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Predictive modeling for tool deflection and part distortion of large machined components

机译:大型加工组件刀具偏转的预测模型和零件失真

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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:机加工单片组件为现代飞机结构提供了在重量,强度和疲劳性能方面需要高性能设计的现代飞机结构的基础。由加工诱导的应力和工具偏转产生的部分扭曲引起的高动态切割力令人沮丧的制造和装配过程,需要昂贵的过程和旨在消除它们的效果的昂贵的校正措施。组件重量和成本要求通常通过添加较厚的部件部分设计或卸载器件翻转过程作为失真控制机构来损害。类似地,采取小的切割深度以最小化切割力和刀具偏转。还考虑了额外的弹簧通行证来消除由意外偏转和失真问题引入的任何削减误差。通过模拟准确地预测和最小化刀具偏转和部分失真的能力可以显着降低制造和组装成本。本文介绍了基于物理的模型,用于通过考虑每个问题的适当物理来预测刀具偏转和部分失真。由基于物理的加工模型预测的动态切割力,刀具合规性地被纳入详细的线性弹性偏转模型,以预测沿着计算机数控(CNC)加工刀具路径的过程内偏转。类似地,考虑到用于预测部分扭曲的大型整体机加工的体积应力状态和加工诱导的应力。应力源可包括热处理,淬火,锻造和加工操作。来自热处理预测模型的批量应力数据也可以进口并映射到工件有限元模型上。 CNC部件程序以及相应工具产生的应力,并进行分析并分析。对于许多单片,薄壁部件,介绍了工件失真预测的验证研究的结果。还与多种切割配置和刀具直径的实验测量比较了对刀具偏转的预测。在预测和偏转测量之间发现了良好的相关性。

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