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    • 1. 发明申请
    • Methods and Systems for Designing Addendum Section of A Die in Sheet Metal Forming
    • 钣金成型中模具附加部分的设计方法与系统
    • US20130041635A1
    • 2013-02-14
    • US13208238
    • 2011-08-11
    • Xinhai ZhuPhilip HoLi Zhang
    • Xinhai ZhuPhilip HoLi Zhang
    • G06F17/50
    • G06F17/5018G06F2217/42
    • An improved method of creating a computerized numerical model representing addendum section is disclosed. Computerized numerical model is created by placing a plurality of surface patches at disjoint locations along an enclosed trim line of the product design surface and corresponding binder opening line. Each surface patch is bounded with top and bottom edges coincided with the enclosed trim line and the binder opening line, respectively. Each surface patch is further bounded with two side edges connecting corresponding ends of the top and bottom edges. To ensure a continuously smooth transition between the product design surface and the binder surface, a number of parameters are adjusted for each surface patch to obtain a desired surface geometry. Any gap between a neighboring pair of surface patches is filled with a filler patch using a blending procedure that ensures continuous smooth transition from two neighboring side edges of the neighboring pair.
    • 公开了一种改进的创建表示附录部分的计算机数字模型的方法。 通过沿着产品设计表面和相应的粘合剂开口线的封闭装饰线放置多个表面贴片而形成计算机化数值模型。 每个表面贴片的顶部和底部边缘分别与封闭的修剪线和粘合剂开口线一致。 每个表面贴片进一步界定了连接顶部和底部边缘的相应端部的两个侧边缘。 为了确保产品设计表面和粘合剂表面之间的连续平滑过渡,为每个表面贴片调整了许多参数以获得所需的表面几何形状。 相邻的一对表面贴片之间的任何间隙用填充片填充,使用混合程序,其确保从邻近对的两个相邻侧边缘的连续平滑过渡。
    • 2. 发明申请
    • Determination Of Failure In Sheet Metal Forming Simulation Using Isotropic Metal Failure Criteria
    • 使用各向同性金属破坏准则确定钣金成形模拟中的失效
    • US20140019099A1
    • 2014-01-16
    • US13549980
    • 2012-07-16
    • Xinhai ZhuLi Zhang
    • Xinhai ZhuLi Zhang
    • G06F17/10
    • G06F17/5018G06F2217/42
    • Systems and methods of determining structural failure in a computer simulation of manufacturing a sheet metal part are disclosed. A FEA model defined for a sheet metal manufacturing procedure includes a plurality of shell elements representing sheet metal blank. Shell elements are configured for emulating anisotropic material properties of the sheet metal. Numerically-simulated structural behaviors are obtained by conducting a computer simulation of manufacturing the sheet metal part using the FEA model with a metal forming simulation application module. The numerically-simulated structural behaviors include structural deformations in forms of equivalent strain and plastic flow direction during forming of the sheet metal part. A structural failure determination criterion is constructed using a planar isotropic material model of the sheet metal. Finally, the obtained structural behaviors are compared with the failure determination criterion to determine whether there is a structural failure in the computer simulation of manufacturing the sheet metal part.
    • 公开了在制造钣金件的计算机模拟中确定结构故障的系统和方法。 为金属板制造程序定义的FEA模型包括多个表示金属板坯的壳单元。 外壳元件被配置用于模拟金属板的各向异性材料性质。 通过使用具有金属成形模拟应用模块的FEA模型进行制造钣金零件的计算机模拟来获得数值模拟的结构行为。 数值模拟的结构行为包括在钣金零件成型期间等效应变和塑性流动方向形式的结构变形。 使用钣金的平面各向同性材料模型构造结构破坏确定标准。 最后,将获得的结构行为与故障确定标准进行比较,以确定在制造钣金零件的计算机模拟中是否存在结构故障。
    • 4. 发明申请
    • Trim Line Determination In A Deep Draw Manufacturing of A Sheet Metal Part
    • 钣金零件深冲制造中的修剪线测定
    • US20130325423A1
    • 2013-12-05
    • US13482703
    • 2012-05-29
    • Xinhai ZhuLi Zhang
    • Xinhai ZhuLi Zhang
    • G06G7/48
    • G06F17/5018
    • Methods and systems of determining a trim line in deep draw manufacturing of a sheet metal part are disclosed. A computerized model of a sheet metal part and the addendum surface geometry are defined. At least one flange portion in the computerized model is identified. Perform a numerical simulation of unfolding of the flange towards the addendum surface by applying a first set of numerical loads to each pair of adjacent finite elements. The first set of numerical loads is configured for flattening out the pair of finite elements with a bending moment determined using relative orientations of the pair finite elements and material properties of the part. A second set of numerical loads is applied to close any remaining gap between the unfolded flange and the addendum thereafter. The outer edge of the flange portions in their final unfolded configuration is designated as a trim line.
    • 公开了一种在钣金零件的深冲制造中确定修剪线的方法和系统。 定义了钣金件和附件表面几何形状的计算机化模型。 识别计算机化模型中的至少一个凸缘部分。 通过对每对相邻的有限元施加第一组数值载荷来执行法兰朝向齿顶表面展开的数值模拟。 第一组数值载荷被配置为使用一对有限元素的相对取向和部件的材料特性确定的弯曲力矩平坦化一对有限元。 应用第二组数值载荷来封闭展开的法兰和附件之间的剩余间隙。 凸缘部分的最终展开构型的外边缘被指定为修剪线。
    • 5. 发明申请
    • Sheet Metal Forming Failure Prediction Using Numerical Simulations
    • 使用数值模拟的钣金成形失效预测
    • US20110295570A1
    • 2011-12-01
    • US12789378
    • 2010-05-27
    • Xinhai ZhuLi Zhang
    • Xinhai ZhuLi Zhang
    • G06F17/50G06F17/11
    • G06F17/5018G06F2217/16G06F2217/42
    • Systems and methods of predicting sheet metal forming failure using numerical simulations (e.g., finite element analysis) are disclosed. A FEA model is defined for a particular sheet metal forming process. Blank sheet metal is modeled with a plurality of shell elements. Additionally, a deformation path-dependent forming limit diagram (FLD) is converted to a path-independent FLD. A time-marching simulation of the sheet metal forming process is conducted using the FEA model. At each solution cycle, equivalent strain at each integration point of shell element is checked against the corresponding forming limit strain value of the path-independent FLD. The ratio of the equivalent strain and the forming limit strain is defined as formability index. A time history of the formability index of each shell element is saved into a file and displayed to a monitor upon user's instructions. When a particular element's formability index reaches one or higher, a localized necking is predicted.
    • 公开了使用数值模拟(例如,有限元分析)预测钣金成形故障的系统和方法。 FEA模型是针对特定的钣金成型工艺定义的。 空白金属板用多个外壳元件建模。 另外,变形路径相关的成形极限图(FLD)被转换成一个独立于路径的FLD。 使用FEA模型进行钣金成型过程的时间推移模拟。 在每个溶液循环中,检查壳单元的每个积分点处的相对应变与相应的形成极限应变值的路径无关FLD。 等效应变和成形极限应变的比值定义为成形性指数。 每个shell元素的可成形性索引的时间历史记录被保存到文件中,并根据用户的指示显示给监视器。 当特定元素的成形性指数达到一个或更高时,预测出局部颈缩。
    • 9. 发明授权
    • ACK/NAK bit bundling in carrier aggregation scenarios
    • 在载波聚合情况下,ACK / NAK位绑定
    • US09577803B2
    • 2017-02-21
    • US14400339
    • 2012-05-11
    • Yu Yu YanChun Hai YaoPeter SkovLi Zhang
    • Yu Yu YanChun Hai YaoPeter SkovLi Zhang
    • H04L1/00H04L5/00H04L1/16
    • H04L5/0046H04L1/1635H04L5/001H04L5/0055
    • Techniques are disclosed for ACK/NAK bit bundling in carrier aggregation scenarios. Such measures exemplarily comprise generating a set of acknowledgement bits confirming receipt of payload data of a radio frame in a carrier aggregation mode aggregating a primary and at least one secondary carrier, said radio frame being divided into a plurality of downlink subframes and uplink subframes, each of said downlink subframes comprising at least one codeword per carrier, each of said acknowledgement bits is allocated to one of said codewords of one of said downlink subframes, and applying spatial domain bundling and/or time domain bundling on said set of acknowledgement bits distinctive for each of said primary and said at least one secondary carrier, wherein said spatial domain bundling is an AND operation of all acknowledgement bits allocated to each codeword of one carrier of said primary and said at least one secondary carrier and one downlink subframe.
    • 公开了在载波聚合情况下的ACK / NAK比特绑定技术。 这样的措施示例性地包括生成一组确认位,确认在聚合主载波和至少一个辅载波的载波聚合模式中接收无线帧的有效载荷数据,所述无线帧被划分为多个下行子帧和上行子帧,每个 的所述下行链路子帧包括每个载波的至少一个码字,每个所述确认位被分配给所述下行链路子帧之一的所述码字之一,并且在所述确认位集合上应用空间域绑定和/或时域绑定, 所述主载波和所述至少一个辅载波中的每一个,其中所述空域绑定是分配给所述主载波和所述至少一个辅载波的一个载波和一个下行链路子帧的每个码字的所有确认比特的“与”运算。