Turning roughness model based on tool-nose displacements/Tekinimo siurkstumo modelis ivertinant irankio virsunes poslinkius.
Zahia, Hessainia ; Nabil, Kribes ; Yalles, M.A. 等
1. Introduction
The surface roughness of workpieces achieved by turning operations
plays a determinable role on product quality. Many factors affect the
roughness directly and also with indirectly manners. To understand and
quantify their influences, many research works have been published
taking into account via different mathematical models, the correlation
between various operating parameters [1]. The latter can be classified
into two types: cutting parameters (cutting speed, cutting depth, and
feed rate), machine-tool parameters (stiffness, geometry, insert
material (substrate and coating grades)).
In order to improve the machining system stability, the control of
machine tool dynamic behaviour presents an important interest during
design, manufacture and exploitation steps [2].
In machining by cutting tool, two vibration types can be observed;
forced vibrations and self-excited ones. The forced vibrations appear
under the effect of various periodic disturbances (unbalance, chip
segmentation and/or its fragmentation, etc), whereas the self-excited
vibrations, which are characterised by the development of surface
imperfections on the workpiece, are commonly named chattering. These
complex vibrations are essentially caused by the lock in stability of
the global cutting system (work-piece, tool and machine).
In this framework, the present study proposes to bring
understandings of the effect of operating parameters and their
interactions on the machined surface roughness. This work is assumed to
be in an independent domain from excited vibration conditions.
Before proposing a modelling, it is interesting to put in review
some important research works considering roughness models. For example,
in their approaches, [3] and [4] have took into account, only tool-nose
radius and the feed rate. They have showed that to get improve surface
texture; it is necessary to decrease the feed rate or to increase the
tool-nose radius. This basic result is in corroboration with the
tool-workpiece geometrical aspects when considering turning operations.
Also, this result is globally known among the industrial community
performing machining with cutting tool. Nevertheless, this model is not
valid for low feed rates, particularly. Indeed, the model predicted
roughness values are far from those deduced by experimentation.
Moreover, it is underlined that working parameters such as feed rate,
cutting depth and cutting speed have an important influence on the cut
surface roughness. Their effect can be remarked directly or via their
interactions. Among the published paper on the subject, it can be cited
the works of [5-7]. In their approaches, these authors have assumed that
only the tool-nose radius has an important role on roughness, whereas
[8] have shown that other geometric features of tool nose can be
considered.
The relative vibrations between tool and work-piece are often
ignored by researchers when studying roughness. [9] have suggested that
the divergence observed on machined surface roughness is mainly due to
the tool vibrations. According to these authors, cutting with a rigid
tool could improve roughness, considerably.
Others parameters can affect the roughness evolution, such as
material hardness. [1] have made experimental tests on a material which
has a different hardness varying between 45 to 70 HRC. They have found
that the roughness increases up to 50 HRC and then decreases.
In order to analyse and bring a robust quantification of roughness
evolution during cutting phenomenon, several statistic and data
treatment methods were adopted. Among, the recent ones, it can be
mentioned the multiple linear regression method which was exploited by
[10] to develop a complete empirical model of the roughness. The
developed experimental approach takes into account many factors such as
feed rate, workpiece material hardness, tool-nose radius, cutting depth
and their mutual interaction. The experimental results were analyzed by
statistic software showing the parameter influence and their level of
importance.
The authors [8] have used another investigation method based on the
analysis of variance ANOVA. To determine the effects of both the
material hardness and the tool-nose geometry on the cut surface
roughness, a factorial design was adopted during carrying out the
experiments. Analysis of the results obtained highlights once more that
the feed rate and the tool geometry have an important influence on
roughness evolution.
Moreover, it can be noted in a set of factorial experiments carried
out by [11] Feng and Hu (2001) and Feng (2001) that cutting angle, the
tool-nose radius, the feed rate, the cutting depth, the cutting speed,
the workpiece stiffness as well as the various interactions between
these factors have a significant effect on the cut surface roughness
variation. These factors can induce vibration rise on the tool-workpiece
interface. Consequently, the vibration amplitudes could induce effects
(degradation or improvement) on the geometric micro quality of the
machined surface.
In the present experimental work, the case of generated surface
during straight and continue turning operations is treated. It is
assumed that the working conditions do not induce chattering phenomenon
(based on the choice of cutting depth and controlling data gathered by
sensors 2 and 3 (Fig. 1), i.e. without maintained workpiece self
vibrations. The proposed study treats the effect of oscillations due to
the segmentation and fragmentation phenomena as that was shown by [12]
on the machined surface micro-defects. For that, an experimental model
for roughness based on the multiple linear regression method is
established in order to quantify the influence of the vibrations on the
surface quality. This model is based on the multiple linear regression
method which is is established according to the tool displacements in
radial, axial and tangential directions.
2. Experimental set-up
The tests were carried out in straight turning operation. The
equipment used in the experiments is defined in Table 1. The measuring
sensors illustrated by Fig. 1 comprise three piezoelectric accelerometers. The first one is a triaxial accelerometer fixed in the
vicinity of the tool-nose. The second one is fixed on the spindle (see
the left side in Fig. 1). The third one is fixed on the machine frame.
The measured forces during cutting are given by a dynamometric platform.
The sensors and the platform are connected to an acquisition data system
(NI PCI 4472) through charge amplifiers. The data are gathered on a
computer by using the Labview software and treated then with the Matlab
software package. The machined surface roughness is measured using a
roughometer.
[FIGURE 1 OMITTED]
Table 2 summarizes the set of working, measured and calculated
parameters used in the proposed work. During carrying out tests, only
one among the three cutting parameters ([a.sub.p], f, [V.sub.c]) is
varied. This choice makes it possible to detect the influence of each
parameter on the studied criteria of roughness (Ra, Rz, Rt, Rsm),
precisely. Table 3 gathers the measured values of the forces components,
[F.sub.x] in radial, [F.sub.y] in axial, [F.sub.z] in tangential
directions during the cutting operation as well as the components of the
toolnose accelerations (in radial [a.sub.x], axial [a.sub.y] and
tangential [a.sub.z] directions), the spindle acceleration, [a.sub.s],
and the frame machine tools [a.sub.f]. Also, it can be found in Table 3
the calculated results concerning the radial, axial and tangential
components of tool-nose displacements [d.sub.x], [d.sub.y], [d.sub.z],
respectively. The radial displacements of the spindle and the machine
tool frame are denoted [d.sub.s] and [d.sub.f], respectively.
Displacements are calculated by dividing the spectrum of the
acceleration temporal signal on the corresponding squared pulse. Thus
the spectrum obtained of displacement is transformed into temporal
signal by the Inverse Fast Fourier Transform (IFFT). This procedure is
illustrated in Fig. 2.
[FIGURE 2 OMITTED]
3. Results and discussions
The aim of test campaign carried out is to determine the tool-nose
vibration influence on the machined surface roughness. This was possible
by getting many results dealing with the temporal signals of tool-nose
accelerations and force components during cutting process as shown in
Fig. 3. The latter demonstrates the evolution of acceleration amplitudes
of tool-nose and the correspondent measured forces according to feed
rate variation during a time acquisition of 1.2 s. The fixed working
parameters are [a.sub.p] = 1 mm and [V.sub.c] = 180 m/min. The
calculation of acceleration amplitude is estimated to the half of the
difference between the minimum and the maximum of the gathered signal.
Tangential cutting force amplitudes given in Fig. 3 evolve with the
values of tangential acceleration. It is observed that the tangential
force component is preva lent regarding the others forces (Table 3).
[FIGURE 3 OMITTED]
Fig. 4, a, b and c deal with radial, axial and tangential tool-nose
displacements in front of the workpiece along three generating lines (in
the direction of tool advance), respectively. These displacements show
comparable amplitudes characterised by similar order of values when
compared with the measured roughness criteria on the machined workpiece
(Rz and Rt). Nevertheless, disturbances on different curves are quite
present. Also, it is remarked a non-noticeable characteristic repetition
when comparing curves. Consequently, a statistical approach seems to be
interesting to adopt.
To detect the stiffness effect of the spindle and the machine tool
frame on the gathered tool-nose displacements, two sensors were placed
on locations (accelerometer 2 and 3, respectively) as shown in Fig. 1.
Displacements correspondent to acceleration signal acquisition given by
the pre-cited accelerometers are illustrated in Fig. 4, d. They are
about of 0.2 to 0.5 um for spindle sleeve and the machine-tool frame,
respectively. These values will be neglected because they very weak
compared to tool-nose displacements.
[FIGURE 4 OMITTED]
[FIGURE 5 OMITTED]
Fig. 5 gives evolutions of roughness and the three components of
tool-nose mean displacements according to feed-rate variations. It can
be observed a great tendency agreement between the roughness values and
tool-nose displacement ones. This makes it possible to assume a close
relationship between them. For average values of feed-rates, the
machined surface quality (roughness Ra) is improved, whereas it is
degraded with higher feed-rates. This observation is already approved in
the literature and the roughness is given by the following equation:
Ra = [f.sup.2]/32[r.sub.s], (1)
where f is feed rate mm/rev; re is tool-nose radius mm.
Nevertheless, for small feed-rates it is noticed that the surface
quality is degraded. This is certainly due to the presence of the
vibrations coming from the increase of tool-nose acceleration amplitude
(Fig. 3).
The cutting depth effect on roughness is less important than that
of feed rate. It acts by interactions with cutting speed and the feed
rate in a product form. According to [13] the higher is cutting speed,
the higher is cut surface quality.
4. Roughness modelling
In order to build roughness models containing all cutting
parameters, tool-nose displacements, spindle and machine tool frame and
also their interactions, the statistical software MINITAB was exploited.
It has allowed developing two correlations based on multiple linear
regressions
* linear model:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (2)
where c is a constant and a, b,...., gg are model coefficients.
* non-linear model:
[MATHEMATICAL EXPRESSION NOT REPRODUCIBLE IN ASCII] (3)
where c is a constant and [alpha], [beta], [psi] are model
exponents.
In order to determine the influence of parameters considered from
the previous roughness equations, a threshold indicator P was defined.
It determines the opportunity of rejecting non-significant predictive
parameters when P is greater or equal to 0.05.
Table 4 summarises the statistic results obtained by considering
the predefined threshold indicator P. The mathematical roughness models
given are obtained with correlation coefficients [R.sup.2] higher than
90% characterising the reliability of models. Consequently, proposed
models are acceptable. Additionally, the correlation coefficient [R.sup.2] shows that linear model is more entrusting than non-linear
one. This is due to that the number of linear model factors is greater
than non linear ones. Nevertheless, the two models confirm the effect of
radial and tangential tool-nose displacements and cutting speed on the
roughness evolution. The nonlinear model shows an improvement of the
surface quality with the increase of cutting speed.
Moreover, it can be noticed an explicit absence of feed rate from
the nonlinear model. This can be explained by the fact that the effect
of feed rate is implicitly acts in radial and tangential displacement
appearing in the model, from where established models:
dx = 1.2 +18.4 (f[a.sub.p]), [R.sup.2] = 85.2%;
dz = 1. 45 [f.sup.0.512] [a.sub.p.sup.0.639] [V.sub.c.sup.0.522],
[R.sup.2] = 78.3%.
The values of the correlation coefficients are less than those of
the nonlinear model of roughness. This implies to conclude that there
are other factors which influence the values of displacements and
consequently the vibrations generated between tool and workpiece.
5. Conclusions
A trial run within the framework of the experimental aspect of the
effect of the vibrations on the surface quality of the parts machined in
turning was carried out. The results obtained concerning the cutting
forces and the signals of accelerations, were treated in order to
calculated displacements in the vicinity of the nozzle of tool, as well
as displacements of the sleeve of pin and those of the frame.
The analysis of the results made it possible to define the relative
influence of the cutting parameters and the three components of the
displacement of the nozzle of the tool on the roughness of the machined
surface. The disturbances due to the vibrations with the interface
tool-part are quite present.
Because of rotation of the machined part, the geometrical
disturbances geometrical microphone along a generating line in a random
way. To analyze the experimental results a globalisation through a
statistical study was planned, this study led to the expression of two
mathematical models which make it possible to highlight the following
points:
* In the two worked out models, the model linear is more trustful
than the nonlinear model.
* The feed rates have a paramount impact on roughness in the linear
model. It acts in a direct way and by interactions with the cutting
speed.
* For the nonlinear model, the feed rate does not appear, but it
influences in an indirect way displacements radial and tangential of the
nozzle of the tool.
* The influence of cutting speed on roughness is appreciable in the
nonlinear model and acts by interaction in the linear model.
* The depth of cut does not have a great influence because it acts
only by interaction on roughness what is in agreement with the
literature.
* The components radial and tangential of the displacement of the
nozzle of the tool have a great influence on roughness.
* The machine used during our tests is sufficiently rigid and its
influence on roughness is negligible. In short, this study confirms the
former results on the importance from the parameters Vf kinematics and
[V.sub.c] for roughness. Moreover, it shows how displacements of the
nozzle of tool related to the vibrations also act on the geometrical
micro state of the machined surface.
The models suggested make it possible to quantify the relative
influence of these various parameters in the context of the experiments
which we undertook. These models have of an industrial interest some.
They allow on the one hand, the prediction of roughness according to the
cutting conditions and the displacement of the nozzle of the tool. In
addition in a context of optimization, they make it possible to
determine a combination of the factors studied to remain lower than a
limit of the criterion of fixed roughness.
Received June 272, 2011
Accepted December 19, 2012
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Hessainia Zahia *, Kribes Nabil *, Yalles M.A. *, T. Mabrouki **,
N. Ouelaa *, J.-F. Rigal **
* Laboratoire Mecanique et Structures (LMS), Departement de Genie
Mecanique, Universite 08 Mai 1945 de Guelma, BP 401, 24000 Guelma,
Algerie, E-mail:
[email protected]
** University of Lyon, CNRS, INSA-Lyon, LaMCoS, UMR5259., F69621,
France, Scientific field of Doua, Batiment Joseph Jacquard, 27avenue
Jean Capelle Villeurbanne
http://dx.doi.org/10.5755/j01.mech.19.1.3612
Table 1
Equipment used during experiments
Equipment Designation Characteristic
Machine-tool NC lathe Electric power: 12 KW
SOMAB T400 Spindle rotation: 3500 rpm
Material grade Steel: AISI 1045 Diameter: 61 mm;
Length: 300 mm
Cutting insert Coated carabide Squared form
CC4025 SNMG.12 0408
Insert Holder PSBNR/L2020K12 Squared section 20 x 20
Vibration Data acquisition card 8 overlap analogical entries
analyser NI PCI 4472 Sampling rate to
102.4 x [10.sup.3] samples/s
Data treatment Labview software Dynamic Analysis of signal
Accelerometer Endevco triaxial 15 g
2228C
Kistler 2012750 11 g
Kistler 2012748 11 g
Roughometer Mahr profilometer Nine parameters of roughness
Dynamometer Platform KISTLER 9257B Three components
Table 2
Test plan
Parameters Units Values
Working [V.sub.c], 90 ; 180 ; 200 ; 300
parameters m/min
[a.sub.p], 1 ; 2
mm
f, mm/tr 0.025 ; 0.05 ; 0.1 ; 0.2 ; 0.4
Measured [micro]m Ra, Rt, Rz, Rsm
parameters
N [F.sub.x], [F.sub.y], [F.sub.z]
m/ [a.sub.x] ; [a.sub.y] ; [a.sub.z] ;
[s.sup.2] [a.sub.s] ; [a.sub.f]
Calculated [micro]m dx, dy, dz, ds, df
parameters
Table 3
Obtained forces, accelerations displacement and roughness
according to cutting parameter variations
Parameters Forces
No. f Vc ap Fx Fy Fz
mm/tr m/min mm N N N
1 0,025 90 1 40,6 44,13 47,06
2 0,05 90 1 45,64 39,81 48,38
3 0,1 90 1 42,72 46,4 43,06
4 0,2 90 1 62,52 69,79 64,62
5 0,4 90 1 162,59 171,32 149,96
6 0,025 180 1 38,03 35,8 43,56
7 0,05 180 1 44,25 30,8 61,1
8 0,1 180 1 83,71 49,97 95
9 0,2 180 1 145,41 93,87 154,88
10 0,4 180 1 181,24 163,51 220,8
11 0,025 200 1 36,58 35 41,24
12 0,05 200 1 41,27 33,92 54,43
13 0,1 200 1 79,45 51,71 105,77
14 0,2 200 1 141,16 94,8 143,89
15 0,4 200 1 300 350 850
16 0,025 300 1 41,7 37,56 41,17
17 0,05 300 1 36,88 37 48,54
18 0,1 300 1 53,79 44,71 77,95
19 0,2 300 1 162,19 154,85 291,9
20 0,4 300 1 350 400 950
21 0,025 90 2 47,96 48 50
22 0,05 90 2 50,72 51 48
23 0,1 90 2 50,64 57 52
24 0,2 90 2 178,41 246 209
25 0,4 90 2 197,4 262 229
26 0,025 180 2 40 34 50
27 0,05 180 2 64 41 80
28 0,1 180 2 104 65 140
29 0,2 180 2 180 162 192
30 0,4 180 2 440 547 1048
31 0,025 200 2 40 41 55
32 0,05 200 2 62 45 64
33 0,1 200 2 120 72 140
34 0,2 200 2 159 152 216
35 0,4 200 2 500 750 1750
36 0,025 300 2 40 40 55
37 0,05 300 2 47 48 74
38 0,1 300 2 71 61 121
39 0,2 300 2 121 140 176
40 0,4 300 2 750 1050 2200
Accelerations
No. ax ay az as af
m/ m/ m/ m/ m/
[s.sup.2] [s.sup.2] [s.sup.2] [s.sup.2] [s.sup.2]
1 29,45 42,22 31,44 1,86 0,82
2 24,48 35,62 35,26 1,49 0,69
3 17,56 29,68 32,67 1,4 1,19
4 25,93 39,68 38,12 1,89 0,64
5 53,24 70,51 57,89 1,62 0,88
6 35,62 53,83 32,5 2,76 1,28
7 30,44 49,2 45,03 3,17 1,24
8 39,49 68,33 84,86 3,18 1,22
9 57,13 94,94 132,46 3,98 1,31
10 101,46 150,32 153,73 4,84 1,27
11 32,2 51,59 37,02 3,28 1,36
12 25 49,66 36,98 3,3 1,49
13 39,68 73,06 78,55 3,66 1,68
14 61,34 106 127,3 4,74 1,46
15 99,97 170,3 171,47 4,6 1,61
16 47,03 70,32 35,13 4,51 2,02
17 37,02 57,6 31,94 5,65 2,19
18 42,5 64,35 47,29 6,56 2,25
19 56,48 84,77 84,14 7,42 2,71
20 197,73 274,47 253,24 9,53 2,65
21 29 41 53 2,13 0,8
22 23 30 51 1,7 0,7
23 21 26 56 1,6 1,1
24 45 50 76 9 1,2
25 66 76 93 8,3 1
26 56 53 54 3,4 1,6
27 33 54 70 3,7 1,5
28 44 69 106 4,6 1,4
29 102 162 150 6,8 1,6
30 152 247 195 21,8 4
31 37 56 58 4 1,72
32 36 53 72 4,1 1,6
33 26,3 50 65,3 4,6 1,9
34 102 125 146 8,3 2,2
35 245 243 232 24,9 2,8
36 43 63 58 6,27 2,6
37 38 59 60 8,35 2,6
38 45 65 85 9,5 2,6
39 90 123 126 10,5 3
40 270 290 340 20 9
Roughness
No. Ra Rz Rt RSM
[micro]m [micro]m [micro]m [micro]m
1 3,31 18,31 24,54 202,21
2 1,3 9,7 19,31 186,08
3 0,72 4,09 5,83 102,83
4 1,52 9,15 11,59 183,13
5 6,04 26,38 28,03 401,19
6 1,59 9,79 19,75 270,12
7 0,59 3,68 4,67 50,69
8 0,97 5,11 6 69,26
9 1,5 8,24 9,17 202,08
10 5,4 26,05 30,17 402,4
11 2,11 12,09 16,81 177,32
12 0,91 6,77 16,32 65,82
13 1,12 6,11 9,54 109,25
14 1,52 8,48 8,89 201,5
15 5,85 26,65 29,15 402,44
16 1,29 7,4 10,08 89,59
17 0,71 3,96 4,2 50,27
18 1,03 4,94 5,56 98,78
19 1,61 9,03 10,98 200,64
20 5,13 24,35 26,68 378,55
21 2,46 14,3 18,02 163
22 0,84 5,99 8,01 91 53
23 1,03 5,52 5,92 98,56
24 2,22 10,56 12,38 206,71
25 6,39 27,94 30,16 389,28
26 2,79 17,74 25,97 175,36
27 1,43 10,44 15,7 108,89
28 1,2 5,44 6,28 98,78
29 2,36 11,16 13,54 197,08
30 5,9 28,62 30,4 393,63
31 2,27 11,57 17,79 129,76
32 1,29 6,89 8 85,98
33 1,27 6 6,56 98,53
34 2,42 9,9 10,85 197,11
35 6,44 28,75 31,16 392,65
36 2,47 12,3 18,41 145,06
37 1,01 7,8 11,1 78,84
38 1,47 7,66 9,36 95,89
39 2,58 10,19 10,87 197,25
40 6,02 29,72 31,84 386,17
Displacements
No. dx dy dz ds df
[micro]m [micro]m [micro]m [micro]m [micro]m
1 1,42 2,18 1,48 0,077 0,038
2 1,15 1,98 2 0,072 0,037
3 1,03 1,8 1,51 0,074 0,101
4 1,26 2,18 2,24 0,07 0,037
5 3,06 4,03 4 0,092 0,092
6 1,63 2,7 2 0,114 0,051
7 1,59 2,8 1,99 0,128 0,051
8 1,96 3,8 4,58 0,144 0,048
9 2,68 4,58 5,87 0,161 0,053
10 5,7 8,36 7,6 0,227 0,056
11 1,6 2,4 1,54 0,136 0,06
12 1,61 2,46 2,38 0,141 0,073
13 2,23 3,96 4,47 0,157 0,146
14 3,36 6,03 7,33 0,2 0,063
15 6,26 7,1 7,09 0,175 0,06
16 2,17 3,39 2,05 0,163 0,081
17 1,87 2,65 1,75 0,219 0,078
18 2,41 3,3 2,47 0,264 0,084
19 2,86 4,24 4,78 0,282 0,084
20 8 74 10,1 6,69 0,24 0,077
21 1,31 1,94 2,6 0,098 0,123
22 1,09 1 41 2,59 0,074 0,039
23 1,01 1,37 2,77 0,076 0,106
24 1,98 3,66 3,35 0,084 0,041
25 3,66 3,59 4,46 0,107 0,051
26 5,47 3,1 2,98 0,126 0,052
27 1,52 2,3 3,16 0,172 0,054
28 2,17 3,4 5,12 0,192 0,057
29 4,12 7,57 8,05 0,244 0,072
30 9 10,7 12,7 0,344 0,088
31 1,64 2,88 2,86 0,129 0,177
32 1,82 2,46 3,36 0,194 0,061
33 2,28 4,01 6,05 0,17 0,496
34 4 5,92 8,46 0,258 0,068
35 8,37 7,63 18,2 0,436 0,087
36 2,36 3,58 2,95 0,178 0,093
37 1,89 2,7 2,8 0,296 0,105
38 2,19 3,1 4,39 0,336 0,11
39 3,15 4,59 5,48 0,39 0,11
40 31,1 18,6 21,1 0,88 0,134
Table 4
Results obtained by regression analysis and variance
Parameters Coefficient P
Linear c = -0.458 0.038
model
dx i = 0.593 0.000
dz k = -0.183 0.000
[V.sub.c] q = 0.00247 0.000
[a.sub.p]
f a = 16.33 0.000
[V.sub.c] f p = -0.0517 0.000
Nonlinear Ln c = 3.59 0.000
model
dx [delta] = -0.256 0.005
dz [phi] = 1.18 0.000
[V.sub.c] [chi] = -0.709 0.000
Roughness models [R.sup.2]
Linear Ra = -0.458 + 0.593 95.6%
model dx - 0.183 dz +
+0.00247 ([V.sub.c]
[a.sub.p]) + 16.3f
0.0517 ([V.sub.c] f)
Nonlinear Ra = 36.23 90.7%
model [dz.sup.-0.256]
[dx.sup.1.18]
[V.sub.c.sup.0.709]