共查询到18条相似文献,搜索用时 187 毫秒
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基于快速回弹补偿的橡皮囊液压成形模面设计方法 总被引:3,自引:1,他引:3
橡皮囊液压成形工艺(简称"橡皮成形")是航空钣金成形的主要方法之一,而回弹是影响其产品制造精度的主要缺陷.回弹补偿技术可有效地消除钣金件回弹误差,但其依赖的数值模拟耗时极长,目前不易于大范围推广.提出一种考虑回弹误差修正的模面设计方法,即在完成模具设计后,直接进行模面的调整,无须单独对零件进行数值模拟.针对橡皮成形零件的特点,提出基于特征的模面快速设计方法.研究曲弯边特征的回弹规律,并建立针对曲弯边的回弹分布函数,以实现回弹角快速预测.基于位移调整法,将回弹角转化为模面网格的调整量,可完成模面的补偿.将该方法应用于某飞机零件的模面设计中,通过数值模拟对补偿后的模具成形效果进行验证,结果表明该方法能明显地减少回弹误差. 相似文献
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型材拉弯件回弹的激光扫描检测技术研究 总被引:1,自引:0,他引:1
《工具技术》2015,(12):95-98
针对拉弯零件的回弹检测,采用激光扫描检测设备得到拉弯零件的点云检测数据,利用Geomagic Qualify软件的比较分析功能,对拉弯件的点云数据和CAD模型进行3D、2D比较,得出了型材的整体偏差分布以及主要截面的偏差情况。并利用Geomagic Studio软件从点云数据提取拉弯零件引导线,对引导线进行曲率分析。 相似文献
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介绍了模具型面应用回弹补偿技术的原理,在此基础上分析了该技术的注意事项及其在模具型面设计中的应用,通过研究为模具型面设计精确度的提高提供参考与借鉴。 相似文献
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叶春 《中国制造业信息化》2015,(6)
为了解决钣金成形后的回弹问题,提出一种基于模具型面的快速回弹补偿算法,能够直接在模具型面上完成回弹补偿。首先,对模具型面上的回弹曲线进行自动识别,并根据型面的回弹规律对曲线进行回弹补偿;其次,对补偿后曲线进行拟合,完成新的回弹补偿曲面;最后,通过对模具胎体的分割,完成模具胎体的回弹补偿。利用CATIA提供的 API接口,开发出橡皮囊模具快速回弹补偿系统,大幅提高了模具的设计效率。 相似文献
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Arild H. Clausen Odd S. Hopperstad Magnus Langseth 《International Journal of Mechanical Sciences》2001,43(2):427
Stretch bending is a process of considerable importance for plastic forming purposes. Effective operations in the industry demand sufficient knowledge of how different parameters influence the process as well as the final shape of the product. Numerical simulations are an effective way of investigating these issues. However, the numerical model must be validated in order to obtain reliable results. This paper presents an analysis model in the code LS-DYNA which is shown to represent the behaviour in laboratory tests well. The model is subsequently used to check the influence of certain parameters on the response in a stretch bending process. Simple, analytical methods are also presented. It is shown that the local deformations of the cross-section during bending are primarily controlled by the geometry and tensile force level. The main parameters influencing the springback during unloading are the strain hardening properties of the material, and the tensile force. 相似文献
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如何减小弯曲件的回弹,以控制制件精度,提高制件质量,一直是弯曲件生产中要解决的关键问题。从弯曲模结构设计角度,阐述了生产中常用减小回弹的方法和技巧。 相似文献
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Masatoshi Yoshida Fusahito Yoshida Haruyuki Konishi Koji Fukumoto 《International Journal of Mechanical Sciences》2005,47(12):1885-1896
Fracture limits in sheet stretch bending were theoretically obtained on the assumption that the fracture occurs when the stretching force reaches its maximum value. From the calculated results, a fracture criterion has been presented where limit wall stretch, Lmax/L0 (Lmax: limit wall length of a sheet, L0: initial wall length), is explicitly given as a function of the non-dimensional bending curvature, t0/R (t0: sheet thickness, R: bending radius) and the material's work hardening exponent (n-value). To verify this criterion, three-point stretch bending tests with various punch-radii were performed on three types of aluminum sheets (A5182-O, JIS6061-T4 and JIS6N01-T5). The predicted limit wall stretch, as well as limit forming height, were in good agreement with the experimental results. 相似文献
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