Investigation of cutting tool diameter influencing wire cutting operation accuracy using several matrix configurations.
Dundulis, R. ; Bortkevicius, R.
1. Introduction
Process description and actuality of the work. In the paper there
is presented an investigation from JSC ITAB NOVENA manufactured
products, containing shape disalignments, i.e. cutting wire strip with
oval matrix and the punch cannot ensure needed geometric form, therefore
it is in need to propose the other geometric shape tools: bigger form of
cutting tools. In the paper it is discussed various punch/matrix ratio
influence to the wire strip endings area and it's precision. The
researches have been conducted using several matrix diametric
configuration. Here in presented deformational characteristically curves
using various diameters ovalic cutting tools. There were used various
diameters wire strip diameters specimens.
The objective of the investigation is to determine the most
effective methods to turn strip endings to ovals since at the present
time it is getting into sort of shape of triangular. Three main problems
were investigated: 1 - the change of cross-sectional area in the cutting
place, 2 - bending angle, 3 - monotonous strain distribution in the
axial direction of wire strip. Cutting operation were investigated by
scientists [1], where is described full formation of the chip in the
cutting operation, described material models used in the modelling
orthogonal cut [2], elements for modelling cutting operation is fully
presented by scientists [3, 4] which models are for used for cutting and
also include high strain rates and plastic deformation therefore are
replicated with our investigation. One parameter is missing in the works
of scientists - material changes in its initial geometry when harder
tool initiates a cut [5]. Orthogonal cut is investigated in the
scientific works [6, 7, 8]. Here in cutting operation presented when the
sharp tool cuts softer material. Major problem of investigation must be
considering how rank angle influence the penetration depth [7, 8]. And
later on forms a chip. No change in initial geometry are observed. Major
object of orthogonal cut is to determine right tool geometry to cut
materials with minimized cutting force, and to reduce friction to the
lowest possible values [1, 2, 9]. There is a lack of investigation when
material is cut with a tool which rank angle is at 90[degrees].
Problem. During normal workday, factory worker cuts several
thousand wires strips, which later on goes to the end-customer. The end
customer wants to buy thousand wire-strips of different diameter. In
order to cut wanted diameter it needed to over-change the punch and the
matrix, which is suited for the only particular wire diameter. The end
customer started to comply about the quality of the wire strip ends. So
the major problem of the investigation is the changed geometry of wire
strip endings after the cutting operation. Therefore, the object of the
investigation is wire strip endings and the determination of the right
cutting tool.
Novelty. The rank angle is considered as obtuse angle [4, 9]. In
the present investigation material is cut with mentioned rake angle, so
actual cutting operation it is hard to describe. Three phases of cutting
operation where there founded and investigated. Some of the problems are
related with a modelling in itself. In the past years cutting operation
where were modelling with solid elements in three dimensions [4, 8].
Recent years scientists [10, 11, 12, 13, 14] tries to use SPH modelling
of cutting operation.
Paper ends up with determined mechanical characteristics of
specimens. Identified 3 critical zones where most likely the fracture
will occur and begins. In these 3 zones plastic deformation distributed
not evenly. In those zones there were measured specimens area reduction
and compared with plastic deformation distribution and variation.
Accordingly, the most important set of plastic strain ratio were
determined.
2. Testing procedures
In order to determine the best available quality for wire cutting
operation there was constructed wire cutting tool, where major
components consisted of classical cutting equipment: the tool holder 1
(it is a main equipment for force supplying), the punch 2 and the matrix
3. It can be seen in the Fig. 1, a.
The punch and the matrix configuration suited only for specific
wire diameter and it can be seen in the Fig. 1, b. Here in number 1
designated exchangeable matrix tools and 2 designated exchangeable punch
tools. In order to make an investigation there were choosing several
simple wire components raging in diameter from [empty set]2 to [empty
set]6 mm. Several different types of cutting equipment there were tested
in order to find the best economically based and quality based solution.
To make research in to more deep there was conducted an experiment with
equipment stored in the company JSC "ITAB NOVENA" and all
copyrights of used equipment solely be-long to the mentioned company.
Cut cross section view of the wire strip with a tool (Fig. 1) are given
in the Fig. 2. Here in are indicated 3 crucial zones after cutting
operation. Experimental measuring of cross section was made using 3D
scanner with scanning processing precision of 0.2 [micro]m. 3D scanned
view of the wire strip with 3 significant areas can be seen in the Fig.
3, a. The same wire strip has been photographed with ordinary camera.
Photo can be seen in the Fig. 3, b. The results of measuring fully
matches between scanned object and measured with properties though
specimens were taken from one Kaunas Mechel factory. Material to produce
wires are delivered from single supplier in the Russian federation.
Withdrawn in Kaunas Mechel factory as well as made final heat treatment.
Material grade to make a wire identified in the Table 1.
[FIGURE 1 OMITTED]
[FIGURE 2 OMITTED]
Therefore, mechanical properties between wire should be identical
but it is not so. In order to complete investigation of chosen materials
there was in need to complete an investigation of tension test.
Investigation were accomplished in the Kaunas University of Technology.
Tension test machine gripers were specially constructed for given wire
strips. Special form of gripers was designed in order to clamp wire
strips between clutches in order to create no movement there in. Several
designs of clutches were introduced to make an experiment, but only one
was suited for particular experimental studies. Tested material
mechanical properties are given in the Table 1. In the both Figs. 2 and
3 there is and the 4th zone, which must be treated as non-perfect and so
has to be treated as defect. Though this 4th zone is not included in
cross-sectional measurements but it is very important. As a matter of
fact, all deformed specimens have had similar shape of deformed 4th
zone. The shape replicates the shape of parabola.
Zones in the cut area do not replicated any known shape describable
by any canonical equation. It need to mention, that the 4th zone has
identical deformation no matter of cutting tool diameter and wire strip
diameter itself. The material properties in the investigation of various
specimens there were gained not identical mechanical properties though
specimens were taken from one Kaunas Mechel factory.
In the Table 2 indexes denote: [[sigma].sub.p] is limit of
proportionality, MPa; [e.sub.y] is yield strain component of the tested
material; [[sigma].sub.Y] is yield stress component of the tested
material, MPa; [[sigma].sub.u] is ultimate stress state, MPa; [e.sub.u]
is ultimate strain state; [[sigma].sub.f] is stress at fracture, MPa; E
is Young modulus, MPa Wire specimen no indicate the tested material rank
number and figures beside rank number indicate tested material diameter.
[FIGURE 3 OMITTED]
3. Investigation of cutting operation by FEM
Finite element model was created using FEM software LS-Dyna [4, 6].
This model can be analysed in the Fig. 4. FEM model consist of the
following equipment: 1 - exchangeable punch, 2 - ex-changeable matrix,
and 3 is wire strip. In order to check whether the oval shape is the
best available shape for cutting operation there were proposed other
cutting shapes: hybrid 1 (consisting from oval punch, which diameter
equal to the cutting material diameter and the matrix which diameter is
bigger than cutting material diameter).
These shapes are presented in the Fig. 5. The investigation was
carried out using several (in this experimental studies we were using 5
different matrix diameters) matrix configuration: 1 matrix is equal to
diameter of cutting material as well as diameter of the punch. The 2-nd
matrix is 15% bigger than cutting material. The 3-rd matrix 24% bigger
then initial matrix diameter. The 4-th matrix is 32% bigger then initial
matrix diameter. And the 5-th matrix is 39% bigger then initial matrix
diameter.
[FIGURE 4 OMITTED]
[FIGURE 5 OMITTED]
Boundary conditions satisfying experimental problem formulated in
the Fig. 6 one end of work piece is fixed in the punch and cannot be
moved through another end in free to move in the Z direction (orthogonal
cut [1-6]).
[FIGURE 6 OMITTED]
[FIGURE 7 OMITTED]
Several unknowns of workpiece are indicated: [empty set]d is
diameter of workpiece, [empty set]D is diameter of cutting tools, U is
cutting tool displacement as function of time, t is distance between
cutting tools, [phi] is rake angle, [S.sub.1] and [S.sub.2] are an edge
of curled edge after cutting operation in orthogonal direction,
[n.sub.1] and [n.sub.2] are curled edge after cutting operation in
longitudinal direction. In the present investigation distance between
cutting tools was chosen to be without any gap and the influence of this
parameter (designated t in the Fig. 6) are not the intensions of this
paper and will be presented in the future. FEM of orthogonal cutis given
in the Fig. 7. Here in can be seen 3 significant zones. Actual
experiment was performed without any gap between tools, though in
reality it is impossible to create any cutting tool without a gap. So it
will be in a tolerance of around 0.2 mm. All units in calculation and
experimental studies are in SI. Though calculation with LS-Dyna are as
following: ton, mm, s, N. In the investigation there were used material
model from LS-Dyna material library:
*Piece_wise_linear_plasticity, where few modulus where chosen
according to equation 1 and 2:
E = d[sigma]/d[epsilon], [sigma] < [[sigma].sub.Y], (1)
[E.sub.TAN] = d[sigma]/d[epsilon], [sigma] > [[sigma].sub.Y],
(2)
where E is Young modulus, d[sigma] is true of stress increments,
d[epsilon] is true strain increments, [[sigma].sub.Y] is yield stress,
[E.sub.TAN] is tangent modulus. Final equation of the material model it
is used:
[[sigma].sub.Y] ([[epsilon].sup.p.sub.eff] [[??].sup.p.sub.eff]) =
[[sigma].sup.s.sub.Y]([[epsilon].sup.p.sub.eff]) [1 +
[([[??].sup.p.sub.eff]/C).sup.1/p]], (3)
here [[sigma].sub.Y] is yield stress, [[epsilon].sup.p.sub.eff] is
effective plastic strain, [[??].sup.p.sub.eff] is effective plastic
strain rate, [[sigma].sup.s.sub.Y] is static stress component, C is
constant, p is Cowper and Symonds coefficient.
[FIGURE 8 OMITTED]
[FIGURE 9 OMITTED]
Tension test apparatus can be seen in the Fig. 8. To fully matched
FEM with experimental investigation there were chosen experimental
mechanical curves use in the FEM and do the same tension test but this
time numerically [7]. Numerical tension test investigations were made
with software LS-Dyna using single precision solver and 64 bit system
[4]. Experimental curves from tension test and curves from FEM can be
seen in the Fig. 9. The highest mismatched between two methodologies are
gained then was testing material No. 4 and this is 8.93%. Other
specimens are situated bellow this value. The average stress component
from experiments are 1122 MPa. From finite element analysis stress
component are only 5 MPa (the percentage expression is 2.83).
4. Results
To compare and relate methodologies (experimental and numerical)
there were made an investigation of cross-section area (A, A',
A") measurement. The cross-section where measured in the real
specimen after 3D scanned (Fig. 3, a) and also cross-section area
(A") data, taken from FE model. The comparison of cross-section
area where made in relation with theoretical data (A). The results are
provided in the Fig. 10. Here in one can see specimens'
cross-section A measured in [mm.sup.2] dependence on the specimens'
initial diameter d, mm. Designation A'-d means, that measurements
were taken from 3D scanned view. Curve d-A means theoretical
cross-section area, without deformation. The 3rd curve d-A' '
means the same cross-section area dependence on initial diameter, but
data are taken from FE model. The difference of measured data from 3D
scan and data taken from FEM is in between 4 percent. So this FEM data
we treating as reliable. True strain of a particular cross-section also
is given in the Fig. 10. Cross-section deformation (dA) dependence from
a value of diameter (d) do not revealed any significant deviation from a
nominal value and it can be treated as linear. Though the measurements
were made at the final stage of cutting and it might be possible that
nonlinearity of cross-sectional are can be obtained in between the
cutting operation stages. This can be perfectly be grasped from the Fig.
11 - Fig. 15 where were obtained nonlinearity in between cutting stages.
Higher and this fully satisfies an investigation data precision [9, 10].
Experimental cross-sectional view with problematic areas are given in
the Figs. 3, b and 4. Numerical analogue view are given in the Fig. 7
the 3 zones are clear. In the experimental view only 2 zones can be
identified from the picture.
[FIGURE 10 OMITTED]
Though the 3-rd zone can be derived at very endings of the
cross-sectional view. After the experimental studies of all diameters
wires were completed we examined the most critical place of the wire
strip where most likely the fracture will occur [11, 12]. We examined
the overall change of area A (listed by the numbers I-V) in parallel
with major stress component [[sigma].sub.1] (listed by the numbers 1-5)
(Figs. from 11 to 15).
[FIGURE 11 OMITTED]
[FIGURE 12 OMITTED]
[FIGURE 13 OMITTED]
The common axis of abscises designated for plastic strain
[[[epsilon].sub.pl]] distribution. The results from Figures show some
common features of wire strip cutting operation. Then diameter of matrix
is equal or slightly bigger than the diameter of wire strip (designated
1 and I in the Figs. 11-15) the bending operation begins and plastic
deformation are growing straight forward depending on the position of
the punch. In the major stress intensity [[sigma].sub.1] shows all
investigated diameters influenced wire in the context of bending. The
differences between ratio of matrix and the punch shows that increasing
matrix diameter proportionally give the wire experiences fracture not at
the same stress level, though the plastic deformation
[[[epsilon].sub.pl]] component. The change of are visible only for I and
II matrix configuration. And there is no any major distinction between
those two. Fig. 9 shows little difference between previous Figure in
context of major stress intensity [[sigma].sub.1]. Only 1 matrix
configuration differs from other. 2 - 5 matrix configuration show only
minor differences.
[FIGURE 14 OMITTED]
[FIGURE 15 OMITTED]
Though area of the cut cross section have had an area change and it
is quite obvious. The reduction of cross sections are: for the matrix I
is 14%, II - 13%, III - 7%, IV - 3% and V - 5%. Figure 11 revealed that
major stress component has a negative sign, what means that fracture in
the cut area begins after compression of wire strip between cutting
tools. The reduction of cross sections are: for the matrix I is 12%, II
- 18%, III - 7.16%, IV - 12% and V - 18%. In the Fig. 11 can be seen a
little different view Here in major stress component has unexpected
changes between 1st and 5th. Matrix configuration. Matrix 3, 4 and the
5th have a tendency of negative major component until reach a 0.15
[[epsilon].sub.pl] and then experience a positive sign i.e. wire strip
experience a tension with no compression at all. But since wire strip of
diameter 5 has fractured under around 0.12-0.15 of plastic deformation
and around 700 MPa of major stress it looks that at the particular case
a fracture of wire strip experienced then major stress component had a
negative sign not depending on matrix configuration. The reduction of
cross section are: I is 15%, II - 13%, III 16%, IV - 15% and V - 13%.
That means that reduction of cross section uphold quit the same rate of
reduction between matrix configurations. In the Fig. 12 there are
absolute different situation from the Fig. 11. Fracture begins at the
compression. And no real reduction of cross section is noticed.
5. Conclusions
1. Seven different diameters wire strips were tested. Mechanical
characteristics by tension test were determined. Seven numerical
experiments were examined by changing diameters of punch giving a total
of 35 different experiment versions.
1. Based on these findings it is recommended to use results in the
design of the new metal sheet cutting tools. As well it is recommended
to use these findings in manufacturing of wire strips.
2. Diameter of cutting tool does not influence the wire trip
endings; though the ratio of tool/wire does influence the wire strip
endings.
3. No single shape solution were determined for a better wire strip
end shape since all proposed shapes provided quite huge variation of the
idle shape.
4. Oval shape of cutting tool gave an inclination at four sides of
wire strip and it cannot be considered as a better shape over others.
5. No better cutting shape was determined, since material for wire
strips are in the wide range.
Received October 23, 2015
Accepted November 12, 2015
http://dx.doi.org/10.5755/j01.mech.21.6.13477
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R. Dundulis *, R. Bortkevicius **
* Kaunas University of Technology, Studenty 56, 51424 Kaunas,
Lithuania, E-mail: romualdas.dundulis@ktu.lt
** Kaunas University of Applied Engineering Sciences, Tvirtoves al.
35, LT-50155 Kaunas, Lithuania, E-mail: rytis.bortkevicius@edu.ktk.lt
Table 1
Technical specification
[empty set], Tensile Standard Steel Standard for
mm strength, for steel grade chemical
MPa product composition
1.0-1.8 1000-1200 EN 10218-2 SAE 1006; ASTM A
(DIN 177) SAE 1008 510M
2.0-6.0 590-830
Table 2
Mechanical characteristics of tested specimens
Wire Diameter of [[sigma].sub.p], [e.sub.y]
specimen wire, mm MPa
number
No.1 2.2 580 0.0029
No.2 2.5 500 0.0028
No.3 3.06 530 0.00313
No.4 3.4 560 0.0033
No.5 4 440 0.002
No.6 5 440 0.0022
No.7 6 360 0.0021
Wire [[sigma].sub.Y], [[sigma].sub.u], [e.sub.u]
specimen MPa MPa
number
No.1 915 936 0.00482
No.2 784 802 0.0049
No.3 750 789 0.00828
No.4 838 862 0.00843
No.5 705 727 0.0071
No.6 710 741 0.0063
No.7 590 623 0.0088
Wire [[sigma].sub.f], E, MPa
specimen MPa
number
No.1 1190 196756
No.2 1160 177368
No.3 1119 169276
No.4 1169 169910
No.5 1004 215651
No.6 1081 196612
No.7 1070 171626