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JP6925706B2 - Press molding simulation method - Google Patents
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JP6925706B2 - Press molding simulation method - Google Patents

Press molding simulation method Download PDF

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JP6925706B2
JP6925706B2 JP2017057790A JP2017057790A JP6925706B2 JP 6925706 B2 JP6925706 B2 JP 6925706B2 JP 2017057790 A JP2017057790 A JP 2017057790A JP 2017057790 A JP2017057790 A JP 2017057790A JP 6925706 B2 JP6925706 B2 JP 6925706B2
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正彦 福島
正彦 福島
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Daihatsu Motor Co Ltd
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Description

本発明は、プレス成形のシミュレーション方法に関する。 The present invention relates to a method for simulating press molding.

金属板(ブランク材)にプレス成形を施すと、離型時に成形品にスプリングバックが生じるため、寸法精度が悪化することは避けられない。そこで、成形品の寸法精度を高めるために、予めプレス成形のシミュレーションを行って成形品の形状を算出し、この算出結果に基づいて金型形状等を調整することが行われている(例えば、下記の特許文献1、2参照)。 When a metal plate (blank material) is press-molded, springback occurs in the molded product at the time of mold release, so that it is inevitable that the dimensional accuracy deteriorates. Therefore, in order to improve the dimensional accuracy of the molded product, the shape of the molded product is calculated in advance by performing a press molding simulation, and the mold shape and the like are adjusted based on the calculation result (for example,). See Patent Documents 1 and 2 below).

特開2002−45920号公報Japanese Unexamined Patent Publication No. 2002-45920 特開2012−153045号公報Japanese Unexamined Patent Publication No. 2012-153045

上記のようなプレス成形シミュレーションでは、通常、金型を剛体、ワークを変形体とみなして計算を行う。しかし、この場合、加工中の成形反力による金型の成形面の撓み変形が考慮されないため、シミュレーションのアウトプット精度が低下してしまう。 In the press molding simulation as described above, the calculation is usually performed by regarding the die as a rigid body and the work as a deformed body. However, in this case, since the bending deformation of the molding surface of the mold due to the molding reaction force during processing is not taken into consideration, the output accuracy of the simulation is lowered.

例えば、金型の弾性体ソリッド要素モデル(金型を多数の立体的なソリッド要素に分割した弾性体モデル)を用いることで、金型の撓み変形を考慮した成形シミュレーションを行うことができる。具体的には、加工中に時々刻々と変化する成形反力を算出し、この成形反力に基づいて金型の弾性体ソリッド要素モデルの各時点における変形量を計算することで、プレス成形過程における金型の撓み変形を動的に再現することが可能となり、成形シミュレーションのアウトプット精度が高められる。しかし、このような金型の三次元的な弾性体ソリッド要素モデルを用いたシミュレーションは、計算負荷が非常に大きいため、膨大な計算時間を要する。 For example, by using an elastic solid element model of a mold (an elastic model in which a mold is divided into a large number of three-dimensional solid elements), it is possible to perform a molding simulation in consideration of bending deformation of the mold. Specifically, the press molding process is performed by calculating the molding reaction force that changes from moment to moment during processing and calculating the amount of deformation of the elastic solid element model of the die at each time point based on this molding reaction force. It is possible to dynamically reproduce the bending deformation of the mold in the above, and the output accuracy of the molding simulation is improved. However, the simulation using such a three-dimensional elastic solid element model of the mold requires a huge calculation time because the calculation load is very large.

そこで、本発明が解決すべき課題は、プレス成形のシミュレーション方法において、成形中の金型の成形面の撓み変形を考慮してシミュレーションの精度を高めると共に、計算負荷を軽減して計算時間を短縮することにある。 Therefore, the problem to be solved by the present invention is to improve the accuracy of the simulation in consideration of the bending deformation of the molding surface of the mold during molding in the press molding simulation method, and reduce the calculation load to shorten the calculation time. To do.

前記課題を解決するために、本発明は、プレス成形のシミュレーション方法であって、成形ストローク過程の複数の段階における金型の成形面の撓み量を算出するステップと、各段階における撓み量を反映した複数の成形面の剛体シェル要素モデルを作成するステップと、ある段階の撓み量を反映した第1の成形面の剛体シェル要素モデルで材料モデルを成形しながら、次の段階の撓み量を反映した第2の成形面の剛体シェル要素モデルが、前記第1の成形面の剛体シェル要素モデルを追い抜いて前記材料モデルを成形するシミュレーションを行うステップとを備えたプレス成形のシミュレーション方法を提供する。 In order to solve the above problems, the present invention is a press molding simulation method, which reflects a step of calculating the amount of bending of the molding surface of a mold at a plurality of stages of a molding stroke process and the amount of bending at each stage. While molding the material model with the step of creating a rigid shell element model of a plurality of molded surfaces and the rigid shell element model of the first molding surface that reflects the amount of deflection at a certain stage, the amount of deflection at the next stage is reflected. Provided is a press molding simulation method including a step in which the rigid shell element model of the second molding surface overtakes the rigid shell element model of the first molding surface to perform a simulation of molding the material model.

このように、本発明では、成形ストローク過程を複数の段階に分け、各段階における成形面の剛体シェル要素モデル(成形面を多数の平面的なシェル要素に分割した剛体モデル)を用いて成形シミュレーションを行う。具体的には、ストローク途中の複数段階における成形反力から金型の成形面の撓み量を計算し、各段階における撓み量を反映させた成形面の剛体シェル要素モデルを作成する。そして、ストローク途中の各段階で、それぞれの段階に応じた剛体シェル要素モデルを用いることにより、成形ストローク過程における成形面の撓み変形を段階的に再現することができるため、シミュレーションの精度が高められる。また、成形面の二次元的な剛体シェル要素モデルを用いてシミュレーションを行うことで、金型の三次元的なソリッド要素モデルを用いる場合と比べて、計算負荷が格段に小さくなるため、計算時間が大幅に短縮される。 As described above, in the present invention, the forming stroke process is divided into a plurality of stages, and a forming simulation is performed using a rigid body shell element model of the forming surface (a rigid body model in which the forming surface is divided into a large number of flat shell elements) in each stage. I do. Specifically, the amount of bending of the molding surface of the mold is calculated from the molding reaction forces in a plurality of stages during the stroke, and a rigid shell element model of the molding surface reflecting the amount of bending in each stage is created. Then, at each stage in the middle of the stroke, by using the rigid body shell element model corresponding to each stage, the bending deformation of the molded surface in the molding stroke process can be reproduced step by step, so that the accuracy of the simulation is improved. .. In addition, by performing the simulation using the two-dimensional rigid shell element model of the molded surface, the calculation load is significantly smaller than when using the three-dimensional solid element model of the mold, so the calculation time Is greatly shortened.

この場合、成形ストロークの途中で、材料モデルと接触して力が釣り合った第1の成形面の剛体シェル要素モデルを、形状(撓み量)の異なる第2の成形面の剛体シェル要素モデルに入れ替える必要がある。このように成形面の剛体シェル要素モデルを入れ替えると、材料モデルと成形面の剛体シェル要素モデルとの位置関係(接触状態)が突然変化し、両者の間の力の釣り合いが崩れるため、両者の接触の連続性を維持しながら成形シミュレーションを続行することが困難となる。 In this case, in the middle of the forming stroke, the rigid shell element model of the first forming surface in which the force is balanced in contact with the material model is replaced with the rigid shell element model of the second forming surface having a different shape (deflection amount). There is a need. When the rigid shell element model of the molded surface is replaced in this way, the positional relationship (contact state) between the material model and the rigid shell element model of the molded surface suddenly changes, and the balance of forces between the two is lost. It becomes difficult to continue the molding simulation while maintaining the continuity of contact.

そこで、本発明では、上記のように、第1の成形面の剛体シェル要素モデルで材料モデルを成形しながら、第2の成形面の剛体シェル要素モデルが第1の成形面の剛体シェル要素モデルを追い抜いて材料モデルを成形するシミュレーションを行う。シミュレーションでは、各成形面同士の接触は考慮しないため、上記のような実際にはあり得ない状況でのシミュレーションが可能である。これにより、第1の成形面の剛体シェル要素モデルと材料モデルとの力の釣り合いや相対的な位置関係を維持しながら、第1の成形面の剛体シェル要素モデルから第2の成形面の剛体シェル要素モデルに材料モデルを徐々に受け渡すことができる。これにより、各段階の成形面の剛体シェル要素モデルと材料モデルとの接触の不連続性の問題が解消されるため、複数の段階における撓み変形を考慮した成形面の剛体シェル要素モデルによる成形シミュレーションが可能となる。 Therefore, in the present invention, as described above, the rigid shell element model of the second molding surface is the rigid shell element model of the first molding surface while the material model is molded by the rigid shell element model of the first molding surface. Perform a simulation to overtake and form a material model. Since the simulation does not consider the contact between the molded surfaces, it is possible to perform the simulation in the above-mentioned situation that is not actually possible. As a result, the rigid body of the first molded surface to the rigid body of the second molded surface are maintained while maintaining the force balance and relative positional relationship between the rigid shell element model of the first molded surface and the material model. The material model can be gradually passed to the shell element model. This solves the problem of contact discontinuity between the rigid shell element model of the molded surface at each stage and the material model, so molding simulation using the rigid shell element model of the molded surface considering bending deformation at multiple stages. Is possible.

上記の成形シミュレーション方法において、例えば、材料モデルを成形している第1の成形面の剛体シェル要素モデルを停止させた後、第2の成形面の剛体シェル要素モデルが第1の成形面の剛体シェル要素モデルを追い抜いて材料モデルと接触すると、第1の成形面の剛体シェル要素モデルを停止させるときや、第2の成形面の剛体シェル要素モデルが材料モデルに接触する際に、材料モデルが慣性力の影響で変形するため、シミュレーションの精度が低下するおそれがある。そこで、第1及び第2の成形面の剛体シェル要素モデルを共に移動させながら、第2の成形面の剛体シェル要素モデルが第1の成形面の剛体シェル要素モデルを追い抜いて材料モデルを受け渡すことが好ましい。 In the above molding simulation method, for example, after stopping the rigid shell element model of the first molding surface forming the material model, the rigid shell element model of the second molding surface is the rigid body of the first molding surface. When the shell element model is overtaken and comes into contact with the material model, the material model causes the material model to stop when the rigid shell element model of the first molding surface is stopped or when the rigid shell element model of the second molding surface comes into contact with the material model. Since it is deformed by the influence of inertial force, the accuracy of the simulation may decrease. Therefore, while moving the rigid shell element model of the first and second molding surfaces together, the rigid shell element model of the second molding surface overtakes the rigid shell element model of the first molding surface and delivers the material model. Is preferable.

以上のように、本発明によれば、成形ストローク過程の複数段階における撓み変形を考慮した複数の成形面の剛体シェル要素モデルを用いて、各段階の成形面の剛体シェル要素モデルと材料モデルとの接触の連続性を維持しながら、成形シミュレーションを行うことが可能となる。このように金型の撓み変形を踏まえることで、シミュレーションの精度が高められる。また、成形面の剛体シェル要素モデルを用いることで、金型のソリッド要素モデルを用いる場合よりも計算負荷が軽減されるため、計算時間が短くなる。 As described above, according to the present invention, the rigid shell element model and the material model of the molding surface of each stage are used by using the rigid shell element model of a plurality of molding surfaces considering the bending deformation in a plurality of stages of the molding stroke process. It is possible to perform molding simulation while maintaining the continuity of contact. By taking into account the bending deformation of the mold in this way, the accuracy of the simulation can be improved. Further, by using the rigid shell element model of the molded surface, the calculation load is reduced as compared with the case of using the solid element model of the mold, so that the calculation time is shortened.

プレス成形金型の断面図である。It is sectional drawing of the press molding die. 成形シミュレーションを用いた金型の撓み解析方法のフロー図である。It is a flow chart of the bending analysis method of a mold using a molding simulation. 図1の金型の成形面の剛体シェル要素モデルの斜視図である。It is a perspective view of the rigid shell element model of the molding surface of the mold of FIG. (A)〜(C)は、成形ストローク過程の各段階における撓み変形を反映させた上型の成形面の剛体シェル要素モデルの断面図である。(A) to (C) are cross-sectional views of a rigid shell element model of the molding surface of the upper mold reflecting the bending deformation at each stage of the molding stroke process. (A)〜(C)は、第1の剛体シェル要素モデルから第2の剛体シェル要素モデルに材料モデルを受け渡す様子を概念的に示す断面図である。(A) to (C) are cross-sectional views conceptually showing how the material model is passed from the first rigid body shell element model to the second rigid body shell element model.

以下、本発明の実施の形態を図面に基づいて説明する。 Hereinafter, embodiments of the present invention will be described with reference to the drawings.

本実施形態では、金属板(ブランク材)に絞り成形を施す場合のシミュレーション方法について説明する。絞り成形は、図1に示すように、上型(ダイ)1とブランクホルダ2とでワークWを挟持した状態で、これらを降下させてワークWを下型(パンチ)3に押し付けることにより、ワークWを引き延ばして所定の形状に成形することで行われる。 In this embodiment, a simulation method in the case of drawing and forming a metal plate (blank material) will be described. As shown in FIG. 1, the draw forming is performed by holding the work W between the upper die (die) 1 and the blank holder 2 and lowering them to press the work W against the lower die (punch) 3. This is done by stretching the work W and forming it into a predetermined shape.

上記のような絞り成形を実際に行う前に、コンピュータを用いた成形シミュレーションによる解析を行い、その解析結果に基づいて金型の形状や加工条件の調整を行うことで、成形精度の向上が図られる。本実施形態では、図2に示す手順に従って解析が行われる。以下、各手順を詳しく説明する。 Before actually performing drawing molding as described above, analysis is performed by molding simulation using a computer, and the shape of the mold and processing conditions are adjusted based on the analysis results, thereby improving the molding accuracy. Be done. In this embodiment, the analysis is performed according to the procedure shown in FIG. Each procedure will be described in detail below.

まず、材料に関するデータ(例えば、金属板の材質や板厚)、加工条件に関するデータ(例えば成形荷重)、金型の成形面に関するデータ等をコンピュータに入力する。金型の成形面に関するデータとしては、金型の成形面の剛体シェル要素モデルが作成される。具体的には、図3に示すように、上型の成形面(下面)の剛体シェル要素モデル10と、ブランクホルダ2の押さえ面(上面)の剛体シェル要素モデル20と、下型の成形面(上面)の剛体シェル要素モデル30とを作成する。これらの材料のデータ、加工条件のデータ、成形面のデータ(剛体シェル要素モデル10,20,30)を用いて、ワークWの弾性体モデル(材料モデルM)の成形シミュレーションを行う。 First, data on materials (for example, material and thickness of a metal plate), data on processing conditions (for example, molding load), data on the molding surface of a mold, and the like are input to a computer. As data on the molding surface of the mold, a rigid shell element model of the molding surface of the mold is created. Specifically, as shown in FIG. 3, a rigid shell element model 10 on the molding surface (lower surface) of the upper mold, a rigid shell element model 20 on the holding surface (upper surface) of the blank holder 2, and a molding surface of the lower mold. A rigid shell element model 30 (upper surface) is created. Using the data of these materials, the data of the processing conditions, and the data of the forming surface (rigid body shell element models 10, 20, 30), the forming simulation of the elastic body model (material model M) of the work W is performed.

上記の成形シミュレーションにより、材料モデルMに生じるひずみ及び内部応力や、金型に加わる加工反力が取得される。材料モデルMに生じるひずみや内部応力等から、ワークにワレやシワが生じるか否かを解析することができ、この解析結果に基づいて、材料、加工条件、成形面の形状等が修正される。 By the above molding simulation, the strain and internal stress generated in the material model M and the machining reaction force applied to the mold are acquired. From the strain and internal stress generated in the material model M, it is possible to analyze whether or not cracks or wrinkles occur in the work, and based on this analysis result, the material, processing conditions, shape of the molded surface, etc. are corrected. ..

また、金型に加わる加工反力と、金型構造に関する情報とから、金型の撓み解析を行う。金型構造に関する情報としては、例えば、金型の弾性体ソリッド要素モデルを使用できる。この撓み解析により、加工反力による金型の成形面の撓み量を取得することができる。本実施形態では、成形ストローク過程(本実施形態では上型1を降下させる過程)の複数の段階における金型の成形面の撓み量を取得する。尚、金型の成形面の撓み変形は、そのほとんどが成形ストローク過程の終期(上型1の下死点付近)で生じるため、下死点直前の複数の段階における成形面の撓み量を取得することが好ましい。 In addition, the bending analysis of the mold is performed from the processing reaction force applied to the mold and the information on the mold structure. As information on the mold structure, for example, an elastic solid element model of the mold can be used. By this deflection analysis, the amount of deflection of the molded surface of the mold due to the machining reaction force can be obtained. In the present embodiment, the amount of bending of the molding surface of the mold at a plurality of stages of the molding stroke process (the process of lowering the upper mold 1 in the present embodiment) is acquired. Since most of the bending deformation of the molding surface of the mold occurs at the end of the molding stroke process (near the bottom dead center of the upper mold 1), the amount of bending of the molding surface at a plurality of stages immediately before the bottom dead center is obtained. It is preferable to do so.

具体的には、例えば、図3に示す成形ストローク過程の第1段階a、第2段階b、及び第3段階cのそれぞれの所定の時期(例えば始点)における加工反力を算出する。この算出結果に基づいて、図4(A)〜(C)に誇張して示すように金型の成形面(例えば上型1の成形面)の撓み量を算出する。通常、加工ストロークが進行するにつれて加工反力が大きくなり、これに伴って成形面の撓み量が大きくなる。そして、各段階における撓み量を上型1の成形面の剛体シェル要素モデル10に反映させて、第1段階aにおける撓み量を反映させた第1の成形面の剛体シェル要素モデル10A(以下、「第1の成形面モデル10A」と言う。)、第2段階bにおける撓み量を反映させた第2の成形面の剛体シェル要素モデル10B(以下、「第2の成形面モデル10B」と言う。)、及び第3段階cにおける撓み量を反映させた第3の成形面の剛体シェル要素モデル10C(以下、「第3の成形面モデル10C」と言う。)を作成する(図2の矢印X参照)。 Specifically, for example, the machining reaction force at each predetermined time (for example, starting point) of the first step a, the second step b, and the third step c of the molding stroke process shown in FIG. 3 is calculated. Based on this calculation result, the amount of bending of the molding surface of the mold (for example, the molding surface of the upper mold 1) is calculated as shown in exaggeratedly shown in FIGS. 4 (A) to 4 (C). Normally, as the machining stroke progresses, the machining reaction force increases, and the amount of deflection of the molded surface increases accordingly. Then, the amount of bending in each stage is reflected in the rigid shell element model 10 of the molding surface of the upper mold 1, and the rigid shell element model 10A of the first molding surface reflecting the amount of bending in the first stage a (hereinafter, hereinafter, It is referred to as a "first molding surface model 10A"), and a rigid shell element model 10B of the second molding surface reflecting the amount of deflection in the second stage b (hereinafter referred to as a "second molding surface model 10B"). ), And a rigid shell element model 10C of the third molded surface (hereinafter referred to as “third molded surface model 10C”) reflecting the amount of deflection in the third step c is created (arrow in FIG. 2). See X).

次に、各段階の成形面モデル10A〜10Cを用いて、再び成形シミュレーションを行う。具体的には、図3に示すように、第1段階aでは、第1の成形面モデル10Aで材料モデルMを成形する。尚、図3の各成形面モデル10A〜10Cのストロークを示す矢印において、実線矢印は材料モデルMと接触した状態を示し、点線矢印は材料モデルMと接触していない状態を示す。 Next, the molding simulation is performed again using the molding surface models 10A to 10C of each stage. Specifically, as shown in FIG. 3, in the first step a, the material model M is molded by the first molding surface model 10A. In the arrows showing the strokes of the molded surface models 10A to 10C in FIG. 3, the solid line arrow indicates the state of contact with the material model M, and the dotted line arrow indicates the state of not contacting the material model M.

そして、第1段階aから第2段階bへの移行期では、第1の成形面モデル10Aで材料モデルMを成形しながら、第2の成形面モデル10Bが第1の成形面モデル10Aを追い抜く。成形シミュレーションでは、成形面モデル同士の接触は考慮しないため、上記のように、第2の成形面モデル10Bが第1の成形面モデル10Aを透過して材料モデルMに接触することが可能である。 Then, in the transition period from the first stage a to the second stage b, the second molding surface model 10B overtakes the first molding surface model 10A while molding the material model M with the first molding surface model 10A. .. Since the contact between the molding surface models is not considered in the molding simulation, the second molding surface model 10B can pass through the first molding surface model 10A and come into contact with the material model M as described above. ..

具体的には、図5(A)に示すように、第1段階aでは、第1の成形面モデル10A(鎖線)のみが材料モデルMに接触してこれを成形する。一方、第2の成形面モデル10B(点線)は、第1の成形面モデル10Aの背後(図中上方)で、第1の成形面モデル10Aと同じ方向に移動している。このとき、両成形面モデル10A,10Bは、ほぼ同速度で移動している(Va≒Vb)。 Specifically, as shown in FIG. 5A, in the first step a, only the first molding surface model 10A (chain line) comes into contact with the material model M to mold it. On the other hand, the second molding surface model 10B (dotted line) moves behind the first molding surface model 10A (upper part in the drawing) in the same direction as the first molding surface model 10A. At this time, both the molded surface models 10A and 10B are moving at substantially the same speed (Va≈Vb).

その後、第1の成形面モデル10Aの速度を徐々に落とすことで(Va<Vb)、図5(B)に示すように、第2の成形面モデル10Bが、第1の成形面モデル10Aを追い抜き始める。これにより、第2の成形面モデル10Bの一部が、第1の成形面モデル10Aよりも材料モデルM側(図中下方)に突出し、材料モデルMに、第1の成形面モデル10A及び第2の成形面モデル10Bの双方が同時に接触する。すなわち、移行期では、第1の成形面モデル10Aと第2の成形面モデル10Bとが協働して材料モデルMを成形する。 Then, by gradually reducing the speed of the first molding surface model 10A (Va <Vb), as shown in FIG. 5 (B), the second molding surface model 10B makes the first molding surface model 10A. Start overtaking. As a result, a part of the second forming surface model 10B protrudes toward the material model M side (lower in the figure) from the first forming surface model 10A, and the material model M has the first forming surface model 10A and the first forming surface model 10A. Both of the molded surface models 10B of 2 come into contact at the same time. That is, in the transition period, the first forming surface model 10A and the second forming surface model 10B cooperate to form the material model M.

その後、図5(C)に示すように、第2の成形面モデル10Bが第1の成形面モデル10Aを完全に追い抜く。これにより、材料モデルMが第2の成形面モデル10Bに受け渡され、第2の成形面モデルBのみで材料モデルMが成形される(第2段階b)。第1の成形面モデル10Aは、第2の成形面モデル10Bに材料モデルMを受け渡した後、停止させる(あるいは消失させてもよい)。 Then, as shown in FIG. 5C, the second forming surface model 10B completely overtakes the first forming surface model 10A. As a result, the material model M is passed to the second forming surface model 10B, and the material model M is formed only by the second forming surface model B (second step b). The first molding surface model 10A is stopped (or may be eliminated) after the material model M is delivered to the second molding surface model 10B.

このように、第2の成形面モデル10Bが第1の成形面モデル10Aを追い抜くことで、各段階の成形面モデル10A,10Bと材料モデルMとの位置関係や力の釣り合いを維持しながら、第1の成形面モデル10Aから第2の成形面モデル10Bに材料モデルMを徐々に受け渡すことができる。これにより、各段階の成形面モデル10A,10Bと材料モデルとの接触の連続性が維持されるため、各段階の撓み量を反映した成形面モデルによる成形シミュレーションが可能となり、シミュレーションの精度が高められる。また、成形面の剛体シェル要素モデルを用いてシミュレーションを行うことで、金型の弾性体ソリッド要素モデルを用いる場合と比べて計算負荷が格段に軽減されるため、計算時間が大幅に短縮される。 In this way, the second forming surface model 10B overtakes the first forming surface model 10A, so that the positional relationship and the force balance between the forming surface models 10A and 10B and the material model M at each stage are maintained. The material model M can be gradually passed from the first molding surface model 10A to the second molding surface model 10B. As a result, the continuity of contact between the molding surface models 10A and 10B at each stage and the material model is maintained, so that molding simulation using the molding surface model that reflects the amount of deflection at each stage becomes possible, and the accuracy of the simulation is improved. Be done. In addition, by performing the simulation using the rigid shell element model of the molded surface, the calculation load is significantly reduced compared to the case of using the elastic solid element model of the mold, so the calculation time is significantly shortened. ..

また、上記のように、第1の成形面モデル10Aと第2の成形面モデル10Bとを共に移動させながら、第1の成形面モデル10Aから第2の成形面モデル10Bに材料モデルMを受け渡すことにより、材料モデルMに働く慣性力が抑えられるため、シミュレーションの精度がさらに高められる。 Further, as described above, while moving the first molding surface model 10A and the second molding surface model 10B together, the material model M is received from the first molding surface model 10A to the second molding surface model 10B. By passing the material model M, the inertial force acting on the material model M is suppressed, so that the accuracy of the simulation is further improved.

その後、第2段階bから第3段階cへの移行期では、第3の成形面モデル10Cが第2の成形面モデル10Bを追い抜くことで、第2の成形面モデル10Bから第3の成形面モデル10Cに材料モデルMが受け渡される。この移行期における詳細は、上記の第1段階aから第2段階bへの移行期と同様であるため、説明を省略する。そして、第3の成形面モデル10Cが下死点に達して停止することで、材料モデルMの成形が完了する。 After that, in the transition period from the second stage b to the third stage c, the third forming surface model 10C overtakes the second forming surface model 10B, so that the second forming surface model 10B to the third forming surface are overtaken. The material model M is delivered to the model 10C. Since the details in this transition period are the same as those in the transition period from the first stage a to the second stage b described above, the description thereof will be omitted. Then, when the third molding surface model 10C reaches the bottom dead center and stops, the molding of the material model M is completed.

こうして得られた成形シミュレーションの算出結果から、金型に加わる成形反力を取得し、この加工反力と金型構造(金型の弾性体ソリッド要素モデル)とから、再び金型の撓み解析を行う。特に、撓み量が最も大きい下死点における撓み解析を行う。こうして得られた金型の撓み解析結果は、成形ストローク過程における撓み変形を段階的に再現した成形面に基づいているため、撓み変形を全く考慮していない成形面に基づいて算出した最初の撓み解析結果よりも精度が高い。そして、上記の撓み量を見込んで、金型の形状(特に成形面)の寸法修正を行う。具体的には、例えば、上記の成形シミュレーションで得られた下死点における撓み量の分だけ、金型の成形面を、撓みが生じる方向と反対側に変位させる。これにより、成形反力による金型の成形面の撓みの影響を相殺することができるため、より精度の高いプレス成形が可能となる。 From the calculation result of the molding simulation obtained in this way, the molding reaction force applied to the mold is obtained, and the bending analysis of the mold is performed again from this processing reaction force and the mold structure (elastic solid element model of the mold). conduct. In particular, the deflection analysis at the bottom dead center where the amount of deflection is the largest is performed. Since the bending analysis result of the mold obtained in this way is based on the molding surface in which the bending deformation in the molding stroke process is reproduced stepwise, the first bending calculated based on the molding surface in which the bending deformation is not considered at all. The accuracy is higher than the analysis result. Then, in anticipation of the above-mentioned amount of bending, the dimensions of the mold shape (particularly the molding surface) are corrected. Specifically, for example, the molding surface of the mold is displaced to the side opposite to the direction in which the bending occurs by the amount of bending at the bottom dead center obtained in the above molding simulation. As a result, the influence of the bending of the molding surface of the mold due to the molding reaction force can be offset, so that press molding with higher accuracy becomes possible.

本発明は、上記の実施形態に限られない。例えば、上記の実施形態では、成形ストローク過程の各段階における撓み変形を反映させた上型1の成形面の剛体シェル要素モデルを用いて成形シミュレーションを行う場合を示したが、これに限らず、成形ストローク過程の各段階における撓み変形を反映させた下型3の成形面の剛体シェル要素モデルを用いて上記と同様の成形シミュレーションを行うこともできる。また、上記の実施形態では、成形完了直前の3段階で撓み解析を行う場合を示したが、これを2段階、あるいは4段階以上としてもよい。また、上記の成形シミュレーションは、絞り加工に限らず、曲げ加工、張り出し加工、鍛造加工等の、各種プレス成形のシミュレーションに適用することができる。 The present invention is not limited to the above embodiments. For example, in the above embodiment, the case where the molding simulation is performed using the rigid shell element model of the molding surface of the upper mold 1 reflecting the bending deformation at each stage of the molding stroke process is not limited to this. A molding simulation similar to the above can also be performed using a rigid shell element model of the molding surface of the lower mold 3 that reflects the bending deformation at each stage of the molding stroke process. Further, in the above embodiment, the case where the deflection analysis is performed in three stages immediately before the completion of molding is shown, but this may be two stages or four or more stages. Further, the above molding simulation can be applied not only to drawing but also to various press molding simulations such as bending, overhanging, and forging.

1 上型
2 ブランクホルダ
3 下型
10 上型の成形面の剛体シェル要素モデル
10A 第1段階における撓み変形を考慮した上型の成形面の剛体シェル要素モデル
10B 第2段階における撓み変形を考慮した上型の成形面の剛体シェル要素モデル
10C 第3段階における撓み変形を考慮した上型の成形面の剛体シェル要素モデル
20 ブランクホルダの押さえ面の剛体シェル要素モデル
30 下型の成形面の剛体シェル要素モデル
M 材料モデル
1 Upper mold 2 Blank holder 3 Lower mold 10 Rigid body shell element model 10A of the upper mold molding surface Considering the bending deformation of the upper mold molding surface Rigid body shell element model 10B Considering the bending deformation in the second stage Rigid body shell element model of the upper mold molding surface 10C Rigid body shell element model of the upper mold molding surface considering the bending deformation in the third stage 20 Rigid body shell element model of the holding surface of the blank holder 30 Rigid body shell of the lower mold molding surface Element model M Material model

Claims (2)

プレス成形のシミュレーション方法であって、
成形ストローク過程の複数の段階における金型の成形面の撓み量を算出するステップと、
各段階における撓み量を反映した複数の成形面の剛体シェル要素モデルを作成するステップと、
ある段階の撓み量を反映した第1の成形面の剛体シェル要素モデルで材料モデルを成形しながら、次の段階の撓み量を反映した第2の成形面の剛体シェル要素モデルが、前記第1の成形面の剛体シェル要素モデルを追い抜いて前記材料モデルを成形するシミュレーションを行うステップとを備えたプレス成形のシミュレーション方法。
It is a simulation method of press molding.
A step of calculating the amount of bending of the molding surface of the mold at multiple stages of the molding stroke process, and
Steps to create a rigid shell element model of multiple molded surfaces that reflect the amount of deflection at each stage,
While molding the material model with the rigid shell element model of the first molding surface that reflects the amount of deflection at a certain stage, the rigid shell element model of the second molding surface that reflects the amount of deflection at the next stage is the first A method for simulating press molding, which comprises a step of overtaking a rigid shell element model of a molding surface and performing a simulation of molding the material model.
前記第1の成形面の剛体シェル要素モデル及び前記第2の成形面の剛体シェル要素モデルが共に移動しながら、前記第2の成形面の剛体シェル要素モデルが前記第1の成形面の剛体シェル要素モデルを追い抜く請求項1に記載のプレス成形のシミュレーション方法。 While the rigid shell element model of the first molding surface and the rigid shell element model of the second molding surface move together, the rigid shell element model of the second molding surface moves the rigid shell element model of the first molding surface. The method for simulating press molding according to claim 1, wherein the element model is overtaken.
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