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The Accuracy of Finishing WEDM of Inconel 718 Turbine Disc Fir Tree Slots

机译:inconel 718涡轮盘枞树插槽的精确度

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摘要

Servicing aircraft engines sometimes requires manufacturing only a single piece of a given part. Manufacturing a turbine disc using traditional methods is uneconomical. It is necessary to use a different machining method recommended for small lot production. One of the proposed methods is WEDM (wire electrical discharge machining). The article presents the results of the research on finishing WEDM of Inconel 718 turbine disc fir tree slots. The influence of infeed, mean gap voltage, peak current, pulse off-time, and discharge energy on the shape accuracy, surface roughness, microcracks, and the white layer thickness were determined. Mathematical models were developed based on the DoE (Design of Experiment) analysis. The statistical significance of the models was verified with the ANOVA (Analysis of Variance) test. The machining parameters control methods that allow achieving the required shape accuracy, surface roughness, and surface layer condition were presented. The obtained surface roughness was Ra = 0.84 μm, the shape accuracy of the slot in the normal-to-feed direction was Δd = 0.009 μm, the profile shape accuracy was Δr = 0.033 μm, and the thickness of recast (white) layer was approximately 5 μm.
机译:维修飞机发动机有时需要制造一件给定部分。使用传统方法制造涡轮盘是不经济的。有必要使用推荐用于小型批量生产的不同加工方法。其中一个提出的方法是WEDM(导线电气放电加工)。本文介绍了Inconel 718涡轮盘枞树槽的整理WEDM研究的结果。确定进给,平均间隙电压,峰值电流,脉冲关闭时间和放电能量对形状精度,表面粗糙度,微裂纹和白色层厚度的影响。基于DOE(实验设计)分析开发了数学模型。通过ANOVA(方差分析)测试验证了模型的统计学意义。提出了允许实现所需形状精度,表面粗糙度和表面层条件的加工参数控制方法。所获得的表面粗糙度是Ra =0.84μm,在常向进给方向上的槽的形状精度为ΔD=0.009μm,轮廓形状精度为ΔR=0.033μm,并且重量(白色)层的厚度是大约5μm。

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