decrease in the presence of foreign materials is recorded, indicating its strong correlation with the discharge energy used during machining.

Originality/value

Investigation on surface integrity features for machining of hybrid composite through rough and trim-cut WEDM has been reported by only a limited number of researchers in the past. This study is attempted at fulfilling few vital gaps by addressing the issues such as evaluation of the efficacy of trim cutting under different discharge energy conditions (using RCH), analysis of wire wear pattern in both rough and trim-cut modes and investigation of the wire breakage phenomenon during machining.

混合复合材料线切割机床粗加工和精加工模式下表面完整性和线材磨损的实验研究
本文旨在研究混合复合材料 (Al6061-90%/SiC-2. 5%/TiB2-7.5%) 在线切割放电加工 (WEDM) 中的表面完整性特征,包括表面粗糙度 (SR)、再铸层 (RL)、材料迁移、形貌和线材磨损模式。设计/方法/途径评估了四个重要因素,即粗切历史 (RCH)、脉冲开启时间 (Ton)、峰值电流 (IP) 和线偏移 (WO) 对微切线切割放电加工机相关响应的影响。实验计划采用盒式贝肯设计(RSM)。对表面完整性的定量指标,即 SR 和 RL,以及选定样品的定性分析,即表面形貌、材料迁移和线材磨损模式进行了调查。吨和 WO 是对 RL 影响最大的因素。如果最初的粗切割是在高放电能量设置下完成的,那么切边后观察到的 RL 厚度为 8.26 µm。而 RCH 水平较低时,RL 厚度的最佳值为 5.36 µm。过去,只有少数研究人员报道过通过粗加工和微切削线切割加工混合复合材料的表面完整性特征。本研究试图通过解决以下问题来填补一些重要空白:在不同放电能量条件下(使用 RCH)评估切边效率、分析粗加工和切边模式下的金属丝磨损模式以及调查加工过程中的金属丝断裂现象。
本文章由计算机程序翻译,如有差异,请以英文原文为准。
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来源期刊
Aircraft Engineering and Aerospace Technology
Aircraft Engineering and Aerospace Technology 工程技术-工程:宇航
CiteScore
3.20
自引率
13.30%
发文量
168
审稿时长
8 months
期刊介绍: Aircraft Engineering and Aerospace Technology provides a broad coverage of the materials and techniques employed in the aircraft and aerospace industry. Its international perspectives allow readers to keep up to date with current thinking and developments in critical areas such as coping with increasingly overcrowded airways, the development of new materials, recent breakthroughs in navigation technology - and more.
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