Machining of a film-cooling hole in a single-crystal superalloy by high-speed electrochemical discharge drilling
Machining of a film-cooling hole in a single-crystal superalloy by high-speed electrochemical discharge drilling
复制标题
高速电化学放电钻孔单晶高温合金气膜冷却孔加工
DOI:
10.1016/j.cja.2015.06.021
复制
发表时间:
2016-04-01
影响因子:
5.7
通讯作者:
Zhu Di
中科院分区:
文献类型:
--
作者:
Zhang Yan;Xu Zhengyang;Zhu Di
Single-crystal superalloys are typical advanced materials used for manufacturing aeroengine turbine blades. Their unique characteristics of high hardness and strength make them exceedingly difficult to machine. However, a key structure of a turbine blade, the film-cooling hole, needs to be machined in a single-crystal superalloy; such machining is challenging, especially considering the increasing levels of machining efficiency and quality demanded by the aeroengine industry. Tube electrode high-speed electrochemical discharge drilling (TSECDD), a hybrid technique of high-speed electrical discharge drilling and electrochemical machining, provides high machining efficiency and accuracy, as well as eliminating the recast layer. In this study, TSECDD is used to machine a film-cooling hole in a nickel-based single-crystal superalloy (DD6). The Taguchi methods of experiment are used to optimise the machining parameters. Experimental results show that TSECDD can effectively drill the film-cooling hole; the optimum parameters that give the best performance are as follows: pulse duration: 12 mu s, pulse interval: 30 mu s, peak current: 6 A, and salt solution conductivity: 3 mS/cm. Finally, a hole is machined by TSECDD, and the results are compared with those obtained by electrical discharge machining. TSECDD is found to be promising for improving the surface quality and eliminating the recast layer. (C) 2015 The Authors. Production and hosting by Elsevier Ltd. on behalf of CSAA & BUAA.