046 Blank Design for a Sheet Product Based on Direct Design Method and FEM Analysis
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Transcript of 046 Blank Design for a Sheet Product Based on Direct Design Method and FEM Analysis
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7/27/2019 046 Blank Design for a Sheet Product Based on Direct Design Method and FEM Analysis
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Blank Design for A Sheet Metal Product Based on Direct Design Method and FEM Analysis
J.W. Yoona
, S.K. Kima
, K. Chungb
J.R Younb
and E.J. Yeonc
aLG Production Engineering Research Center, 19-1 Cheongho-Ri, Jinwuy-Myun,
PyungtaekCity, Kyungki-Do, 451-713, Korea.bSchool of Material Science and Engineering, Seoul National University, 56-1 Shinlim-Dong,
Kwanak-Gu, Seoul, 151-742, Korea.cVCR OBU, LG Electronics, 19-1 Cheongho-Ri, Jinwuy-Myun,
PyungtaekCity, Kyungki-Do, 451-713, Korea.
Abstract
The ideal forming theory was previously developed as a direct design method to guide iterative
design practices by optimizing initial blank shapes in the sheet metal forming process. In this work,
the sequential design method based on the ideal forming theory and FEM analysis was applied to
optimize a practical die design procedure for sheet metal forming. In particular, the design method
was applied to optimize the forming process of complicated sheet metal part (VCR deck chassis)
which is difficult to fabricate without good lubricant. In this sequential method, the ideal forming
theory was used to obtain an initial optimum blank shape which complies with the minimum plastic
work path condition. Based on the solution of the ideal forming theory, the FEM analysis was
iteratively utilized to further optimize the blank shape by taking account the realistic process
condition under the non-lubrication state. The experiment showed that the optimum banks obtained
from the sequential design method can form the final parts without lubrication, confirming that the
proposed sequential design procedure based on the direct design method and FEM analysis can be
successfully applied to optimize the practical die design procedure of sheet metal forming processes.
Keywords: Direct design method, Ideal forming, Optimum blank design, FEM analysis
1.IntroductionIn order to improve conventional trial-and-error based practices for optimizing forming processes,
a direct design method, called the ideal forming theory, has been previously developed [1 - 4]. In
this theory, materials are prescribed to deform following the proportional true strain path (or the
minimum plastic work path for isotropic materials) and the initial blank shape is obtained from a
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one-step backward calculation in which the final sheet product shape is specified. The theory can
be used to determine the ideal initial blank shape needed to best achieve a specified final shape
while resulting in optimum strain distributions. Because of its assumed deformation path, the
result of the theory does not completely comply with real forming so that it is used to guide the
iterative design procedure based on analytic methods.
The blank design procedure based on the ideal forming theory and the iterative applications of the
FEM analysis was shown to be effective [5, 6]. In this sequential design method, as shown in
Fig.1, the optimum blank shape obtained from the direct design method can be effectively used as
good initial guess for incremental analysis codes in order to significantly save computational and
experimental trials in the die design stage. In order to demonstrate the practical used of the
sequential method, the method was applied to design an optimum blank of a complicated VCR
deck chassis in this work. Experiments were also carried out using the optimum blank shape
developed from the sequential method to confirm the validity of the method. The automatic strain
measurement system (ASAME)[7] was also used to measure the formability of the formed part.
Fig.1 Sequential procedure utilizing Fig. 2 Target final shape(VCR deck
the direct design method chassis) to be formed
2.TheoryWhen materials are discretized with meshes and the surface traction is approximated by point
forces, the plastic work is a function of the initial position vectors X and the final position vectors
x:
Direct Design FEM Code
Incremental Analysis Code
Experimental Trials
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)X,x(WW 2,1i3,2,1ie === . (1)
In Equation 1, the value of the effective strain e is dependent on the deformation paths of
material elements and so is the plastic work. In the ideal forming theory, the minimum plastic
work path is imposed for each material. The minimum plastic work path is equivalent to the
proportional true strain path, whose principal directions are restricted to be aligned with specific
material directions for anisotropic materials. However, in the design code, the principal directions
are allowed to be arbitrary. When the proportional true strain path is imposed, the effective strain
in Equation 1, obtained from the effective strain-rate by substituting the rate of deformation
tensor & with the true strain tensor , becomes a function of x and X. In fact, the effective
strain is obtained from the flow theory by applying the deformation theory based on the minimum
plastic work path[8, 9]. When the final sheet product shape is prescribed, the final configuration
is specified so that the plastic work in Equation 1 is a function of X only. Furthermore, the initial
sheet surface on which the initial blank resides is specified in advance. The blank shape is
obtained by optimizing the plastic work [3];i.e.,
2and1ibdVX
)( ioi
eee ==
(2)
where e is the effective stress, Vo is the material volume and bi is the component of a kind of
force vector related to the external force vector. After the initial blank cutout is obtained from
Equation 2, the optimum strain distribution and intermediate shapes of a sheet during forming as
well as nodal force history are obtained under the minimum plastic work path assumption.
3.Results and DiscussionsFig.2 shows the VCR deck chassis on which a VCR head drum is located. The product requires
precise dimensional accuracy for height and slope in order to prevent the distortion of the headdrum when it is placed on the chassis. The process to fabricate this product was newly changed
from die-casting to press forming because of productivity and cost competitiveness. But, when
press forming is employed to make the product, tearing problem is the most difficult obstacle to
overcome because of the severe stretching of this product during the forming process. Fig.3
shows a schematic diagram to design the optimum blank shape using the direct design method
and incremental FEM analysis code. In the figure, the optimum blank shape is predicted by the
direct design method, when the final target shape and initial thickness are specified. Then, FEM
analysis was performed based on the optimum blank to account for the detailed process
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Fig. 3 Sequential design procedure using the direct design method and FEM analysis
Fig.4 Initial blank shapes before and after modifications
conditions, including non-proportional true strain paths, during sheet forming. Fig. 4 shows two
initial blank shapes: a blank previously obtained from 14 times experimental trials and a blank
obtained from seqiential design method. The differences were marked in the figure. In the
present work, the ABAQUS Explicit code [10] was used for the process analysis. In order to
describe no lubricant condition in this process, 0.2 was used for the Coulomb friction coefficient.
In Fig.4, the ideal blank shape obtained from the sequential design method is supposed to best
achieve a specified final shape while resulting in optimum strain distributions. In order to verify
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AAnnaallyyssiiss CCooddee
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< Blank shape obtained by
experimentally before modification >
< Blank shape optimized by
the sequential design method >
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Fig.5 Comparison of forming limit diagrams between before and after modifications
Fig.6 FLD measured by ASAME for the part formed from the modified blank
the optimum blank, incremental analysis code was introduced to perform forming analysis. Fig.5
shows FEM analysis results obtained for the blank experimentally optimized and the blank
optimized, respectively. As shown in the figure, the result obtained from the blank modified using
0
0.2
0.4
0.6
0.8
1
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
FLD(instability)FLD(fracture)Final modification
Ma
jorstrain
Minor strain
0
0.2
0.4
0.6
0.8
1
1.2
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
FLD (fracture)FLD (instability)Original (without lubrication)
Ma
jorstrain
Minor strain
Maximum thickness strain : 0.39
< Blank optimized experimentally > < Blank optimized by sequential design method>
Maximum thickness strain : 0.19
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the sequential design method is in the safe region of FLD and the minimum thickness strain is
improved about 50 % compared to that obtained from the blank experimentally optimized. Finally,
real forming was performed using the optimum blank shape obtained from the sequential design
method to verify the better performance. Fig. 6 shows FLD measured by the automatic strain
measurement system (ASAME). It is shown that the simulation and experimental results are
compatible in Fig.5 and Fig.6, confirming the significantly improved performance of the new blank.
The optimum blank shape has been successfully feed-backed to the mass production line. LG
Electronics produces 5 million pieces of deck chassises per year using the optimum blank shape.
4.ConclusionsPractical application of the sequential design method involving the direct design method was
introduced to design the optimum blank shape of VCR deck chassis when the final target shape,
initial thickness and martial properties are specified. Experimental verification showed that the
new blank optimized using the direct design method and the sequential use of the FEM analysis
significantly better preformed than that previously optimized only experimentally. Therefore, it
was confirmed that the new design method based on the direct design method and FEM analysis
can be useful for the practical blank design procedure.
References
[1] K. Chung & O. Richmond, Int. J. Mech. Sci. 34 (1992) 575-591.
[2] K. Chung & O. Richmond, Int. J. Mech. Sci. 34 (1992) 617-633.
[3] K. Chung, J.W. Yoon and O. Richmond, Int. J. of Plasticity 16 (2000) 595-610.
[4] J.W. Yoon, K. Chung, O. Richmond and F. Barlat, Proceedings of Plasticity2000 (Eds. A.S.
Khan et al.), Neat Press, 2000, p.267.
[5] K. Chung, F. Barlat, J.C. Brem, D.J. Lege & O. Richmond, Int. J. Mech. Sci. 39 (1997) 105-
120.
[6] S.H. Park, J.W. Yoon, D.Y. Yang and Y.H. Kim, Int. J. of Mech. Sci. 41, (1999) 1217-1232.
[7] CamSys Inc., ASAME reference manual, Ver. 3.8, 1995.
[8] K. Chung & O. Richmond, Int. J. of Plasticity 9 (1993) 907-920.
[9] J.W.Yoon, D.Y. Yang and K. Chung, Comp. Methods in Appl. Mech. & Eng. 174 (1999) 23-56.
[10] HKS Inc., ABAQUS/ Exaplicit manual, Ver. 5.8, 1998.
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Figure List
Fig.1 Sequential procedure utilizing the direct design method
Fig.2 Target final shape(VCR deck chassis) to be formed
Fig.3 Sequential design procedure using the direct design method and FEM analysis
Fig.4 Initial blank shapes before and after modifications
Fig.5 Comparison of forming limit diagrams between before and after modifications
Fig.6 FLD measured by ASAME for the part formed from the modified blank
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Fig.1 Sequential procedure utilizing the direct design method
Direct Design FEM Code
Incremental Analysis Code
Experimental Trials
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Fig. 2 Target final shape(VCR deck chassis) to be formed
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Fig. 3 Sequential design procedure using the direct design method and FEM analysis
FFiinnaall TTaarrggeett SShhaappee
DDiirreecctt DDeessiiggnn MMeetthhoodd
((OOppttiimmuumm bbllaannkkddeessiiggnn))
AAnnaallyyssiiss CCooddee
((FFoorrmmiinngg AAnnaallyyssiiss))
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Fig.4 Initial blank shapes before and after modifications
< Blank shape obtained by
experimentally before modification >
< Blank shape optimized by
the sequential design method >
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Fig.5 Comparison of forming limit diagrams between before and after modifications
0
0.2
0.4
0.6
0.8
1
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
FLD(instability)FLD(fracture)Final modification
Majorstrain
Minor strain
0
0.2
0.4
0.6
0.8
1
1.2
-0.6 -0.4 -0.2 0 0.2 0.4 0.6
FLD (fracture)FLD (instability)Original (without lubrication)
Majorstrain
Minor strain
Maximum thickness strain : 0.39
< Blank optimized experimentally > < Blank optimized by sequential design method>
Maximum thickness strain : 0.19
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Fig.6 FLD measured by ASAME for the part formed from the modified blank