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JP4232566B2 - Shape grasp method in numerical analysis by finite element - Google Patents
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JP4232566B2 - Shape grasp method in numerical analysis by finite element - Google Patents

Shape grasp method in numerical analysis by finite element Download PDF

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JP4232566B2
JP4232566B2 JP2003274914A JP2003274914A JP4232566B2 JP 4232566 B2 JP4232566 B2 JP 4232566B2 JP 2003274914 A JP2003274914 A JP 2003274914A JP 2003274914 A JP2003274914 A JP 2003274914A JP 4232566 B2 JP4232566 B2 JP 4232566B2
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善樹 深田
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Description

本発明は、有限要素を用いた応力解析等で必要とされる面要素の3次元曲面形状を把握する形状把握方法に関する。 The present invention relates to a shape grasp how to grasp the 3-dimensional curved surface shape of the surface elements required by the like stress analysis using the finite element.

機械製品や建築物の構造材の応力解析手法として有限要素法(FEM=finite-element method)を用いた数値解析が広く用いられている。FEMは、対象物を比較的簡単な特性を有する有限の要素に分割してモデル化し、系全体の性能、挙動等を解析するものである(例えば、特許文献1参照)。   Numerical analysis using a finite-element method (FEM) is widely used as a stress analysis method for mechanical products and building structural materials. FEM divides an object into finite elements having relatively simple characteristics and models them, and analyzes the performance, behavior, and the like of the entire system (see, for example, Patent Document 1).

近年、ガラス繊維や炭素繊維などを充填して形成したFRP(fiber reinforced plastics)等の複合材を含む積層材料が航空機、船舶、自動車等の構造材として用いられるようになってきた。特許文献1記載の技術は、積層材料を同等の特性を有する均一な材質で置き換えるモデル化を行うことにより、こうした積層材料において、FEMの要素数を減少させて、演算を高速化させるものである。
特開2002−082998号公報(段落0013〜0042、図1〜図6)
In recent years, laminated materials containing composite materials such as FRP (fiber reinforced plastics) formed by filling glass fibers or carbon fibers have been used as structural materials for aircraft, ships, automobiles, and the like. The technique described in Patent Document 1 performs modeling by replacing a laminated material with a uniform material having equivalent characteristics, thereby reducing the number of FEM elements in such a laminated material and speeding up computation. .
JP 2002-082998 A (paragraphs 0013 to 0042, FIGS. 1 to 6)

ところで、このようなシェルモデルを用いたFEMでは、対象を節点によって面要素に分割して計算を行う。モデル形状の分析のために、面要素の曲率が必要な場合が考えられる。しかしながら、これまでの手法では、面要素の曲率を正確に求めるためには、曲率変化に対して要素を十分に小さくすることが必要とされており、シェルモデルそのものの要素数を減少させることは困難であった。   By the way, in FEM using such a shell model, calculation is performed by dividing an object into plane elements by nodes. It is conceivable that the curvature of the surface element is necessary for the analysis of the model shape. However, in the conventional methods, in order to obtain the curvature of the surface element accurately, it is necessary to make the element sufficiently small with respect to the curvature change, and reducing the number of elements of the shell model itself is not possible. It was difficult.

そこで、本発明は、シェルモデルの要素数が少ない場合でも、面要素の曲率を正確に求めることを可能とした面要素の3次元曲面形状を把握する形状把握方法を提供することを課題とする。 Therefore, an object of the present invention is to provide a shape grasping method for grasping a three-dimensional curved surface shape of a surface element that enables accurate calculation of the curvature of the surface element even when the number of elements of the shell model is small. .

上記課題を解決するため、本発明に係る形状把握方法は、解析対象物を節点によって面要素に分割する有限要素法による数値解析において面要素の3次元曲面形状を把握する形状把握方法であって、対象節点の位置座標ベクトルをX0、この節点の近傍節点の座標ベクトルをX、曲面に垂直な方向の単位ベクトルをP、節点における各方向の曲率半径の逆数を成分とする対称行列をQとするとき、対称行列Qに仮定した曲率値を代入して、 In order to solve the above problems, a shape grasping method according to the present invention is a shape grasping method for grasping a three-dimensional curved surface shape of a surface element in numerical analysis by a finite element method in which an analysis object is divided into surface elements by nodes. , The position coordinate vector of the target node is X 0 , the coordinate vector of the neighboring node of this node is X, the unit vector in the direction perpendicular to the curved surface is P , and the symmetric matrix whose component is the reciprocal of the radius of curvature in each direction at the node When substituting the assumed curvature value into the symmetric matrix Q,

Figure 0004232566

の近似解として単位ベクトルPを求め、得られた単位ベクトルPにより上記(1)を満たす近似解として対称行列Qの各成分を求めることにより、節点における各方向の曲率を対象節点と近傍の節点を通る2次関数により近似することで面要素の曲面形状を把握することを特徴とする
Figure 0004232566

A unit vector P is obtained as an approximate solution of, and each component of the symmetric matrix Q is obtained as an approximate solution satisfying the above (1) by the obtained unit vector P, whereby the curvature in each direction at the node is determined from the target node and nearby nodes. The curved surface shape of the surface element is grasped by approximating with a quadratic function passing through .

単位ベクトルPを求める際、仮定した曲率値として0を用いることが好ましい。曲率値0とは、要素が平面である場合に相当する When determining the unit vector P, preferably Rukoto using 0 as the assumed curvature value. A curvature value of 0 corresponds to a case where the element is a plane .

対称行列Qの各成分を求める際に、所定の重み付け係数をCとするとき、式(1)と、QP=0から近似値としてQの値を求めることがさらに好ましい。テンソルQには6個の独立成分があるが、2次関数で曲面を表現するには、曲面形状の自由度が多すぎる。この式は、曲面形状が不正に変形する方向の自由度を抑制する働きを持つ。さらに重みづけは最小自乗法を用いて解析的に解く場合の各式の寄与度を等価にする機能を有する。
When obtaining each component of the symmetric matrix Q, when the predetermined weighting coefficient is C, it is more preferable to obtain the value of Q as an approximate value from Equation (1) and C QP = 0. The tensor Q has six independent components, but there are too many degrees of freedom of the curved surface shape to express the curved surface with a quadratic function. This expression has a function of suppressing the degree of freedom in the direction in which the curved surface shape is illegally deformed. Further, the weighting has a function of equalizing the contribution of each expression when analytically solving using the least square method.

本発明によれば、シェルモデルの節点データから対象要素の3次元曲面形状を把握することができる。これにより、例えば、応力による曲面の変形、それに伴う応力成分の解析を簡単に行うことが可能となる。特に、曲面形状を把握する目的で、対象を細分割して要素数を増大させる必要はないため、計算精度を低下させることなく、少ない要素数で解析を行うことが可能となり、高速化と計算機資源の低減が図れる。   According to the present invention, the three-dimensional curved surface shape of the target element can be grasped from the node data of the shell model. As a result, for example, it is possible to easily analyze the deformation of the curved surface due to stress and the accompanying stress component. In particular, it is not necessary to subdivide the object and increase the number of elements for the purpose of grasping the curved surface shape, so it is possible to perform analysis with a small number of elements without reducing the calculation accuracy. Resources can be reduced.

以下、添付図面を参照して本発明の好適な実施の形態について詳細に説明する。説明の理解を容易にするため、各図面において同一の構成要素に対しては可能な限り同一の参照番号を附し、重複する説明は省略する。   DESCRIPTION OF EXEMPLARY EMBODIMENTS Hereinafter, preferred embodiments of the invention will be described in detail with reference to the accompanying drawings. In order to facilitate the understanding of the description, the same reference numerals are given to the same components in the drawings as much as possible, and duplicate descriptions are omitted.

図1は、本発明に係る曲面モデル形状の分析方法を含む数値解析の手法を示すブロック図である。この数値解析は、積層体からなる板を曲げた場合の層間応力をFEMを利用して解析する。この数値解析は、各種のコンピュータ上で行われるが、以下に示される各手段は、それぞれ単体のプログラムから構成されていてもよいし、複数のプログラムからなるプログラム群からなるソフトウェアとして構成されていてもよい。さらに、各手段は、異なるコンピュータ上で作動してもよいし、各手段が異なるコンピュータ上で作動する複数のソフトウェアにより構成されていてもよい。ここでいうプログラムには、それ自体が入出力機能を有するプログラムのほか、特定のプログラム上で作動するいわゆるマクロ、スクリプト等を含む。   FIG. 1 is a block diagram showing a numerical analysis technique including a curved surface model shape analysis method according to the present invention. In this numerical analysis, the interlaminar stress when a laminated plate is bent is analyzed using FEM. This numerical analysis is performed on various computers, but each means shown below may be configured as a single program or as software including a program group including a plurality of programs. Also good. Furthermore, each unit may operate on a different computer, or each unit may be configured by a plurality of software programs that operate on different computers. In this case, the program includes not only a program having an input / output function itself but also a so-called macro, script, etc. that operates on a specific program.

まず、FEM用モデル生成手段20では、対象手段の形状を表すバルクデータ(対象となる板をシェルモデルにより表す。)と、板に付与される荷重や板の拘束条件データを生成する。バルクデータは、各節点のデータを直接入力することで生成してもよいが、CADデータ等の形状データを基に、分割数を設定することにより、節点データを生成するようにしてもよい。あるいは、GUI(Graphical User Interface)を用いて形状、分割数等を設定して入力データを生成するようにしてもよい。   First, the FEM model generation unit 20 generates bulk data representing the shape of the target unit (a target plate is represented by a shell model), and a load applied to the plate and plate constraint data. Bulk data may be generated by directly inputting data of each node, but node data may be generated by setting the number of divisions based on shape data such as CAD data. Alternatively, input data may be generated by setting the shape, the number of divisions, and the like using a GUI (Graphical User Interface).

FEM解析手段30では、生成されたバルクデータと荷重・拘束条件を基にして既知のFEM解析手法に基づいて、各要素について面方向に働く面内応力を計算する。得られた面内応力データは、FEM用モデル生成手段20で生成されたバルクデータとともに、層間応力解析手段40へと送られる。層間応力解析手段40は、バルクデータを用いて本発明に係るモデル形状の分析方法を行う形状分析手段41と、面内応力について分析を行う応力分析手段42と、モデル形状と面内応力から層間応力を求める応力算出手段43からなる。   The FEM analysis means 30 calculates the in-plane stress acting in the plane direction for each element based on the known bulk data and load / constraint conditions based on the known FEM analysis technique. The obtained in-plane stress data is sent to the interlayer stress analysis means 40 together with the bulk data generated by the FEM model generation means 20. The interlaminar stress analysis means 40 includes a shape analysis means 41 for performing the model shape analysis method according to the present invention using bulk data, a stress analysis means 42 for analyzing the in-plane stress, and an interlaminar stress from the model shape and the in-plane stress. It comprises stress calculating means 43 for obtaining stress.

続いて、形状分析手段41におけるモデル形状の分析手法について詳細に説明する。図2は、曲面を表すシェルモデルの一例を示している。以下、対象節点の位置座標ベクトルをX0=(x0,y0,z0)、この節点の周囲の位置座標ベクトルをX=(x,y,z)とし、対象要素をSで表すこととする。この形状分析手段41では、さらに、面に直角な単位ベクトルとしてP=(Px,Py,Pz)(つまり、|P|=1である。)を設定するとともに、曲率を表すテンソルとして Next, the model shape analysis method in the shape analysis means 41 will be described in detail. FIG. 2 shows an example of a shell model representing a curved surface. Hereinafter, the position coordinate vector of the target node is X 0 = (x 0 , y 0 , z 0 ), the position coordinate vector around this node is X = (x, y, z), and the target element is represented by S. And In this shape analyzing means 41, P = (Px, Py, Pz) (that is, | P | = 1) is set as a unit vector perpendicular to the surface, and as a tensor representing the curvature.

Figure 0004232566
を用いる。QはQij=Qjiとなる対称行列であり、その独立な成分は、Qxx、Qxy、Qxz、Qyy、Qyz、Qzzの6個である。各成分は曲率半径の逆数を表す。例えば、QxxはX方向の曲率半径の逆数である。
Figure 0004232566
Is used. Q is a symmetric matrix with Qij = Qji, and there are six independent components Qxx, Qxy, Qxz, Qyy, Qyz, and Qzz. Each component represents the reciprocal of the radius of curvature. For example, Qxx is the reciprocal of the radius of curvature in the X direction.

図4は、この形状分析手段41における形状分析のフローチャートである。この計算は、モデル形状全体について行われる。   FIG. 4 is a flowchart of shape analysis in the shape analysis means 41. This calculation is performed for the entire model shape.

まず、対象節点および周辺節点の座標値を読み込む(ステップS1)。次に、ベクトルPを算出する(ステップS2)。これは、式(1)において、Q=0とすることで、(X−X0)・P=0を解くことにより、Pを求める。具体的には、(X−X0)・P=0を展開すると、(x−x0)Px=0、(y−y0)Py=0、(Z−Z0)Pz=0になる。そこで、Px=1、Py=1、Pz=1のそれぞれの場合について、この展開した各式の左辺に、対象節点とその周辺の節点座標を代入していき、その値の自乗値の和が最も小さくなるPを3つ求める。そして、その中で|P|が最も小さくなる解を選択し、その|P|が1になるよう、規格化することにより、Pを求める。 First, the coordinate values of the target node and the peripheral nodes are read (step S1). Next, the vector P is calculated (step S2). This is to obtain P by solving (X−X 0 ) · P = 0 by setting Q = 0 in equation (1). Specifically, when (X−X 0 ) · P = 0 is expanded, (x−x 0 ) Px = 0, (y−y 0 ) Py = 0, and (Z−Z 0 ) Pz = 0. . Therefore, in each case of Px = 1, Py = 1, and Pz = 1, the target node and its surrounding node coordinates are substituted into the left side of each expanded formula, and the sum of the squares of the values is calculated. Find the smallest three Ps. Then, the solution with the smallest | P | is selected, and P is obtained by standardizing the solution so that | P |

なお、Pは、図3に示されるように四角形である対象要素Sの周囲の節点をe1〜e4とし、節点ejからekに向かうベクトルをVjkで表すとき、例えば、 Note that when P is a node around the target element S is rectangular as shown in FIG. 3 and e 1 to e 4, which represents the vector directed from the node e j to e k in V jk, for example,

Figure 0004232566
により求めてもよい。
Figure 0004232566
You may ask for.

次に、式(1)からQの各成分Qxx、Qxy、Qxz、Qyy、Qyz、Qzzの値を求める(ステップS3)。ここで、式1を変形して展開すると、   Next, the value of each component Qxx, Qxy, Qxz, Qyy, Qyz, Qzz of Q is obtained from the equation (1) (step S3). Here, if equation 1 is transformed and expanded,

Figure 0004232566
となる。これは、節点周辺の曲面を2次関数で表現したものである。例えば、曲面がほぼXY面にあるとすると、z2の項は本来不要である。すなわち、図5に示されるように、本来の曲面がCactであるのに対し、式(1)にz2の項が存在することで、Ccal1のような曲面をフィッテングしてしまう可能性が出てくる。そこで、本発明では、QP=0となる式を条件として追加することでこのz2の項を小さくし、滑らかな曲線で節点間をつなぐようにした。
Figure 0004232566
It becomes. This is a representation of a curved surface around a node by a quadratic function. For example, if the curved surface is substantially in the XY plane, the term z 2 is not necessary. That is, as shown in FIG. 5, the original curved surface is Cact, but the presence of the z 2 term in equation (1) may cause fitting of a curved surface such as Ccal1. Come. Therefore, in the present invention, the expression of QP = 0 is added as a condition to reduce the term of z 2 so that the nodes are connected by a smooth curve.

具体的には、QP=0に重みCをかけて展開すると、次の3つの式が得られる。   Specifically, when QP = 0 is expanded by applying a weight C, the following three expressions are obtained.

Figure 0004232566
ここで、Cは、式(1)と次元を揃えるため、以下のように設定した。
Figure 0004232566
Here, C was set as follows in order to align the dimension with the formula (1).

Figure 0004232566
なお、C0は定数であり、0.1に設定したときに良好な結果が得られた。
Figure 0004232566
C 0 is a constant, and good results were obtained when set to 0.1.

これらの式に対象節点および周囲の節点座標を入力すると、周辺節点の数+3個の式が得られる。(図2に示される形状モデルでは、例えば、周辺節点として8節点を用いると、11個の式が得られる。)Pはすでに求めているから、未知の変数はQの各成分の6個であり、変数の数を式の数が上回る。そこで、誤差が最小となるよう最小自乗法によりQの各成分を求める。   When the target node and surrounding node coordinates are input to these equations, the number of the peripheral nodes + 3 equations are obtained. (In the shape model shown in FIG. 2, for example, if 8 nodes are used as the peripheral nodes, 11 equations are obtained.) Since P has already been obtained, the unknown variables are 6 of each component of Q. Yes, the number of expressions exceeds the number of variables. Therefore, each component of Q is obtained by the method of least squares so that the error is minimized.

次に、モデル内の節点全てについて計算が終了したか否かを判定し(ステップS4)、終了するまで節点を移動させてステップS1〜S3の処理を繰り返すことで、全節点について計算を行う。全ての節点について計算が終了したら各要素Sごとにその要素の周囲の節点のP、Qを平均することで、面要素のP、Qを算出して、面要素の曲率を求める(ステップS5)。このとき、Pの方向は、面の表を向く場合と、裏を向く場合の二通りが考えられる。そこで、要素座標e3の方向に揃える。 Next, it is determined whether or not the calculation has been completed for all the nodes in the model (step S4), the nodes are moved until the calculation is completed, and the processes in steps S1 to S3 are repeated to calculate for all the nodes. When the calculation is completed for all nodes, the P and Q of the surface elements are calculated for each element S by averaging the P and Q of the nodes around the element, thereby obtaining the curvature of the surface element (step S5). . At this time, there are two possible directions of P, that is, when facing the front of the surface and when facing the back. Therefore, it is aligned in the direction of the element coordinate e 3 .

ここでは、FEM解析に入力する形状データからモデル形状を分析する例を説明したが、応力付与に伴う変形後のモデル形状を解析するような場合には、FEM解析手段30から得られる面内応力解析結果も利用して各要素位置の移動を考慮して分析を行えばよい。   Here, an example in which the model shape is analyzed from the shape data input to the FEM analysis has been described. However, in the case where the model shape after deformation accompanying stress application is analyzed, the in-plane stress obtained from the FEM analysis means 30 The analysis result may be used in consideration of the movement of each element position.

また、本実施形態では有限要素法を用いて数値解析を行う場合について説明したが、有限要素法に代えて、対象物を有限の要素にモデル化して解析する他の解析方法を用いた場合にも、同様の効果を得ることができる。   Further, in the present embodiment, the case where the numerical analysis is performed using the finite element method has been described. However, instead of the finite element method, the case where another analysis method for modeling and analyzing the object as a finite element is used. The same effect can be obtained.

なお、本発明は曲面形状の分析方法に関するものであるが、曲面形状の再現にも利用できる。   The present invention relates to a method for analyzing a curved surface shape, but can also be used to reproduce a curved surface shape.

本発明に係る曲面モデル形状の分析方法を含む数値解析の手法を示すブロック図である。It is a block diagram which shows the method of numerical analysis including the analysis method of the curved surface model shape which concerns on this invention. FEM解析において曲面を表すシェルモデルの一例を示している。An example of a shell model representing a curved surface in FEM analysis is shown. 対象要素と節点ベクトルの関係を示す図である。It is a figure which shows the relationship between an object element and a nodal vector. 形状分析のフローチャートである。It is a flowchart of shape analysis. 余分な自由度の影響を示す図である。It is a figure which shows the influence of an extra freedom degree.

符号の説明Explanation of symbols

20…FEM用モデル生成手段、30…解析手段、40…層間応力解析手段、41…形状分析手段、42…応力分析手段、43…応力算出手段。   20 ... FEM model generation means, 30 ... analysis means, 40 ... interlayer stress analysis means, 41 ... shape analysis means, 42 ... stress analysis means, 43 ... stress calculation means.

Claims (3)

解析対象物を節点によって面要素に分割する有限要素法を用いたコンピュータによる数値解析において面要素の3次元曲面形状をその曲面方向と各方向の曲率半径により把握する形状把握方法であって、
対象節点の位置座標ベクトルをX0、この節点の近傍節点の座標ベクトルをX、対称節点を中心とする曲面に垂直な方向の単位ベクトルをP、節点における各方向の曲率半径の逆数を成分とする対称行列をQとして、
対称行列Qに所定の曲率値を代入して、
Figure 0004232566

の近似解として単位ベクトルPを求めるステップと、
得られた単位ベクトルPにより上記式(1)を満たす近似解として解析的に対称行列Qの各成分を求めることにより、節点における各方向の曲率を対象節点と近傍の節点を通る2次関数により近似して求めるステップとを備えることを特徴とする形状把握方法。
A shape grasping method for grasping a three-dimensional curved surface shape of a surface element by a curved surface direction and a radius of curvature in each direction in a numerical analysis by a computer using a finite element method for dividing an analysis object into surface elements by nodes ,
The position coordinate vector of the target node is X 0 , the coordinate vector of the neighboring node of this node is X, the unit vector in the direction perpendicular to the curved surface centered on the symmetric node is P , and the reciprocal of the radius of curvature in each direction at the node is the component Let Q be a symmetric matrix
Substituting a predetermined curvature value into the symmetric matrix Q,
Figure 0004232566

Obtaining a unit vector P as an approximate solution of
Analyzing each component of the symmetric matrix Q analytically as an approximate solution satisfying the above equation (1) from the obtained unit vector P, the curvature in each direction at the node is expressed by a quadratic function passing through the target node and nearby nodes. A shape grasping method comprising the step of obtaining by approximation .
前記単位ベクトルPを求めるステップにおいて、仮定した曲率値として0を用いることを特徴とする請求項1記載の形状把握方法。 In determining the unit vector P, the shape grasping method according to claim 1, wherein Rukoto using 0 as the assumed curvature value. 前記節点における各方向の曲率を求めるステップにおいて、所定の重み付け係数をCとするとき、式(1)と、CQP=0の近似解としてQの値を求めることを特徴とする請求項2記載の形状把握方法。 3. The value of Q is obtained as an approximate solution of Equation (1) and C QP = 0 , where C is a predetermined weighting coefficient in the step of obtaining curvature in each direction at the node. How to grasp the shape of
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