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A rapid and intelligent approach to design forming shape model for precise manufacturing of flanged part

机译:一种快速智能化的设计形状模型,用于精确制造法兰零件

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Adjusting the part shape with complex flanges to compensate springback deformation is key to forming shape design for manufacturing rapidly and precisely. Classical forming shape design by displacement adjustment (DA) method using finite element (FE) simulation is usually time-consuming and not accurate enough for complex surface part in industrial application. In this paper, the forming shape is modeled by changing the relations of geometric features of part model with the new flange control surfaces directly. Control surface processing (CSP) method is presented including control surface trimming, cross section division, springback compensation, and extending to design forming shape model of doubly curved flange part with joggles rapidly. The algorithms of cross section curves division of control surfaces and subsequent subdivision of each curve with circular arc and line segments are proposed. A case-based reasoning (CBR) technique and gray relation analysis (GRA) are used to support the intelligent springback prediction of each bending segment of the cross section curve. The geometric data of control surface is expressed in XML format to realize the integration of the CAD-based tools of control surface division and compensation with the Web-based springback prediction system. The approach is demonstrated on an industrial aircraft wing rib part. The forming shape model could be designed rapidly by comparison with DA method. The part shape deviations of flange angle (-0.465 degrees similar to 0.528 degrees) and surface position (-0.3 mm similar to 0.3 mm) were detected by comparing the desired geometry with the actual digital formed part shape, and the results indicate that the approach can achieve the industrial part manufacturing rapidly and precisely.
机译:用复杂的凸缘调节部件形状以补偿回弹变形是形成迅速且精确地制造形状设计的关键。通过位移调节(DA)方法使用有限元(Fe)模拟的古典成型形状设计通常是耗时的,并且对于工业应用中的复杂表面部分而言不够准确。在本文中,通过直接改变与新的法兰控制表面的部分模型的几何特征的关系来建模成形形状。提出了控制表面处理(CSP)方法,包括控制表面修剪,横截面分割,回光补偿,并延伸到迅速慢速设计双弯曲法兰部分的形状模型。提出了一种横截面曲线曲线划分控制表面的分割和随后具有圆弧和线段的每个曲线的子段。基于案例的推理(CBR)技术和灰色关系分析(GRA)用于支持横截面曲线的每个弯曲段的智能回调预测。控制表面的几何数据以XML格式表示,实现基于CAD的控制表面划分的工具和利用基于Web的回弹预测系统的补偿的集成。该方法在工业飞机翼肋骨部分上证明。通过与DA方法比较,可以快速设计成形形状模型。通过将所需的几何形状与实际数字形成部分形状进行比较,检测法兰角(类似于0.528度的-0.465度,类似于0.528度)和表面位置(类似于0.3mm)的部分形状偏差,并且结果表明该方法可以快速且精确地实现工业部件制造。

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