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Metal Forming

A Numerical Approach to Robust In-Line Control of Roll Forming Processes

J.H. Wiebenga1), M. Weiss2), B. Rolfe3), A.H. van den Boogaard4)

1)

Materials innovation institute (M2i), Delft, the Netherlands, J.Wiebenga@M2i.nl; 2) Centre for Material and Fibre Innovation, Deakin University, Waurn Ponds, Australia, Matthias.Weiss@Deakin.edu.au; 3) School of Engineering, Deakin University, Waurn Ponds, Australia, Ber-nard.Rolfe@Deakin.edu.au; 3) Engineering Technology, University of Twente, Enschede, the Netherlands, A.H.vandenBoogaard@utwente.nl;

Abstract. The quality of roll formed products is known to be highly sensitive and dependent on the process parameters and thus the unavoidable variations of these parameters during mass production. To maintain a constant high product quality, a new roll former with an adjustable final roll forming stand is developed at Deakin University enabling the continuous compensation for possible shape defects. In this work, a numerical approach to robust line control of the roll forming of a V-section profile is presented, combining the aspects of robust process design and in-line compensation methods. A numerical study is performed to determine the relationship between controllable process settings and uncontrolla-ble variation of incoming material properties with respect to the common product defects longitudinal bow and springback. The computationally expensive non-linear FE simulations used in this study are subsequently replaced by metamodels based on efficient Single Response Surfaces. Using these metamodels, the optimal setting for the adjustable stand is determined with robust optimization techniques and the effect on product quality analyzed. It is shown that the subsequent adjustment of the final roll stand position leads to a significantly improved product quality by preventing product defects and minimizing the deteriorating effects of scattering variables.

Keywords: Roll forming, Finite Element Method, Process variables, Variation, Robustness, In-line control

1. INTRODUCTION

Cold roll forming is a common and efficient metal forming process for the production of constant-profile parts with high geometrical accuracy, high lengths and in large quantities. A strip of material is hereby formed through successive pairs of rolls, each applying an incre-mental part of the bend. The materials deformation beha-vior during the bending process is highly complex. In addition to longitudinal elongation, longitudinal bending, transverse bending and shear, undesirable strains are generated in the sheet. These strains or redundant defor-mations are known to cause product defects like longitu-dinal bow, twist or springback [1-2].

Next to the process design, the quality of the final product is known to be highly sensitive to the material properties and the unavoidable variations of these proper-ties during mass production, see e.g. [3]. With an increas-ing usage of Advanced High Strength Steels (AHSS) in recent years, these aspects have become even more criti-cal. Compared to milder steel grades, the combination of reduced formability and larger variations of material properties makes it even more difficult to control the product quality when roll forming AHSS.

In this work, a first approach to robust in-line control of the roll forming of a V-section profile is presented. The goal of this research is to develop a method for the com-pensation of product defects by combining the aspects of robust process design [4] and in-line compensation me-thods [1, 5]. Therefore, a roll forming process is devel-oped at Deakin University with an adjustable final stand. This stand facilitates the re-adjustment of the bottom and top roll by intelligent in-line control. This will enable continuous compensation for possible shape defects throughout the production process.

As a first approach, a numerical study is performed to determine the relationship between controllable process settings and uncontrollable variation of incoming material

properties with respect to the common product defects longitudinal bow and springback. The considered V-section product and accompanying roll forming process are introduced in Section 2. The computationally expen-sive non-linear FE simulations used in this study are subsequently replaced by metamodels, see Section 3. Us-ing these surrogate models, the optimal settUs-ings for the adjustable stand are determined using robust optimization techniques and the effect on product quality analyzed. Section 4 presents the conclusions and recommendations for future work.

2. ROLL FORMING PROCESS V-SECTION

2.1. FE model

FE simulations are used to determine the relationships between controllable process settings and uncontrollable variation of incoming material properties with respect to the product defects. Figure 1 presents the geometry of the V-section profile used in this academic study and the accompanying flower pattern design with a total bending angle of 80°and an inner bending radius of 15 mm.

Figure 1. Flower pattern of the V-section profile

A schematic of the roll forming process is given in Figure 2, COPRA FEA has been used as FE code. The product is formed by five stands, each applying a bending angle of 10°. Due to symmetry, only half of the sheet is modeled and subsequently discretized using solid ele-ments with 1 element through the thickness. Increasing

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Metal Forming

this number hardly affected the numerical outcomes but did significantly increase the calculation time. The rolls, with an inter-distance of 305 mm, are modeled using an analytical rigid surface description. One simulation of the frictionless roll forming of a 2000 mm pre-cut strip takes about 9 hours on a 3.5 GHz Intel Xeon processor with 16 GB RAM memory.

Figure 2. Schematic of the roll forming process 2.2. Variation modeling

The material used in this study is the AHSS Dual Phase (DP) 780. Hooke’s law and Swift’s isotropic strain hardening law are adopted as material models, see Equa-tion (1) and (2) respectively. The nominal material prop-erties and resulting coefficients for the Swift hardening law are listed in the second column of Table 1. The scat-ter of the mascat-terial properties around their mean values is based on the work presented in [6, 7] and given in the remainder of Table 1. The material properties are as-sumed to vary according to a normal distribution where the scatter is defined in terms of the standard deviation. In order to accurately represent the true scatter of the DP material and to prevent overestimation of the response variation, a linear correlation between the yield stress (σy)

and the ultimate tensile stress (Rm) is adopted as reported

in [6, 7]. The strain hardening exponent (n) remains con-stant at 0.138 from which the hardening coefficient (K) can be calculated using Rm, see Equation (3).

e σ = (1) n p y K(ε0 ε ) σ = + (2) n m n n R K= exp( ) (3)

Table 1. Material properties and variation

Parameter Mean (µ) Std. Dev. (σ) Min. (µ-3σ) Max. (µ+3σ) t 2 mm 0.01 mm 1.97 mm 2.03 mm σy 586 MPa 13 MPa 547 MPa 625 MPa Rm 894 MPa 20 MPa 834 MPa 953 MPa K 1349 MPa 30 MPa 1259 MPa 1439 MPa ε0 0.0024

E 210 MPa

2.3. Process control

To enable product defect compensation, a new roll former with an adjustable final roll forming stand is de-veloped. See Figure 2. This stand facilitates the re-adjustment of the roll gap (D) by vertically adjusting the

top roll, the vertical alignment (H) of the final roll stand and the inter-distance (L) between the final two roll stands. The nominal settings and Upper and Lower Speci-fication Limits (denoted as USL and LSL respectively) of the control variables are given in Table 2.

Table 2. Nominal, lower and upper specification limits of the control variables

Parameter Nominal LSL USL

H 0 mm -5 mm 10 mm

L 305 mm 205 mm 405 mm D 2 mm 1.8 mm 2.5 mm

3. ROBUST IN-LINE CONTROL

3.1. Strategy

To enable continuous compensation for possible shape defects throughout the production process, changes to the process set up have to be made according to a model. The basis for this model is created in this study using FE si-mulations. The non-linear simulations are very time-consuming and unsuitable for direct use in an in-line control system. Therefore, these simulations are replaced by metamodels based on the Response Surface Methodol-ogy (RSM). The resulting RSM models enable very fast evaluation with which the action taken by the system can be calculated based on a combined measurement of the input and output of the model.

The approach applied in this work for the creation of metamodels and robust optimization is presented in [8] and shortly outlined next. As a first step, the objective, constraints, control variables and noise variables of the problem under consideration are defined and quantified. The noise variables and control variables (x) have been discussed and quantified in Section 2.2 and Section 2.3 respectively. The main product defects for the V-shaped product are longitudinal bow and springback. The former defect is defined as the maximum height deviation from a straight product, over the length of the strip. The latter defect is defined as the angle difference between the measured product angle and the required angle of 80°, see Figure 1. The deformed front and end part of the product are often removed by cutting. Therefore, the objective of this study is to optimize the product dimensional quality by minimizing the longitudinal bow and centre spring-back. The longitudinal bow is hereby taken into account as the objective function f while satisfying ±3σ-constraints on the centre springback (CS) angle where the USL and LSL is chosen 2° and -2° respectively. The quantified robust optimization formulation is now given by:

find x min µf ±3σf s.t. −2≤µcs±3σcs ≤2 −5≤H ≤10 (4) 205≤L≤405 1.8≤D≤2.5 t~N(2,0.012) ~N(586,132) y σ

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Metal Forming

The next step is the creation of metamodels of the lon-gitudinal bow and springback. At the basis of the RSM model is a Design Of Experiment (DOE) plan in the com-bined control–noise variable space. A DOE is created based on a space-filling Latin Hypercube Design (LHD) combined with a Full Factorial Design (FFD). The num-ber of DOE points is chosen equal to 10 times the numnum-ber of variables [9], i.e. 50 simulations.

After running the FE simulations corresponding to the settings specified by the DOE, the longitudinal bow, strain and springback at the front, centre and end of the product are extracted from the FE results. The numerical strain measurements are taken halfway the length of the strip at 1.5 mm away from the outer edge, see Figure 1. A single metamodel is subsequently fitted in the combined design space. Since the shape and complexity of the re-sponse behavior in the design space is unknown before-hand, different types of RSM models are fitted for creat-ing a set of approximate models. The performance of each metamodel is subsequently estimated using ANalysis Of VAriance (ANOVA) techniques [10]. The level of fit of each metamodel is calculated and used to select the most accurate metamodel with respect to the FE model re-sponse. The ANOVA results for the different responses are presented in Table 3. For each response, a full qua-dratic response surface (containing linear, interaction and quadratic terms) resulted in the most accurate fit.

Howev-er, no clear trend is found for the longitudinal strain which is reflected by the poor metamodel fit quality, i.e.

R2 < 0.8. Based on this result, the longitudinal strain is assessed unsuitable for use in the robust optimization procedure.

Two approximate models of the response mean µf and standard deviation σfare extracted from the single meta-model. This is done for each response, providing the re-quired statistical measures for the robust optimization procedure. This can be done analytically in case of a RSM metamodel, see [10]. Both models can now be used for robust optimization by applying a global optimization algorithm to solve Equation (4). The procedure as de-scribed above is implemented and solved by the optimiza-tion software OPTFORM developed at the University of Twente [8].

Table 3. ANalysis Of VAriance (ANOVA) results for the best RSM metamodel fit of each response

Response RSM model R2

Longitudinal bow f Full quadratic 0.96 Longitudinal strain g1 Full quadratic 0.71 Front springback g2 Full quadratic 0.99 Centre springback g3 Full quadratic 0.98 End springback g4 Full quadratic 0.98

Figure 3. Effect of control and noise variables on longitudinal bow height

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Metal Forming

3.2. Metamodel results

Impressions of the longitudinal bow and springback metamodels are shown in Figure 3 and Figure 4 respec-tively. The longitudinal bow and springback at the front, centre and end of the product are plotted as a function of the control variables. For visualization purposes, the re-maining variables are set to their nominal process settings as reported in the second column of Table 2. The vertical bars represent the ±3σ bounds of bow and springback variation around the mean value caused by the influence of the noise variables.

Evaluating the shape of the models in Figure 3, a de-crease of the longitudinal bow is observed for increasing

H and L. Also the springback angle decreases for a higher

vertical alignment (see Figure 4) but it is unaffected by the inter-distance. Also note that the flanging effect (dif-ference in front-centre and centre-end springback angle) is not affected by any of the control variables while both the longitudinal bow and springback are significantly influenced by the roll gap D. As long as the roll gap D is larger than the nominal material thickness t, the material is only bent between the rolls. This initially results in an increasing bow and springback angle if D > t, after which the effect flattens for a larger D. Once the distance D is smaller than the nominal material thickness, the material is coined between the rolls. Due to the resulting elonga-tion of the products bottom part, both the bow and spring-back is reduced.

Looking at the robustness of the process, a significant variation of longitudinal bow is observed caused by the scatter of the material thickness and yield stress. At the nominal process settings, a ±3σ bow variation of 6.8 mm around the mean value of 10.3 mm can be observed. See Table 4. At this setting, the springback angle at the centre of the product shows a ±3σ variation of 0.57° around the mean value of 4.69°. For varying control variable settings, only minor changes of the robustness are observed.

3.3. Optimal process settings

The set of metamodels are subsequently used for robust optimization, solving Equation (4). The optimal robust process settings and accompanying responses are pre-sented in the last column of Table 4.

Longitudinal bow: By decreasing the depth setting and

increasing the inter-distance and vertical alignment, the mean response of longitudinal bow can be reduced to approximately zero. In other words, longitudinal bow can be fully compensated by adjusting the process settings of the final roll forming stand. Moreover, a 1 mm decrease of bow variation is achieved. However, the scatter of bow around the mean value remains significant. Both the variation of yield stress and material thickness still cause a bow variation of ±5.8 mm.

Springback: Looking at centre springback, a reduction of

4° is achieved at the expense of a slight variation increase of 0.14°. Similar trends can also be observed for the front and end springback angle.

Table 4. Nominal and optimized process settings and corresponding responses

Control variable Norminal setting Optimal setting Vertical alignment H 0 mm 10 mm Inter-distance L 305 mm 390 mm Roll gap D 2 mm 1.94 mm Response µ ± 3σ µ ± 3σ Longitudinal bow f 10.3 ± 6.8 mm -0.2 ± 5.8 mm Front springback g2 0.64° ± 1.06° -3.31° ± 1.30° Centre springback g3 4.69° ± 0.57° 0.68° ± 0.71° End springback g4 6.65° ± 0.53° 4.67° ± 0.77°

4. CONCLUSIONS AND FUTURE WORK

The present numerical study confirms the potential of robust in-line control of roll forming processes. The di-mensional quality of the considered V-shaped product is significantly improved by changing the process settings of the final stand in the adjustable roll former. The longitu-dinal bow, which is considered as one of the main product defects, is fully compensated. Moreover, the sensitivity of bow with respect to scatter of material properties is re-duced. However, the variation of bow around the mean value remains significant. Finally, a significant reduction of 85% for the products centre springback is achieved by application of the robust optimization strategy.

Future work will focus on experimental validation of the numerical trends and the subsequent robust in-line control of the roll forming process.

5. REFERENCES

[1] M. Lindgren: Experimental and computational investigation of the roll forming process, PhD thesis, Luleå University of Technology, Luleå, Sweden (2009)

[2] Halmos GT (ed): Roll forming handbook. Taylor & Francis Group (2006)

[3] Q.V. Bui, J.P. Ponthot: Numerical simulation of cold roll-forming processes, Journal of Materials Processing Technology (2008) 202 (1-3): 275–282

[4] H.G. Beyer, B. Sendhoff: Robust optimization - a comprehensive survey, Journal of Computer Methods in Applied Mechanics and En-gineering (2007) 196:3190–3218

[5] H. Ona, J. Takashi, N. Fukaya: Experiments into the cold roll-forming of straight asymmetrical channels, Journal of Mechanical Working Technology (1983) 8(4):273–291

[6] T. de Souza, B. Rolfe: Characterising material and process variation effects on springback robustness for a semi-cylindrical sheet metal forming process, International Journal of Mechanical Sciences (2010) 52:1756 – 1766

[7] M. Abspoel, M. Scholting, E. Atzema: Characterisation and modelling of the stochastic behaviour of deep drawing steels, Forming Technol-ogy Forum, ETH Zurich, Switserland (2011)

[8] J.H. Wiebenga, A.H. van den Boogaard, G. Klaseboer: Sequential robust optimization of a V-bending process using numerical simula-tions, Journal of Structural and Multidisciplinary Optimization (2012) In press. DOI 10.1007/s00158-012-0761-0

[9] M. Schonlau: Computer experiments and global optimization, PhD Thesis, University of Waterloo, Ontario, Canada (1997)

[10] R.H. Myers, D.C. Montgomery: Response surface methodology, John Wiley & Sons Inc., New York, USA (2002)

Acknowledgement. This research was carried out under the project number M22.1.08303 in the framework of the Research Program of the Materials innovation institute (www.m2i.nl) and was assisted from equipment and resources from the Centre for Material and Fibre Innovation and the Aus-tralian Research Council Linkage project LP0883399.The industrial part-ners co-operating in this research are gratefully acknowledged for their useful contributions to this research.

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