CN109948206B - A Parametric Modeling Method of Plate Finite Element Mesh for Diamond Pattern Processing by High Energy Beam - Google Patents

A Parametric Modeling Method of Plate Finite Element Mesh for Diamond Pattern Processing by High Energy Beam Download PDF

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CN109948206B
CN109948206B CN201910168671.1A CN201910168671A CN109948206B CN 109948206 B CN109948206 B CN 109948206B CN 201910168671 A CN201910168671 A CN 201910168671A CN 109948206 B CN109948206 B CN 109948206B
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蒋建伟
邱浩
王树有
门建兵
李梅
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Beijing Institute of Technology BIT
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Abstract

本发明提供了一种高能束加工菱形图案的平板有限元网格参数化建模方法,利用节点构造菱形六面体网格,完成包含高能束槽线的平板网格划分;然后补齐平板网格四周四个端面;接着根据高能束槽线与平板宽度和高度方向上的比例关系,确定高能束槽线缺陷区的单元数;其次分别沿平板宽度和高度方向删除高能束槽线缺陷区的区域网格完成建模;最后根据有限元软件的格式要求输出网格的节点和单元信息。本发明能够实现不同几何特征的高能束加工菱形图案的平板有限元网格建模,方法简便且效率高,供弹体做强度分析。

Figure 201910168671

The invention provides a method for parametric modeling of flat plate finite element grids for processing rhombus patterns by high-energy beams. A rhombic hexahedral grid is constructed by using nodes to complete the division of flat-plate grids including groove lines of high-energy beams; Four end faces; then according to the proportional relationship between the high-energy beam slot line and the width and height of the plate, the number of cells in the defect area of the high-energy beam slot line is determined; secondly, the area network of the defect area of the high-energy beam slot line is deleted along the width and height of the plate respectively. The grid completes the modeling; finally, the node and element information of the grid is output according to the format requirements of the finite element software. The invention can realize the high-energy beam processing diamond pattern flat plate finite element grid modeling with different geometric features, the method is simple and efficient, and the projectile body is used for strength analysis.

Figure 201910168671

Description

一种高能束加工菱形图案的平板有限元网格参数化建模方法A Parametric Modeling Method of Plate Finite Element Mesh for Diamond Pattern Processing by High Energy Beam

技术领域technical field

本发明涉及弹药技术领域,具体涉及一种高能束加工菱形图案的平板有限元网格参数化建模方法。The invention relates to the technical field of ammunition, in particular to a method for parametric modeling of flat plate finite element grids for processing diamond patterns with high-energy beams.

背景技术Background technique

为了提高战斗部的威力,采用高能束预控技术,可以使弹体在爆轰加载下获得形状和质量比较一致的预控破片,从而提高战斗部威力。高能束预控技术是使用电子束、激光束或者离子束等高能束将材料局部迅速加热到融化状态,弹体将融化的金属迅速冷却,在弹体上形成区域单元控制弹体的破碎。高能束菱形刻槽是指高能束刻槽的单元形状为菱形。在进行弹体高能束菱形刻槽设计时,需要对菱形刻槽的弹体强度进行分析,一般地可在弹体上取一平板试件进行分析。通过对高能束刻槽平板拉伸试验,可研究不同刻槽参数对弹体强度的影响,结合数值模拟分析,可获得高能束刻槽对弹体强度的影响规律。然而,由于平板高能束菱形刻槽的几何形状较为复杂,高能束加工的区域组成复杂,包含融化区、过渡区和缺陷区,如图1所示。In order to improve the power of the warhead, the use of high-energy beam pre-control technology can enable the projectile to obtain pre-control fragments with relatively consistent shape and quality under detonation loading, thereby improving the power of the warhead. The high-energy beam pre-control technology uses high-energy beams such as electron beams, laser beams or ion beams to rapidly heat the material locally to a molten state, and the projectile body rapidly cools the molten metal, forming a regional unit on the projectile body to control the fragmentation of the projectile body. The high-energy beam rhombic groove means that the unit shape of the high-energy beam grooving is a rhombus. When designing the diamond-shaped groove for high-energy beams of the projectile, it is necessary to analyze the projectile strength of the diamond-shaped groove. Generally, a flat plate specimen can be taken on the projectile for analysis. Through the tensile test of the high-energy beam grooved plate, the influence of different groove parameters on the projectile strength can be studied. Combined with the numerical simulation analysis, the influence law of the high-energy beam groove on the projectile strength can be obtained. However, due to the complex geometry of the flat plate high-energy beam diamond groove, the region processed by the high-energy beam has a complex composition, including melting, transition, and defect regions, as shown in Figure 1.

然而,由于平板菱形刻槽的几何形状较为复杂,利用商业建模软件实现平板菱形刻槽的有限元网格的建立非常耗时。首先建立菱形刻槽平板的三维模型,然后导入有限元软件进行网格划分,一般采用四面体网格划分,精度不高;若采用六面体网格,需要先对其中一个刻槽进行划分,然后镜像复制到其他刻槽,但是如果每个刻槽的角度不同,就不能直接镜像,还需要重新划分,步骤繁琐。另外,如需改变刻槽特征尺寸,则需要重新划分有限元网格,建模上大量的重复操作既繁琐又易出错,严重影响设计效率。However, due to the complex geometry of flat rhombus grooves, the establishment of finite element meshes for flat rhombus grooves using commercial modeling software is very time-consuming. First, build a 3D model of the diamond-shaped grooved plate, and then import the finite element software for mesh division. Generally, tetrahedral mesh is used, and the accuracy is not high; if hexahedral mesh is used, one of the grooves needs to be divided first, and then mirrored. Copy to other grooves, but if the angle of each groove is different, it cannot be mirrored directly, and it needs to be divided again, and the steps are cumbersome. In addition, if the feature size of the groove needs to be changed, the finite element mesh needs to be re-divided. A large number of repeated operations in modeling are cumbersome and error-prone, which seriously affects the design efficiency.

发明内容SUMMARY OF THE INVENTION

有鉴于此,本发明提供了一种高能束加工菱形图案的平板有限元网格参数化建模方法,能够实现不同几何特征的高能束加工菱形图案的平板有限元网格建模,方法简便且效率高,供弹体做强度分析。In view of this, the present invention provides a method for parametric modeling of flat plate finite element meshes with diamond-shaped patterns processed by high-energy beams, which can realize the modeling of flat-plate finite element meshes with diamond-shaped patterns processed by high-energy beams with different geometric features, and the method is simple and convenient. High efficiency, for projectile strength analysis.

本发明采取的技术方案如下:The technical scheme adopted by the present invention is as follows:

一种高能束加工菱形图案的平板有限元网格参数化建模方法,包括以下步骤:A method for parametric modeling of flat plate finite element mesh for processing diamond pattern by high-energy beam, comprising the following steps:

步骤一、利用节点构造菱形六面体网格,完成包含高能束槽线的平板网格划分;Step 1. Use nodes to construct a rhombic hexahedral mesh, and complete the plate mesh division including the high-energy beam groove lines;

步骤二、补齐平板网格四周四个端面;Step 2. Fill up the four end faces around the flat grid;

步骤三、根据高能束槽线与平板宽度和高度方向上的比例关系,确定高能束槽线缺陷区的单元数;Step 3: Determine the number of cells in the defect area of the high-energy beam slot line according to the proportional relationship between the high-energy beam slot line and the width and height of the plate;

步骤四、分别沿平板宽度和高度方向删除高能束槽线缺陷区的区域网格完成建模;Step 4. Complete the modeling by deleting the regional grid of the defect area of the high-energy beam groove line along the width and height of the plate respectively;

步骤四、根据有限元软件的格式要求输出网格的节点和单元信息。Step 4: Output the node and element information of the mesh according to the format requirements of the finite element software.

进一步地,以平板长度方向为X方向,所述步骤一的具体方法为:Further, taking the length direction of the flat plate as the X direction, the specific method of the step 1 is:

步骤101、计算笛卡尔坐标系下X、Y和Z方向的剖分数,并设定Z方向的剖分数;Step 101: Calculate the division fractions in the X, Y and Z directions under the Cartesian coordinate system, and set the division fractions in the Z direction;

步骤102、根据所述X、Y和Z方向的剖分数生成节点;Step 102, generating nodes according to the division fractions in the X, Y and Z directions;

步骤103、沿X正方向移动节点,使所述移动节点与原Y向的节点连线与X方向呈刻槽角度的一半;Step 103, moving the node along the positive X direction, so that the connection line between the moving node and the original node in the Y direction and the X direction are half of the groove angle;

步骤104、根据刻槽深度、平板厚度及Z方向剖分数确定高能束槽线Z方向刻槽的网格区域;Step 104: Determine the grid area of the high-energy beam groove line in the Z direction of the groove according to the groove depth, the thickness of the plate and the Z-direction section fraction;

步骤105、Z方向移动节点使槽底节点和刻槽深度一致;同时Z方向移动节点使槽线缺陷区上层节点与缺陷区高度一致;Step 105: Move the node in the Z direction to make the groove bottom node and the depth of the groove consistent; at the same time, move the node in the Z direction to make the height of the upper node in the defect area of the groove line consistent with the height of the defect area;

步骤106、利用节点构造菱形单元,得到包含高能束槽线的菱形六面体网格。Step 106 , using nodes to construct a rhombus element to obtain a rhombic hexahedron mesh including high-energy beam groove lines.

进一步地,所述步骤二的具体方法为:Further, the concrete method of described step 2 is:

步骤201、X方向上的两个端面:复制X方向的起始端一列和结束端一列节点,分别沿X方向正、负两个方向移动得到两个端面的端面节点;对于已沿X正向移动的节点,复制移动后与由起始端一列或结束端一列复制移动后的节点共线;Step 201. Two end faces in the X direction: copy the nodes of the first column and the end column of the X direction, and move them in the positive and negative directions of the X direction to obtain the end face nodes of the two end faces; The node copied and moved is collinear with the node copied and moved from the first column or the end column;

Y方向上的两个端面:复制Y方向的起始端两列和结束端两列节点,分别沿Y方向正、负两个方向移动得到两个端面的端面节点;Two end faces in the Y direction: Copy the nodes in the two columns at the start and the end in the Y direction, and move them along the positive and negative directions of the Y direction to obtain the end nodes of the two end faces;

步骤202、由节点构造四个端面的端面单元。Step 202 , constructing end face units of four end faces from nodes.

进一步地,所述步骤201的移动方法为:Further, the moving method of step 201 is:

X方向上:起始端一列和结束端一列移动距离取Lc/2Nx,已沿X方向移动的节点复制后移动距离取Lc/Nx,Lc为平板长度,Nx为X方向剖分数;In the X direction: L c /2N x is the moving distance of one column at the beginning and one column at the end, and L c /N x is the moving distance of the nodes that have moved in the X direction after copying, L c is the length of the plate, and N x is the cross section in the X direction Fraction;

Y方向上:起始端第一列和结束端的最后一列移动距离可取b/Ny,起始端第二列和结束端的第二列移动距离取2b/Ny,b为平板宽度,Ny为Y方向剖分数。In the Y direction: the movement distance of the first column at the start end and the last column at the end end can be b/N y , the movement distance of the second column at the start end and the second column at the end end is 2b/N y , b is the width of the plate, and N y is Y Orientation section fraction.

进一步地,所述步骤202由节点构造端面单元的具体方法为:8个节点构造一个单元,按照先z,再y,然后x方向存储节点,节点索引indexnodei按下式计算,i、j、k分别为X、Y、Z三个方向的节点索引,Nx为X方向剖分数,Ny为Y方向剖分数,Nz为Z方向剖分数,Further, in the step 202, the specific method of constructing the end face unit by the nodes is as follows: 8 nodes construct a unit, according to the first z, then y, and then the x direction stores the nodes, and the node index index nodei is calculated as follows, i, j, k is the node index in the three directions of X, Y, and Z, respectively, N x is the division fraction in the X direction, N y is the division fraction in the Y direction, and N z is the division fraction in the Z direction.

Figure GDA0002573602410000041
Figure GDA0002573602410000041

进一步地,所述步骤三的具体方法为:Further, the concrete method of described step 3 is:

步骤301、由Y方向刻槽间隔单元数和Z方向刻槽单元数确定过渡区区域单元;Step 301: Determine the transition zone area unit by the number of grooved spacing units in the Y direction and the number of grooved units in the Z direction;

步骤302、由Y方向刻槽间隔单元数和Z方向刻槽单元数确定融化区区域单元;Step 302: Determine the melting zone area unit by the number of groove interval units in the Y direction and the number of groove units in the Z direction;

步骤303、由Y方向刻槽间隔单元数和Z方向刻槽单元数确定缺陷区区域单元。Step 303 , determining the defect area region unit according to the number of groove spacing units in the Y direction and the number of groove units in the Z direction.

有益效果:Beneficial effects:

1、本发明能够实现不同几何特征的高能束加工菱形图案的平板有限元网格建模,由于加工图案为菱形,本方法直接构造菱形六面体网格进行划分,简单易实现;若要更改高能束槽线特征尺寸,仅需更改构造菱形六面体网格的几何特征参数即可建模,避免了改变高能束槽线特征尺寸的同时,重新建立三维模型并划分有限元网格的操作,避免给分析人员带来大量的重复劳动,解决了高能束加工菱形图案平板的几何形状较为复杂、有限元网格的建立过程繁琐的问题,对高能束加工菱形图案的弹体分析提供了便利、效率高。1. The present invention can realize the high-energy beam processing rhombus-shaped flat plate finite element mesh modeling with different geometric features. Since the processing pattern is rhombus, this method directly constructs a rhombic hexahedral mesh for division, which is simple and easy to implement; if the high-energy beam needs to be changed The feature size of the slot line can be modeled only by changing the geometric feature parameters of the rhombic hexahedral mesh, which avoids the operation of re-establishing the 3D model and dividing the finite element mesh while changing the feature size of the high-energy beam slot line, avoiding the need for analysis. The personnel brought a lot of repetitive work, which solved the problems of complex geometry of the high-energy beam processing diamond pattern plate and the cumbersome process of establishing the finite element mesh, which provided convenience and high efficiency for the projectile analysis of the high-energy beam processing diamond pattern.

2、本发明通过移动节点的方式构造菱形六面体网格,通过改变节点的几何特征精确控制高能束槽线的尺寸,响应速度快。2. The present invention constructs a rhombic hexahedron mesh by moving nodes, precisely controls the size of the high-energy beam slot lines by changing the geometric features of the nodes, and has a fast response speed.

3、本发明通过复制端部节点的方式移动补齐四个端面,构造出矩形端面,端面一致性好,便于与其他模型对接。3. The present invention moves and complements four end faces by duplicating the end nodes to construct a rectangular end face. The end faces have good consistency and are convenient for docking with other models.

4、本发明限定端部节点的移动距离,使得构造出的矩形端面网格不会过大也不会过小,因此不会由于网格大小影响有限元步长的计算时间。4. The present invention limits the moving distance of the end nodes, so that the constructed rectangular end face mesh is neither too large nor too small, so the calculation time of the finite element step size will not be affected by the size of the mesh.

附图说明Description of drawings

图1为基于高能束加工的模型区域分布示意图;Fig. 1 is a schematic diagram of model area distribution based on high-energy beam processing;

图2为本发明平板菱形六面体网格的主视图;Fig. 2 is the front view of the flat rhombic hexahedron grid of the present invention;

图3为本发明平板的局部截面图;3 is a partial cross-sectional view of a flat panel of the present invention;

图4为本发明菱形边长示意图;Fig. 4 is the schematic diagram of rhombus side length of the present invention;

图5为本发明节点沿X方向移动前示意图;Fig. 5 is the schematic diagram before the node of the present invention moves along the X direction;

图6为本发明节点沿X方向移动后示意图;Fig. 6 is the schematic diagram after the node of the present invention moves along the X direction;

图7为本发明8个节点构造一个单元的索引顺序示意图;7 is a schematic diagram of the index sequence of 8 nodes of the present invention constructing a unit;

图8为本发明四个端面的节点移动示意图;8 is a schematic diagram of node movement of four end faces of the present invention;

图9为本发明端面单元的网格划分示意图;Fig. 9 is the mesh division schematic diagram of the end face unit of the present invention;

图10为本发明平板高能束菱形六面体网格划分示意图;FIG. 10 is a schematic diagram of mesh division of a flat plate high-energy beam rhombic hexahedron according to the present invention;

图11为本发明高能束槽线的菱形六面体网格划分示意图;11 is a schematic diagram of the rhombic hexahedral mesh division of the high-energy beam slot line of the present invention;

图12为本发明平板网格划分后的左视图。Fig. 12 is a left side view of the present invention after the flat plate mesh is divided.

具体实施方式Detailed ways

下面结合附图并举实施例,对本发明进行详细描述。The present invention will be described in detail below with reference to the accompanying drawings and embodiments.

本发明提供了一种高能束加工菱形图案的平板有限元网格参数化建模方法,利用节点构造菱形六面体网格进行包含高能束槽线的平板网格划分,补齐平板网格四周四个端面,然后根据高能束槽线与平板宽度和高度方向上的比例关系,确定高能束槽线缺陷区的单元数,分别沿平板宽度和高度方向删除高能束槽线缺陷区的区域网格完成建模,如图10、图11及图12所示,具体包括以下步骤:The invention provides a method for parametric modeling of flat plate finite element grids for processing diamond patterns by high-energy beams. The rhombic hexahedral grid is constructed by using nodes to divide the plate grids including the groove lines of the high-energy beams. Then, according to the proportional relationship between the high-energy beam slot line and the width and height of the plate, the number of cells in the defect area of the high-energy beam slot line is determined, and the area grid of the defect area of the high-energy beam slot line is deleted along the width and height of the plate respectively to complete the construction. The mold, as shown in Figure 10, Figure 11 and Figure 12, specifically includes the following steps:

步骤1、归纳平板高能束菱形刻槽的几何特征;Step 1. Summarize the geometric features of the diamond-shaped grooves of the flat plate high-energy beam;

平板厚度t=10mm,平板宽度b=20mm,平板长度Lc=100mm,刻槽宽度w=1mm,刻槽深度h=5mm,刻槽间隔a=10mm,刻槽角度θ=90°,槽线相交所得菱形沿刻槽宽度方向的单元数量N=3,缺陷区高度h0=1mm,融化区宽度占刻槽宽度的比例S0=1/3。如图2、图3和图4所示。Plate thickness t = 10mm, plate width b = 20mm, plate length L c = 100mm, groove width w = 1mm, groove depth h = 5mm, groove interval a = 10mm, groove angle θ = 90°, groove line The number of cells in the intersecting rhombus along the width direction of the groove is N=3, the height of the defect area is h 0 =1 mm, and the ratio of the width of the melted area to the width of the groove is S 0 =1/3. As shown in Figure 2, Figure 3 and Figure 4.

步骤2、计算槽线相交所得菱形的边长;Step 2. Calculate the side length of the rhombus obtained by the intersection of the groove lines;

如图4所示,槽线相交所得菱形边长用l表示,即菱形六面体网格边长,菱形边长l计算按式(1)计算得l=1mm,As shown in Figure 4, the side length of the rhombus obtained from the intersection of the groove lines is represented by l, that is, the side length of the rhombic hexahedron mesh.

Figure GDA0002573602410000061
Figure GDA0002573602410000061

步骤3、计算笛卡尔坐标系下的X、Y、Z方向的剖分数;Step 3. Calculate the section fractions in the X, Y, and Z directions under the Cartesian coordinate system;

以平板长度方向为X方向,X方向剖分数为Nx,Y方向剖分数为Ny,Z方向剖分数为Nz。Nz可根据需要给一个定值,X方向剖分数Nx和Y方向剖分数Ny可按式(2)计算,Nx=212,Ny=28,取垂直剖分数Nz=10。The length direction of the plate is taken as the X direction, the X-direction section is N x , the Y-direction section is N y , and the Z-direction section is N z . N z can be given a fixed value as required, and the X-direction division fraction N x and the Y-direction division fraction N y can be calculated according to formula (2), N x =212, N y =28, and the vertical division fraction N z =10.

Figure GDA0002573602410000062
Figure GDA0002573602410000062

Figure GDA0002573602410000063
Figure GDA0002573602410000063

步骤4、生成平板节点;Step 4. Generate a flat node;

根据步骤3的X方向剖分数为Nx,Y方向剖分数为Ny,Z方向剖分数为Nz生成平板内部节点,由线的端点得到线的节点,由对边节点得到面的节点,由对面节点得到体的节点。节点按照先X,再Y,然后Z方向存储,方便后续步骤构造菱形单元。According to step 3, the X-direction section fraction is N x , the Y-direction section fraction is N y , and the Z-direction section fraction is N z to generate the internal nodes of the plate, the line nodes are obtained from the endpoints of the lines, and the surface nodes are obtained from the opposite edge nodes, The node of the volume is obtained from the opposite node. Nodes are stored in the X, Y, and Z directions first, which is convenient for subsequent steps to construct diamond-shaped elements.

步骤5、X向移动节点;Step 5. Move the node in the X direction;

对节点进行X正方向移动,在笛卡尔坐标系下,X、Y、Z三个方向的节点索引分别为i、j、k,其中,i=1,2,……,Nx;j=1,2,……,Ny;k=1,2,……,Nz。则每个节点的移动距离Δx按式(3)计算,计算得Δx=0.2358。如图5所示,虚线框I为移动前节点位置,如图6所示,虚线框I’为移动后节点位置。Move the node in the positive X direction. In the Cartesian coordinate system, the node indices in the three directions of X, Y, and Z are i, j, and k, respectively, where i=1, 2,  , N x ; j= 1, 2, ..., N y ; k=1, 2, ..., N z . Then the moving distance Δx of each node is calculated according to formula (3), and Δx=0.2358 is calculated. As shown in FIG. 5 , the dotted frame I is the node position before the movement, and as shown in FIG. 6 , the dotted frame I′ is the node position after the movement.

Figure GDA0002573602410000071
Figure GDA0002573602410000071

步骤6、计算Z方向刻槽区域的网格;Step 6. Calculate the grid of the grooved area in the Z direction;

Z方向要刻槽的网格数N’r由式(4)计算得到Nr'=5。The number of grids N' r to be grooved in the Z direction is calculated by formula (4) to obtain N r '=5.

Figure GDA0002573602410000072
Figure GDA0002573602410000072

步骤7、Z方向移动节点使槽底节点和槽深一致;Step 7. Move the node in the Z direction to make the bottom node of the groove and the groove depth consistent;

Z方向移动节点使槽底节点和槽深一致,移动距离按式(5)计算,计算得Move the node in the Z direction so that the bottom node of the groove is consistent with the groove depth, and the moving distance is calculated according to formula (5).

Δz=0。Δz=0.

Figure GDA0002573602410000073
Figure GDA0002573602410000073

步骤8、计算缺陷区Z方向单元数;Step 8. Calculate the number of units in the Z direction of the defect area;

缺陷区Z方向单元数用Hz表示,按式(6)计算得Hz=1。The number of units in the Z direction of the defect area is represented by Hz , and Hz = 1 is calculated according to formula (6).

Figure GDA0002573602410000074
Figure GDA0002573602410000074

步骤9、Z方向移动节点使缺陷区上层节点与缺陷区高度一致;Step 9. Move the node in the Z direction to make the upper node of the defect area consistent with the height of the defect area;

在柱坐标系下,r、

Figure GDA0002573602410000076
z三个方向的节点索引分别为i、j、k,对索引i=Nr-N'r+Hr的节点进行径向移动,Z方向移动节点使缺陷区上层节点与缺陷区高度一致,移动距离按式(7)计算,计算得Δzh=0。In the cylindrical coordinate system, r,
Figure GDA0002573602410000076
The node indices in the three directions of z are i, j, and k, respectively. Move the node with index i=N r -N' r +H r radially, and move the node in the Z direction to make the upper node of the defect area consistent with the height of the defect area. The moving distance is calculated according to formula (7), and Δzh =0 is calculated.

Figure GDA0002573602410000075
Figure GDA0002573602410000075

步骤10、由节点构造菱形单元;Step 10. Construct a rhombus element from nodes;

八个节点构造一个单元,索引顺序如图7所示,以笛卡尔坐标系原点为节点1,y方向上的点为节点2,xy平面上的点为节点3,x方向上的点为节点4,z方向上的点为节点5,yz平面上的点为节点6,xyz空间内的点为节点7,xz平面上的点为节点8。对于按照先z,再y,然后x方向存储的所有节点,单元的节点索引indexnodei可按式(8)计算。构造的菱形单元按照先z,再y,然后x方向存储,方便后续刻槽。Eight nodes construct a unit. The index order is shown in Figure 7. The origin of the Cartesian coordinate system is node 1, the point in the y direction is node 2, the point on the xy plane is node 3, and the point in the x direction is node 3 4. The point in the z direction is node 5, the point on the yz plane is node 6, the point in the xyz space is node 7, and the point on the xz plane is node 8. For all nodes stored in the first z, then y, and then x directions, the node index nodei of the element can be calculated according to equation (8). The constructed diamond-shaped units are stored in the z, then y, and then x directions, which is convenient for subsequent grooving.

Figure GDA0002573602410000081
Figure GDA0002573602410000081

当Y方向的索引j为偶数时按式(9)计算When the index j in the Y direction is an even number, it is calculated according to formula (9)

Figure GDA0002573602410000082
Figure GDA0002573602410000082

步骤11、生成四个端面节点;Step 11. Generate four end face nodes;

X轴负方向为后端面,X轴正方向为前端面,Y轴负方向为左端面,Y轴正方向为右端面。后端面的节点通过复制X方向起始端的第一列节点,然后沿X方向移动得到,移动方向为X轴负方向,移动距离可取Lc/2Nx,对于已向X正向移动的节点,复制后移动距离可取Lc/Nx。前端面的节点通过复制X方向结束端的一列节点移动后得到,移动方向为X轴正方向,移动距离可取Lc/2Nx和Lc/Nx。左端面的节点通过复制Y轴方向起始端的第一列和第二列节点,然后沿Y方向移动得到,移动方向为Y轴的负方向,起始端的第一列移动距离可取b/Ny,起始端第二列移动距离可取2b/Ny。右端面的节点通过复制Y轴方向结束端的最后两列节点,然后沿Y方向移动得到,移动方向为Y轴的正方向,第一列移动距离可取b/Ny,第二列移动距离可取2b/Ny,生成的四个端面节点如图8虚线框所示。The negative direction of the X axis is the rear end surface, the positive direction of the X axis is the front end surface, the negative direction of the Y axis is the left end surface, and the positive direction of the Y axis is the right end surface. The nodes on the rear face are obtained by copying the first column of nodes at the beginning of the X direction, and then moving along the X direction. The moving direction is the negative direction of the X axis, and the moving distance can be L c /2N x . For the nodes that have moved to the positive X direction, The moving distance after copying can be L c /N x . The nodes on the front face are obtained by copying a column of nodes at the end of the X direction and moving, the moving direction is the positive direction of the X axis, and the moving distances can be L c /2N x and L c /N x . The nodes on the left end face are obtained by copying the first and second columns of nodes at the starting end of the Y-axis direction, and then moving them along the Y -direction. , the moving distance of the second column of the starting end can be 2b/N y . The nodes on the right end face are obtained by copying the last two columns of nodes at the end of the Y-axis direction, and then moving them along the Y-direction. The moving direction is the positive direction of the Y-axis. The first column can be moved by b/N y , and the second column can be moved by 2b /N y , the generated four end-face nodes are shown in the dotted box in Figure 8.

步骤12、由节点构造四个端面单元;Step 12. Construct four end face elements from nodes;

由8个节点构造一个单元,对于按照先Z,再Y,然后X方向存储的节点,单元的节点索引indexnodei可按式(10)计算,四个端面单元如图9所示。A unit is constructed by 8 nodes. For nodes stored in the Z, Y, and X directions first, the node index nodei of the unit can be calculated according to formula (10), and the four end face elements are shown in Figure 9.

Figure GDA0002573602410000091
Figure GDA0002573602410000091

步骤13、计算Y方向刻槽间隔网格数;Step 13: Calculate the grid number of grooves in the Y direction;

Y方向刻槽间隔网格数由刻槽宽度和单个槽的网格数量计算得到,可按式(11)计算。The grid number of the groove interval in the Y direction is calculated from the groove width and the grid number of a single groove, and can be calculated according to formula (11).

Figure GDA0002573602410000092
Figure GDA0002573602410000092

步骤14、设置过渡区;Step 14, set the transition area;

由Y方向刻槽间隔单元数和Z方向刻槽单元数分别确定刻槽区域单元的Y方向索引和Z方向索引,设置单元中所有满足Y方向索引和Z方向索引的单元为过渡区。The Y direction index and Z direction index of the groove area unit are respectively determined by the number of groove interval units in the Y direction and the number of groove units in the Z direction, and all units that satisfy the Y direction index and the Z direction index in the unit are set as transition areas.

步骤15、计算融化区Z方向单元数和融化区宽度上单元数;Step 15: Calculate the number of cells in the Z direction of the melting zone and the number of cells in the width of the melting zone;

由式(12)计算融化区Z方向单元数HmThe number of elements H m in the Z direction of the melting zone is calculated from the formula (12).

Hm=Nz-Hz (12)H m =N z -H z (12)

由式(13)计算融化区宽度上单元数NmThe number of units N m across the width of the melting zone is calculated from equation (13).

Nm=NS0 (13)N m =NS 0 (13)

步骤16、设置融化区;Step 16, set the melting area;

由Y方向刻槽间隔单元数和Z方向刻槽单元数分别确定融化区域单元的Y方向索引和Z方向索引,设置单元中所有满足Y方向索引和Z方向索引的单元为融化区。The Y-direction index and Z-direction index of the melting area unit are respectively determined by the number of grooved interval units in the Y direction and the number of grooved units in the Z direction.

步骤17、删除缺陷区单元;Step 17, delete the defective area unit;

由Y方向刻槽间隔单元数和Z方向刻槽单元数分别确定缺陷区域单元的Y方向索引和Z方向索引,设置单元中所有满足Y方向索引和Z方向索引的单元为缺陷区,删除缺陷区单元。Determine the Y-direction index and Z-direction index of the defective area unit by the number of grooved interval units in the Y direction and the number of grooved units in the Z direction unit.

步骤18、输出单元和节点;Step 18, output unit and node;

可依据不同求解器的格式要求,格式化输出网格的节点和单元信息。The node and element information of the output mesh can be formatted according to the format requirements of different solvers.

综上所述,以上仅为本发明的较佳实施例而已,并非用于限定本发明的保护范围。凡在本发明的精神和原则之内,所作的任何修改、等同替换、改进等,均应包含在本发明的保护范围之内。To sum up, the above are only preferred embodiments of the present invention, and are not intended to limit the protection scope of the present invention. Any modification, equivalent replacement, improvement, etc. made within the spirit and principle of the present invention shall be included within the protection scope of the present invention.

Claims (6)

1. A flat finite element mesh parametric modeling method for processing diamond patterns by high energy beams is characterized by comprising the following steps:
constructing a rhombohedral grid by using nodes to finish the division of a flat grid containing high-energy beam slot lines;
step two, four end faces around the flat grid are filled;
determining the number of units in the defect area of the high-energy beam slot line according to the proportional relation between the high-energy beam slot line and the width and height directions of the flat plate;
deleting the area grids of the high-energy beam slot line defect area along the width direction and the height direction of the flat plate respectively to complete modeling;
and step four, outputting node and unit information of the grid according to the format requirement of the finite element software.
2. The parametric modeling method for finite element meshes of a plate with a diamond-shaped pattern processed by high energy beams as claimed in claim 1, wherein the length direction of the plate is taken as the X direction, and the specific method of the step one comprises the following steps:
101, calculating X, Y subdivision numbers in a Z direction under a Cartesian coordinate system, and setting the subdivision number in the Z direction;
102, generating nodes according to the X, Y and the subdivision number in the Z direction;
103, moving the node along the positive X direction, so that the connecting line of the moving node and the adjacent node in the Y direction forms a half of the grooving angle with the X direction;
104, determining a grid area of the high-energy beam groove line in the Z direction according to the groove depth, the plate thickness and the Z direction section;
105, moving the node in the Z direction to enable the depth of the node at the bottom of the groove to be consistent with that of the notch groove; meanwhile, moving the node in the Z direction to enable the upper-layer node of the slot line defect area to be consistent with the height of the defect area;
and 106, constructing a diamond unit by using the nodes to obtain a diamond hexahedron grid containing the high-energy beam slot line.
3. The method for modeling a flat finite element mesh with a diamond pattern processed by high energy beams according to claim 2, wherein the specific method in the second step is as follows:
step 201, two end faces in the X direction: copying a starting end row and an ending end row of nodes in the X direction, and respectively moving along the positive direction and the negative direction of the X direction to obtain end surface nodes of two end surfaces; for the nodes which have moved along the X forward direction, the nodes which are copied and moved by the starting end column or the ending end column after copying and moving are collinear;
two end faces in the Y direction: copying two columns of nodes of a starting end and two columns of nodes of an ending end in the Y direction, and respectively moving along the positive direction and the negative direction of the Y direction to obtain end surface nodes of two end surfaces;
and 202, constructing end face units of four end faces by the nodes.
4. The method for parameterizing the finite element mesh of a slab with a diamond-shaped pattern processed by high energy beams of claim 3, wherein the moving method of the step 201 comprises the following steps:
in the X direction: taking L as the moving distance of the starting end column and the ending end columnc/2NxThe moving distance after copying the node which has moved in the X direction is taken as Lc/Nx,LcIs the length of the plate, NxIs the fraction in the X direction;
in the Y direction: the moving distance of the first column at the starting end and the last column at the ending end can be b/NyThe moving distance of the second row of the starting end and the second row of the ending end is 2b/NyB is the width of the plate, NyIs the fraction in the Y direction.
5. The method of parametric modeling of high energy beam machined diamond patterned flat finite element mesh as claimed in claim 3 wherein said step 202 of constructing end face elements from nodes is by: 8 nodes construct a unit, and the nodes and the node index are stored according to the directions of z, y and xnodeiThe calculation is as follows, i, j, k are node indexes of X, Y, Z directions respectively, NxIs the fraction in the X direction, NyIs a fraction in the Y direction, NzIs the section in the Z direction, and is the section in the Z direction,
Figure FDA0002573602400000031
6. the method for modeling a flat finite element mesh with a diamond pattern processed by high energy beams according to claim 1, wherein the specific method in the third step is as follows:
step 301, determining a transition area unit according to the number of the notching interval units in the Y direction and the number of the notching units in the Z direction;
step 302, determining a melting area unit according to the number of the interval units of the groove in the Y direction and the number of the groove units in the Z direction;
step 303, determining the defective area unit according to the number of the spacing units for notching in the Y direction and the number of the notching units in the Z direction.
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Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101763653A (en) * 2010-01-06 2010-06-30 大连民族学院 Auxiliary parallelepiped space-based method for generating face-centered cubic grid straight line
CN104077455A (en) * 2014-07-08 2014-10-01 天津大学 Method for optimizing size of key part of two-phase-flow annular space lumped sensing system
CN106844963A (en) * 2017-01-20 2017-06-13 中国水利水电科学研究院 Excavation simulation extremely runs the arch dam three-dimensional grid model automatic division method of overall process
CN108509693A (en) * 2018-03-13 2018-09-07 中南大学 Three-dimensional frequency domain controllable source method for numerical simulation
CN108563887A (en) * 2018-04-23 2018-09-21 北京智交慧桥科技有限公司 A kind of intelligent analysis system of Test on Bridge Loading

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9115554B2 (en) * 2010-11-19 2015-08-25 Baker Hughes Incorporated Earth-boring tools including replaceable cutting structures and related methods

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101763653A (en) * 2010-01-06 2010-06-30 大连民族学院 Auxiliary parallelepiped space-based method for generating face-centered cubic grid straight line
CN104077455A (en) * 2014-07-08 2014-10-01 天津大学 Method for optimizing size of key part of two-phase-flow annular space lumped sensing system
CN106844963A (en) * 2017-01-20 2017-06-13 中国水利水电科学研究院 Excavation simulation extremely runs the arch dam three-dimensional grid model automatic division method of overall process
CN108509693A (en) * 2018-03-13 2018-09-07 中南大学 Three-dimensional frequency domain controllable source method for numerical simulation
CN108563887A (en) * 2018-04-23 2018-09-21 北京智交慧桥科技有限公司 A kind of intelligent analysis system of Test on Bridge Loading

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
"A High-Accuracy Approach to Finite Element Analysis Using the Hexa 27-Node Element";Pedro V. Marcal.et al;《ASME 2016 Pressure Vessels and Piping Conference》;20160731;全文 *
"空间理性八节点块体元";王永富等;《应用力学学报》;20030930;第20卷(第3期);第131-135页 *

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