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Predictive Modeling for Tool Deflection and Part Distortion of Large Machined Components

机译:大型加工零件的刀具变形和零件变形的预测模型

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Machined monolithic components provide the foundation for modern aircraft structures requiring high performance designs in terms of weight, strength, and fatigue properties. Part distortions arising from machining-induced stresses and tool deflection resulting from high dynamic cutting forces frustrate manufacturing and assembly processes, necessitating expensive in-process and post-machining corrective measures aimed at eliminating their effects. Component weight and cost requirements are often compromised by adding thicker component section designs or off-machine part flipping processes as a distortion control mechanism. Similarly, small depths of cut are taken to minimize cutting forces and tool deflection. Additional spring passes are also taken to eliminate any undercut errors introduced by unanticipated deflection and distortion problems. The ability to accurately predict and minimize tool deflections and part distortion via simulations can significantly reduce manufacturing and assembly costs. This paper presents physics-based models for predicting tool deflection and part distortions by considering the appropriate physics for each problem. Dynamic cutting forces predicted by physics-based machining models, and tool compliance properties are incorporated into a detailed linear elastic deflection model in order to predict in-process deflections along a computer numerical control (CNC) machining toolpath. Similarly, bulk stress state and machining-induced stresses for large, monolithic part machining are taken into account for predicting part distortions. Sources of stresses may include heat treatment, quenching, forging, and machining operations. Bulk stress data from heat treatment predictive models can also be imported and mapped onto the workpiece finite element model. CNC part programs, along with stresses arising from corresponding tooling, are processed and analyzed. Results of a validation study for workpiece distortion predictions are presented for a number of monolithic, thin-walled components. Predictions for tool deflection are also compared against experimental measurements for multiple cutting configurations and tool diameters. Good correlation is found between predictions and measurements of deflection.
机译:机加工的整体组件为现代飞机结构奠定了基础,这些飞机结构在重量,强度和疲劳性能方面需要高性能设计。由于高动态切削力导致的由加工引起的应力和刀具偏斜引起的零件变形使制造和组装过程受挫,因此需要采取昂贵的过程中和机加工后纠正措施来消除其影响。零件重量和成本要求通常会因添加较厚的零件截面设计或机器外零件翻转过程作为变形控制机制而受到损害。同样,采用较小的切削深度以最小化切削力和刀具偏斜。还采取了附加的弹簧行程,以消除由于意外的偏斜和变形问题而引起的任何咬边误差。通过仿真准确预测和最小化工具变形和零件变形的能力可以大大降低制造和组装成本。本文提出了基于物理学的模型,通过考虑每个问题的适当物理学来预测工具的变形和零件变形。通过基于物理的加工模型预测的动态切削力以及刀具的柔顺特性被合并到详细的线性弹性挠度模型中,以便预测沿计算机数控(CNC)加工刀具路径的加工中挠度。同样,在预测零件变形时,会考虑大块整体零件加工的整体应力状态和加工引起的应力。应力来源可能包括热处理,淬火,锻造和机加工操作。来自热处理预测模型的整体应力数据也可以导入并映射到工件有限元模型上。将对CNC零件程序以及相应工具产生的应力进行处理和分析。给出了许多整体式薄壁部件的工件变形预测验证研究的结果。还将针对多种切削配置和刀具直径将刀具变形的预测与实验测量值进行比较。在变形的预测和测量之间发现良好的相关性。

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