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Experimental research on the belt grinding technology for the real-R edge of the aero-engine precision-forging blade

机译:航空发动机精密锻造叶片real-R边缘砂带磨削技术的实验研究

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摘要

Because of the special characteristics of aero-engine precision-forging blade edge, the edge profile shape errors are easily caused by using conventional processing methods. The purpose of this research is to improve real-R profile shape errors and also exploring the belt grinding mechanism for the high-strength materials. Firstly, the grinding characteristics and process planning to the blade real-R edge are analysed. And then, the methodology of EBG with CBN belt is illustrated, at the same time, the control equation for EBG is established. Finally, the method of EBG with CBN belt is analysed by the experiment investigated to the aero-engine precision-forging blade, comparing to the method of hand. The experimental results show that the real-R profile shape errors ≤ ± 0.07 mm, and the real-R shape smoothing, profile clear and the inter sectional surface smooth transition. It is verified that the method of EBG is better than the conventional method.
机译:由于航空发动机精密锻造叶片边缘的特殊特性,使用常规加工方法很容易造成边缘轮廓形状误差。这项研究的目的是改善real-R型材的形状误差,并探索高强度材料的砂带磨削机理。首先,分析了磨削特性和对刀片real-R边缘的工艺计划。然后,阐述了带CBN带的EBG的方法,同时建立了EBG的控制方程。最后,通过对航空发动机精密锻造叶片进行的实验研究,与手工方法进行比较,分析了带CBN皮带的EBG方法。实验结果表明,R实轮廓形状误差≤±0.07 mm,且R实形状平滑,轮廓清晰且截面表面平滑过渡。证明了EBG方法优于常规方法。

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