面向航空传动轴零件孔口倒圆数控宏程序与用户界面开发

Research on NC macro program and user interface development for hole rounding of aviation transmission shaft parts

  • 摘要: 针对航空传动轴类零件孔口倒圆特征的CAM数控编程效率不足的问题,面向西门子840D数控系统开发了专用数控宏程序及用户操作界面。选用孔口倒圆专用刀具,建立了结构特征参数化轨迹方程并完成刀路轨迹的设计,开发了多孔口倒圆数控宏程序,可实现轴类零件规律分布、任意数量的孔口倒圆加工。针对所开发的宏程序,基于 SinuTrain 软件开发了相应的用户操作界面,实现了孔口倒圆参数的可视化及特征参数量输入,提高操作便捷性与准确性。使用VERICUT软件开展数控宏程序仿真验证,并在航空制造企业传动轴类零件加工中完成应用验证。结果表明与原有孔口倒圆加工工艺相比效率提升86%,孔口倒圆轨迹规划合理、参数传递无误,可完成多规格孔口加工,加工后孔口过渡光滑、无刀痕与过切、欠切问题。本研究为传动轴类零件孔口倒圆加工工序提供了高效可靠的技术方法。

     

    Abstract: Aiming at the low efficiency of CAM-based NC programming for the hole rounding feature of aviation transmission shaft parts, a dedicated NC macro program and corresponding user interface are developed for the Siemens 840D CNC system. A specialized hole rounding tool is adopted, a parametric trajectory equation for structural features is established, and the tool path design is finalized. The developed multi-hole rounding NC macro program enables hole rounding of shaft parts with regularly distributed holes and arbitrary quantities. Based on the macro program, a matching user interface is developed using SinuTrain software, achieving the visualization and input of hole rounding parameters, thus enhancing operational convenience and accuracy. Simulation validation of the NC macro program is performed via VERICUT software, followed by application validation in the actual processing of transmission shaft parts at an aviation manufacturing enterprise. The results indicate an 86% efficiency improvement relative to the conventional hole rounding process. The hole rounding trajectory planning is rational with accurate parameter transmission, enabling multi-specification hole processing. Post-processing, the hole transitions are smooth without tool marks, overcutting, or undercutting issues. This study provides an efficient and reliable technical method for the hole rounding process of transmission shaft parts.

     

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