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2005 NUMISHEET BENCHMARK 3
 

─ Channel Draw/Cylindrical Cup Benchmark ─

 

The objective of this benchmark is to document the forming characteristics of metals in a two stage process with the first stage dominated by cyclic bending and unbending and the second stage dominated by plane-strain conditions either parallel or perpendicular to the first stage principal strains. In addition to conventional strain and springback measurements, the benchmark will include residual stress measurements through the sheet thickness by neutron diffraction techniques after a deep symmetric channel draw, and an in-situ surface stress measurement under punch load by X-ray diffraction during a subsequent cylindrical cup test on the metal trimmed from the channel wall area.

This benchmark is provided by the General Motors Corporation, Industrial Research and Development Institute (IRDI), the US National Institute of Standards and Technology (NIST), and US Steel Corporation. Tooling for the STAGE 1 forming was made available by the US Auto-Steel Partnership and NIST provided the tooling for STAGE 2. Materials and property measurements are provided by US Steel Corporation and Alcoa, Inc.

 

TOOL GEOMETRY

The simulation process consists of three operations performed in two stages with two separate sets of tools: STAGE 1: binder closure, channel draw, stage 2 blank trimming, STAGE 2: binder closure and cup draw.

 

STAGE 1. Binder Closure and Forming

 

The punch, binder and upper die are illustrated in Figure 1. This shows a side view of the tooling geometry in the x-z plane with symmetry at y=0. Four different blank materials are used for stamping: 1.001 mm DQSK (US Steel), 1.000 mm DP600 (US Steel), 0.800 mm HSLA-50 (Bethlehem Steel) and 0.991 mm AL6022-T43 (Alcoa).

 

Total blank holding force: Kiss blocks shown in Figure 1 and highlighted in Figure 3 are used to hold the binder and upper die to a fixed clearance after binder closure that is 0.42 mm larger than the nominal sheet thickness for all materials. The blank holding force of 637 kN is generated by four 140 mm diameter cylindrical cushions set at 1500 psi. This is sufficient to set the beads and maintain a fixed clearance between the upper die and binder throughout the forming process.

 

Binder Travel: 245 mm final punch depth, see Figure 2.

 

Initial blank setup position: see Figure 4.

 

Tool moving direction:

Lower Punch: stationary

 

Upper Die: moving (-z direction)

 

Binder: moving (-z direction)

 

 

Figure 1. STAGE 1 Tooling Components and Coordinate System in Side-View.

 

Figure 2. STAGE 1 Major Tooling Dimensions.

 

 

Figure 3. STAGE 1 Kiss block and Drawbead Dimensions and Location. Note the upper die and lower binder are shown in an OPEN position.

 

 

Figure 4. STAGE 1 Blank Size and Location, Rolling (0 degree) Direction of Sheet Coil, and XY coordinate system in Plan-View. If symmetry is used, restrict analysis to the upper-right quadrant (,).

 

 

  Description

 Symbol

Value (mm)

  Upper Die

 

 

     Width of Die Cavity

Wd

319.90

     Radius of Die Profile

Rd

12.00

  Punch

 

 

     Width of Punch

Wp

224.00

     Radius of Punch Profile

Rp

12.00

  Binder

 

 

     Binder Gap

Bg

See Table 1.1

  Drawbead

 

 

     Bead Position

Bp

31.05

     Depth of Bead[1]
 

Db

6.85

     Radius of Bead

Rb

4.00

     Width of Channel

Wc

10.80

     Radius of Channel

Rc

4.00

  BLANK

 

 

     Width

BW

254.00

     Length

BL

1066.80

Table 1. STAGE 1 Tooling, Drawbead and Processing Parameters in Figures 2 and 3.

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[1] Officially, the Standard Benchmark defined in Table 1 involves a single bead depth of 6.85 mm for all materials, which corresponds to approximately a 75% bead penetration. However, an Extended Benchmark study will include bead depths at 25, 50, 75, and 100% penetration as described in Table 1.1. (Due to an experimental difficulty, a maximum bead depth was reduced from 100% penetration for the DP 600.) The additional bead depths are defined in these instructions only to inform interested parties that additional data will be available from this study in case they want to write a technical paper on the role of the magnitude of prestrain in this process. The Report File format does not permit inclusion of the additional analysis and therefore the Benchmark Analysis Committee will not compare them.

  

Material

Bg (mm)

Db (mm) 75%

Db (mm)

25%

Db (mm)

50%

Db (mm)

~100%

DQSK

1.42

6.85

2.34

4.75

9.09

HSLA 50

1.18

6.85

2.34

4.75

9.09

DP 600

1.42

6.85

2.34

4.75

8.35

AL 6022-T43

1.42

6.85

2.34

4.75

9.09

Table 1.1 Binder Gap and Drawbead Depth for the Standard Benchmark. The additional drawbead depths are used in the Extended Benchmark study as described in the footnote. The bead depths are nominally set at 25, 50, 75, and 100% penetration.

 

 STAGE 1. Springback and Blank Trimming for Stage 2.

 

Following Stage 1 forming, the side view of the sheet after springback has the nominal shape shown in Figure 5. Profiles of the sheet will be measured and the radius of curvature (R-curl) in the sidewall will be determined as shown in the figure.

 

Two trimmed blanks are cut from separate specimens of the Stage 1 channel draw test after springback in preparation for Stage 2 forming. The trim lines are at arc length distances DA and DB from the centerline of the Stage 1 process (), as shown in Figure 5 for Specimens A and B, respectively. Specimen A is cut from the side wall as illustrated in RED with the longer dimension (LA) out of the plane of the page in this figure. Point 1, located at one end of the RED line, forms one edge of the width of Specimen A at a arc length distance (DA) from the centerline. Point 2 is located at an arc length distance (DA+WA) from the centerline to form the opposite edge of the specimen width. The length of the blank (LA) is nominally 254 mm, but is in fact determined by the STAGE 1 forming process, which is not precisely in a plane-strain condition. Specimen B is cut from the sidewall as illustrated in BLUE in Figure 5 with the longer dimension (LB) along the arc length of the sidewall curl of the STAGE 1 forming process. Point 2 along the BLUE line is located at a distance (DB) from the centerline. Point 1 of this specimen is located at an arc length distance (DB+LB) from the centerline.

 

Since the metal near edge 2 is in the punch radius contact area, it has a much higher curvature than the majority of the specimen, which is also curved in the opposite direction. For practical reasons, the curvature of this edge is reduced to nearly a flat condition using a manual 3 ton Arbor press as illustrated in Figure 7 using wood tools to avoid marring the sheet surface. This procedure is necessary to ensure proper control of the blank location and bead setting during binder closure of Stage 2. The flattening process may be simulated as illustrated, but since all the metal that is affected in this process remains outside the drawbead/lockstep of the Stage 2 process, it is not considered to be necessary.

 

Since all the metal for Specimen A and all the metal that ends up inside the drawbead/lockstep after binder closure in Stage 2 is nearly uniformly prestrained from Stage 1, the precise location of trimming for both Specimen A and B is not considered to be critical to the Stage 2 forming process.

 

Figure 5. Illustration of the metal shape after STAGE 1 Springback.

 

Although Specimens A and B are illustrated as coming from opposing sides of the same preformed specimen in Figure 5, this is only for illustration purposes. Since there may be slight differences in the experiment that would introduce a bias in the behavior of Specimens A and B if they were taken from opposite sides, both specimens were taken from the same side of the geometry of the Stage 1 forming process to eliminate this potential bias.

Figure 6. Perspective Views of Test Specimen A (left) and Specimen B (right).

 

 

  Description

 Symbol

Value (mm)

  Specimen A

 

 

     Distance to trim line

DA

166

     Width

WA

135

     Length

LA

Width of Stage 1 Specimen

  Specimen B

 

 

     Distance to trim line

DB

  88

     Width

WB

135

     Length

LB

254

 Table 2. STAGE 1 to STAGE 2 trimming dimensions referenced in Figures 5 and 6.

 

Figure 7. Illustration of process for “flattening” edge 2 of Specimen B. The affected area is outside the drawbead in Stage 2 forming.


 

Residual stresses through the sheet thickness are measured at the center of one of the cutoffs from Specimen B as shown in Figure 8. Note that prior to removing the cutoffs, the width of metal is the same dimension as the length of Specimen A. The stress measurements are obtained by neutron diffraction with a spatial resolution of XX mm.

Figure 8. Cutoffs of Specimen B for Residual Stress Measurement at Point 3, which is roughly at 30 mm from the edge. The dimensions of the cutoffs are 254 mm by roughly 60 mm.

 

 

STAGE 2. Binder Closure and Forming

 

The punch, binder and upper die are axisymmetric and illustrated in Figure 9 and the process is similar to a Marciniak Cup test with a blank width near plane strain forming conditions. This shows a side view of the axisymmetric tooling geometry in the x-z plane with symmetry along the Z-axis. Critical dimensions are shown in Figures 10 and 11 with the values given in Table 5. Punch speed during forming is a constant 1 mm/sec.

 

A washer, or coupon, of width WW=WA=WB and length LW=LB is inserted between the blank and the lower binder/punch tools as illustrated in Figure 12. The washer is used to improve metal flow over the punch radius during forming and obtain significantly higher levels of strain. The washer has a hole in its center of diameter DW and is made from the DQSK steel in the as-received condition for all four materials in the benchmark. The rolling direction of the washer material is always aligned with the long axis of the blank geometry for Stage 2 testing of both Specimens A and B.

 

Total blank holding force:

 

Material

Blank Holding Force (kN)

DQSK

350

HSLA 50

350

DP 600

350

AL 6022-T43

250

 Table 3. Blank holding forces are the same for Specimens A and B.

 

Binder Travel:

 

Prestrained Material

Specimen A (mm)

Specimen B (mm)

DQSK

8

15

HSLA 50

6

11

DP 600

9

10

AL 6022-T43

10

11

 Table 4. Final Punch Depths for the Standard Benchmark in Stage 2 forming.

 

The punch depths listed in Table 4 are for the Standard Benchmark specification. As discussed in the footnote on page 4, tests will be done and reported at the conference using the additional bead depths listed in Table 4.1 Furthermore, flat, non-prestrained samples of all four metals in the as-received condition will be tested in Stage 2 forming with the longer dimension of Specimen A cut along the rolling direction of the sheet and Specimen B cut along the transverse direction. Each prestrained Stage 1 test and as-received condition is taken to a different punch depth in Stage 2 as listed in Table 4.1. The punch depths used for these different conditions are empirically selected to maximize the amount of plastic deformation during Stage 2 without exceeding the forming limits of the materials. The same washer material and material axis orientation is used for all tests.

  

Material

Prestrained Condition

Bead Depth (mm)

Specimen A (mm)

Specimen B (mm)

DQSK

As-received

21

23

 

2.34

20

22

 

4.74

13

18

 

6.85

8

15

 

9.09

6

14

HSLA 50

As-received

19

18

 

2.34

16

16

 

4.74

9

13

 

6.85

6

11

 

9.09

6

10

DP 600

As-received

20

18

 

2.34

17

16

 

4.74

12

13

 

6.85

9

10

 

8.35

9

10

AL 6022-T43

As-received

17

18

 

2.34

13

15

 

4.74

11

13

 

6.85

10

11

 

9.09

10

11

 Table 4.1 Final Punch Depths for the Expanded Benchmark in Stage 2 forming. Only the 6.85 mm Stage 1 drawbead depth tests are to be reported to the Benchmark Analysis Committee.

 

The additional tests in Table 4.1 are not included in the Standard Benchmark due to the large amount of data, which would likely inhibit completion of all test conditions by the benchmark participants. Such a result would interfere with a meaningful comparison and reduce the value of the Standard Benchmark for the Numisheet Conference. However, experimental results for the Extended Benchmark may be of considerable interest from a theoretical and practical standpoint, and that is why they will also be reported at the conference.

 

Initial blank setup position: see Figures 12-16. The net result is that the blank is aligned with and lays flat against the washer at the end of binder closure and both are centered in the tooling.

 

Tool moving direction:

Lower Punch: moving (+z direction)

 

Upper Die: stationary

 

Binder: moving (+z direction)

 

 

Figure 9. STAGE 2 Tooling Components and Coordinate System in Side-View.

 

Figure 10. STAGE 2 Major Tooling Dimensions.

 

Figure 11. STAGE 2 Drawbead Dimensions and Location.

 

Figure 12. Illustration of STAGE 2 Blank and Washer Setups.

 

Figure 13. Illustration of plan view of curved specimen alignment prior to binder closure. See Figures 15 and 16 for actual photos.

 

Figure 14. Illustration of plan view of specimen alignment after binder closure. Location of Point 4 where in-situ stress and strain components are measured at the end of Stage 2.

 

Figure 15. View of Specimen A before binder closure in Stage 2.

 

Figure 16. View of Specimen B before binder closure in Stage 2.

 

 

  Description

 Symbol

Value (mm)

  Upper Die

 

 

     Diameter of Die Cavity

Dd

110.0

     Radius of Die Profile

Rd

12.0

  Punch

 

 

     Diameter of Punch

Dp

100.0

     Radius of Punch Profile

Rp

12.0

  Drawbead

 

 

     Bead Position

Bp

21.2

     Depth of Bead

Db

3.18

     Radius of Bead

Rb

3.18

     Width of Channel

Wc

7.94

     Inside Channel Radius

Rc1

1.98

     Outside Channel Radius

Rc2

1.19

  BLANK

 

 

     Width (A and B)

WA=WB

135.0

     Length (B only)

LB

254.0

  WASHER

 

 

     Width

WW

135.0

     Length

LW

254.0

     Hole Diameter

DH

32.5

 Table 5. STAGE 2 Parameters identified in Figures 10, 11 and 13.

 

Files for simulation

 

All geometry data is defined parametrically in the above description. The tooling for Stage 1 has a uniform section along the y-axis as defined in Figures 2 and 3. The tooling for Stage 2 is axisymmetric with a section through its axis of symmetry defined in Figures 10 and 11. No IGES surface geometry or NASTRAN mesh files are provided for this benchmark.

 

Material Property Files:

 

Standard properties are listed in the following worksheet and additional information is provided from auxiliary downloads in case participants want to use more sophisticated material models. Data for this benchmark are in the following 4 Excel spreadsheets.

 

                                   BM3_AKDQ.xls                                             BM3_DP600.xls        

                                   BM3_HSLA50.xls                                          BM3_AL6022-T43.xls

 

 

BENCHMARK REPORT


The due date for benchmark submission is listed on the website. All results are to be reported using the benchmark report template that is included in the download (BM1_Report_TMP.xls). Instructions for participating in the benchmark are provided in the file General_Benchmark_Instructions.pdf.  A total of 20 distributions and 44 data values are required for completion of Benchmark 3. Note that results for each of the four materials are to be reported in a separate worksheet within the same spreadsheet, each containing 5 distributions and 11 data values. The following information is requested for each material on the appropriate worksheet:

 

  1. Load1 (displacement). Distribution of punch load vs. punch displacement (100 points or less) during Stage 1 Forming. Distributions: 1.

  2. Rcurl. Sidewall curl (Rcurl in Figure 5) after Stage 1 springback. Data values: 1.

  3. Epsilon1 and Epsilon2. Major and minor strain components at Point 3 in Figure 6 after Stage 1 springback and blank trimming on the convex (Stage 1 punch) side. Strains must be dimensionless, not in units of percent. Data values: 2.

  4. SigmaXX (thickness) and SigmaYY (thickness). Distribution of major and minor residual stress components through the sheet thickness at Point 3 in Figure 6 after Stage 1 springback and blank trimming. Distributions: 2.

  5. Load2A (displacement). Distribution of punch load vs. punch displacement (100 points or less) during Stage 2 Forming for Test Specimen A. Distributions: 1.

  6. SigmaXXA and SigmaYYA. In-situ stress components on the upper surface at Point 4 in Figure 14 at maximum punch depth at the end of Stage 2 Forming (Table 4) for Specimen A. Data values: 2.

  7. EpsilonXXA and EpsilonYYA. Net major and minor strain components on the upper surface at Point 4 in Figure 14 after Stage 2 unloading for Specimen A. Strains must be dimensionless, not in units of percent. Data values: 2.

  8. Load2B (time), SigmaXXB, SigmaYYB, Epsilon1B and Epsilon2B. Repeat items 5-7 for Test Specimen B. Distributions: 1. Data values: 4.

 

 

It is critical to update the number of points used in each of the distributions in ROW 10 of the appropriate columns and worksheets.

 

 

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