Effect of Anodic Behavior on Electrochemical Machining of TB6 Titanium Alloy

被引:105
|
作者
Liu, Weidong [1 ]
Ao, Sansan [1 ]
Li, Yang [1 ]
Liu, Zuming [1 ]
Zhang, Hui [1 ]
Manladan, Sunusi Marwana [2 ]
Luo, Zhen [1 ,3 ]
Wang, Zhiping [4 ]
机构
[1] Tianjin Univ, Sch Mat Sci & Engn, 31 Bldg,Room 291,Peiyang Pk Campus, Tianjin 300350, Peoples R China
[2] Univ Malaya, Dept Mech Engn, Fac Engn, Kuala Lumpur 50603, Malaysia
[3] Collaborat Innovat Ctr Adv Ship & Deep Sea Explor, Shanghai 200240, Peoples R China
[4] Civil Aviat Univ China, Sch Aviat Engn, Tianjin 300300, Peoples R China
关键词
Jet electrochemical machining; Anodic behavior; Novel simulation model; Nozzle travel rate optimization; TB6 titanium alloy; NEAR-ECM CONDITIONS; DISSOLUTION BEHAVIOR; COPPER DISSOLUTION; MASS-TRANSPORT; SURFACE; ELECTROLYTE; FILMS; IRON; MICROSTRUCTURE; STABILITY;
D O I
10.1016/j.electacta.2017.03.025
中图分类号
O646 [电化学、电解、磁化学];
学科分类号
081704 ;
摘要
Jet electrochemical machining is a promising shaping method that has the potential to replace traditional sinking ECM in the industry owing to its flexibility and stability. However, its machining quality is impaired by the occurrence of a unique phenomenon (i.e., the anode cannot be uniformly dissolved with high nozzle travel rate). This paper aims to analyze this unique phenomenon from the viewpoint of anodic behavior and to select the optimum travel rate parameter window. The anodic behavior of TB6 titanium alloy in sodium chloride solution was investigated by linear sweep voltammetry, cyclic voltammetry, electrochemical impedance spectroscopy and chronoamperometry. A time-dependent mechanism of pitting/large localized corrosion/polishing for the anodic interface structure was developed. The full electricity quantity of the equivalent oxide layer capacitor, Q, was proposed as a criterion for the initiation of uniform dissolution state. Subsequently, a novel model that incorporates the parameter Q was developed to account for the effect of anodic behavior. This model is able to predict the machined profile as well as the localized corrosion range. Finally, the effect of nozzle travel rate on jet ECM performance was investigated, and a nozzle travel rate of 10 to 25 mu m s(-1) was selected as the optimum parameter window in the present work. (C) 2017 Elsevier Ltd. All rights reserved.
引用
收藏
页码:190 / 200
页数:11
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