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Cathode Design of Aero-engine Blades in Electrochemical Machining Based on Characteristics of Electric and Electrolyte Flow Field

机译:基于电化学和电解质流场特性的电化学加工中的航空发动机叶片的阴极设计

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The procedure for cathode design in electrochemical machining (ECM) is plagued by limited applicability, inaccuracy, and nonconvergence. So cathode design is a difficult problem must be faced and solved in ECM. We develop a new numerical approach for cathode design by employing a finite element method and this approach has been applied in the cathode design of aero-engine blades in ECM. The mathematic models of the electric filed and electrolyte flow filed distribution in EMC process are described primarily. Then the realization procedure of this approach is presented, in which the effects of electric filed and electrolyte flow filed distribution within the inter-electrode gap domain are concentrated. In order to verify the machining accuracy of the designed cathodes, the experiments are conducted using an industrial scale electrochemical machining system. The experimental results demonstrate that the machined blade have high surface quality and dimensional accuracy which proves the proposed approach for cathode design of aero-engine blades in ECM is applicable and valuable.
机译:电化学加工(ECM)中的阴极设计的步骤通过有限的适用性,不准确和非熔化来困扰。因此,阴极设计是一个难题,必须面对和解决ECM。我们通过采用有限元方法开发一种新的数值方法,采用有限元方法,并且这种方法已经应用于ECM中航空发动机叶片的阴极设计。主要描述了EMC工艺中电解电流和电解质流动分布的数学模型。然后提出了这种方法的实现过程,其中浓缩了电极孔和电解质流量的效果的效应。为了验证设计的阴极的加工精度,使用工业尺度电化学加工系统进行实验。实验结果表明,加工刀片具有高表面质量和尺寸精度,证明了ECM中的航空发动机叶片的阴极设计的建议方法是适用的和有价值的。

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