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Design of the cross-structural cathodes in electrochemical machining of aero-engine blades

机译:航空发动机叶片电化学加工中的交叉结构阴极设计

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摘要

Blades are crucial parts of aero-engines. Their manufacturing is difficult because of their thinness, complex profile and stringent requirements. Electrochemical machining (ECM) is an important approach for manufacturing blades, but it is difficult to machine the leading and trailing edges. This article adopts cross-structural cathodes in ECM to solve the open electric field space problem. The key difficulty in the design of cross-structural cathodes is the position of the crossed-point. The height and the offset of the crossed-point are optimized using the ANSYS software. The simulation results show that the position of the crossed-point obviously affects the machining accuracy, along the leading and trailing edges of the blade. A pair of cross-structural cathodes with one uniform section is designed, and a series of corresponding ECM experiments are carried out. The experiments demonstrate that the ECM process is stable, the profiles are sleek and the machining dimensional error is reduced to 0.08 mm at the leading and trailing edges of the blade when using the new cathode structure.
机译:刀片是航空发动机的关键部分。由于它们的薄弱,复杂的概况和严格的要求,他们的制造很困难。电化学加工(ECM)是制造刀片的重要方法,但是难以将领先和后缘和拖曳边缘加工。本文采用ECM中的交叉结构阴极来解决开放式电场空间问题。交叉结构阴极设计的关键难度是交叉点的位置。交叉点的高度和偏移是使用ANSYS软件进行优化的。仿真结果表明,交叉点的位置明显影响加工精度,沿着叶片的前缘和后缘。设计了一对具有一个均匀部分的交叉结构阴极,并进行一系列相应的ECM实验。实验表明,ECM工艺稳定,在使用新的阴极结构时,曲线是时尚的,并且加工尺寸误差在刀片的前缘和后缘处减小到0.08mm。

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