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Experimental modelling and optimisation of process parameters of hole drilling by electrical discharge machining of aerospace titanium alloy

机译:航空钛合金放电加工钻孔工艺参数的实验建模与优化。

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摘要

Advancement of new materials and machining technology has changed the domain and ranges both of aerospace vehicles, still a few problems of conventional as well as non-conventional machining processes is unresolved such as low material removal rate (MRR), frequent tool wear and poor surface finish, etc. In this experimental study, a new process in electrical discharge machining (EDM), termed as electrical discharge drilling (EDD is used to make the hole in titanium alloy (Ti-6Al-4V) and also used altogether a new approach of hybrid of methodologies for modelling as well as optimisation of the hole made for MRR, average surface roughness (R_a) and average circularity (C_a). The used methodology comprises of Taguchi methodology (TM) with response surface methodology (RSM) for modelling and RSM coupled with principal component analysis-based (PCA) grey relational analysis (GRA) for optimisation. The obtained results indicate that applied hybrid approaches in present study of EDD process are reasonable and substantiates with facts of improvement in MRR by 30.80%, R_a by 24.81% and C_a by 26.09%.
机译:新材料和机械加工技术的进步改变了航天飞行器的领域和范围,仍然解决了常规和非常规加工过程中的一些问题,例如材料去除率(MRR)低,频繁的工具磨损和不良的表面在本实验研究中,放电加工(EDM)的一种新工艺被称为放电钻孔(EDD用于在钛合金(Ti-6Al-4V)上打孔),并且还一起使用了一种新方法建模方法的混合以及对MRR,平均表面粗糙度(R_a)和平均圆度(C_a)进行的孔的优化。使用的方法包括Taguchi方法(TM)和响应表面方法(RSM)用于建模和RSM结合基于主成分分析(PCA)的灰色关联分析(GRA)进行优化,获得的结果表明,目前在EDD工艺研究中采用的混合方法合理并证实了MRR改善了30.80%,R_a改善了24.81%,C_a改善了26.09%的事实。

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