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M

ay

2009

www.read-tpt.com

118

Once at this stage of the theoretical parabolic contour, there

is a 1.39° deflection of the reflected light of the formed section’s

outset point. However, the reflected light can only be reflected to

the effective decalescence position. According to the marginal

ray principle

[4]

, all of the parallel light arrives at the effective

decalescence position after reflection by the formed section, which

shows that the spotlight performances of formed section and

parabolic contour are closed to a considerable degree.

4. Finite element analysis simulation

For practical engineering, the required parabolic parameters and

experimental model cannot be fully in accordance. The method

involves an extensive application of the feasibility of the forming

parabolic using rollforming and the accuracy of roll design.

Therefore, finite element analysis was used for the forming process

of the parabolic section in this study. Rollforming is a complicated

non-linear problem. Therefore, the forming process for the parabolic

section was simulated by the commercial FEA software MSC Marc.

4.1 Finite element analysis simulation of forming process

experiments

Because the rollforming process is very complicated, the FEA model

used in simulation should be simplified according to the practical

condition. In this study, during setup of the simulation forming

model, sheet material is deformable and the roll is rigid, and friction

force is not considered. Sheet material fed through the rolling tool is

replaced with a quarter roll sliding on the strip, and the entire long

sheet material is replaced by precut pieces of strip.

The centre distance between two stations is 250mm, and the

length of precut strip material is 300mm and the width 120mm.

The strip is divided equally to 60 elements in X-axis (transverse

direction) and 50 elements in Z axis (forming direction). There are

3,000 elements in total, and the element thickness is the practical

thickness of forming aluminium sheet (0.48mm). The element type

is No.139 with 4

nodes of thin shell.

The

simulation

geometric model is

shown in figure 9.

Boundary conditions comprise the fixed displacement at the

beginning and end of the forming strip in Z direction, and all

fixed displacement areas on the centre point of the end strip in X

direction. The Von Misses

yield and isotropic hardening criterion

were used.

In the simulation result of the forming strip, displacement in Y axis

(vertical direction) is shown as figure 10. Here different colours have

been used to represent different displacement. It can be observed

that Y displacements of the forming strip are always shown as the

same colour, which means that the length of the forming direction

of the parabolic section is uniform and the forming of the parabolic

section is comparative.

4.2 Simulation result analysis

The formed section can be compared with the simulation result. For

analysis, the experiment results had 3 corresponding sections that

keep the distance respectively of 400mm, 500mm and 600mm to

the beginning of the formed strip. For this reason, 3 sections were

picked that keep the respective distances of 100mm, 150mm and

200mm to the start of strip simulation.

Firstly, coordinates are based in the unfolding centre of the formed

section. Because of the symmetry, only the positive half axle of

transversely unfolding section coordinates is taken into account.

Then, this strip is divided equally into 6 parts, and on the divided

point, the normal error between formed section and simulation

section is shown in table 2. In the table, the positive value shows

that the simulation section is blow formed section on the divided

point, and the negative value shows that the simulation section is

formed from above on the divided point.

The mean value of normal errors of every divided point is shown in

figure 11. Given the data of table 2, the maximum error is 0.3mm. It

is observed that simulation section and formed section are basically

identical, and simulation results in high precision, so that simulating

results are reliable for engineering design.

4.3 Finite element simulation of aluminium sheet forming

process with the thickness of 0.5mm

In order to establish the thickness difference of material and roll

design setting, 0.5mm thickness aluminium sheet is used for finite

element simulation. The error is compared with a simulation strip

thickness of 0.48mm.

Sample

No.

Formed

section in Z

coordinate

(mm)

Transverse unfolding coordinate of section (mm)

X=0 X=10 X=20 X=30 X=40 X=50 X=60

1

Z=400

0 0.16 0.22 0.25 0.37 0.49 0.55

Z=500

0

0 -0.04 0.21 0.31 0.10 -0.15

Z=600

0 0.16 0.18 0.43 0.50 0.28 0.07

2

Z=400

0 -0.07 -0.19 0.04 0.2 0.14 0.11

Z=500

0 -0.06 -0.10 0.25 0.36 0.2 -0.04

Z=600

0 -0.11 -0.20 0.10 0.35 0.38 0.44

3

Z=400

0 -0.11 -0.23 0 0.13 0.01 -0.11

Z=500

0 -0.01 -0.1 0.12 0.25 0.15 0.07

Z=600

0 -0.18 -0.27 0.05 0.27 0.20 0.05

Table 2

:

A normal error between simulation section and formed section (mm)

Table 3

:

A normal error between simulation section and idea parabolic section (mm)

Formed

section in Z

coordinate

(mm)

Transverse unfolding coordinate of section (mm)

X=0 X=10 X=20 X=30 X=40 X=50 X=60

Z=100

0

-0.12 -0.2 -0.33 -0.35 -0.56 -0.95

Z=150

0

-0.17 -0.17 -0.31 -0.38 -0.5 -0.88

Z=200

0

-0.11 -0.21 -0.29 -0.36 -0.54 -0.89

Figure 9

:

Simulation

geometric model