Cutting speed influence on surface integrity of hard turned bainite steel
-
Upload
michael-jacobson -
Category
Documents
-
view
214 -
download
0
Transcript of Cutting speed influence on surface integrity of hard turned bainite steel
Cutting speed influence on surface integrity of hard turned bainite steel
Michael Jacobson*, Patrik Dahlman, Fredrik GunnbergProduction Engineering, Chalmers University of Technology, Gothenburg, Sweden
Received 2 October 2001; received in revised form 4 July 2002; accepted 4 July 2002
Abstract
The purpose of this paper is to examine how the surface integrity of bainite steels is affected by hard turning. Tests were conducted on a
lathe using different cutting speeds. The surface was evaluated in terms of residual stress, surface roughness and microstructure analysis. Tests
showed that hard turning provides good surface integrity. Effect of cutting speed on residual stress was investigated in order to find how the
residual stress could be altered. It was found that there is a cutting speed where maximum compressive residual stress is generated. The surface
roughness of the hard turned test samples followed the same pattern; an certain cutting speed gives the lowest surface roughness values. The
surface of the test samples showed no or little alteration to the microstructure. Based on the results it can be concluded that hard turning of
bainite steel is a suitable manufacturing process.
# 2002 Elsevier Science B.V. All rights reserved.
Keywords: Hard turning; Surface integrity; Residual stress; Bainite steel
1. Introduction
The conventional method for producing precision pro-
ducts has been soft machining and heat-treatment, finishing
with rough and fine grinding, and finally honing the heat-
treated component. In order to increase flexibility of pro-
duction and make it more agile, manufacturers have realized
the potential of replacing the grinding operations with hard
turning. The turning lathe can incorporate more operations,
making it easier to reset, and it has fewer type-dependent
tools than a grinding machine. In short, the hard turning of
components is a more suitable technology for the production
of small lots than grinding.
In order to change from grinding to hard turning, three
levels of substitution can be recognised: the first level
substitutes rough grinding; the second level substitutes fine
grinding; and the last level includes substitution of the
honing operation. The more grinding and honing that can
be substituted, the greater are the benefits of hard turning.
In order to accomplish this, it is necessary to have good
knowledge of the surface integrity created by hard turning.
Field and Kahles [1] have defined surface integrity as the
relationship between the physical properties and the func-
tional behaviour of a surface. The surface integrity is built
up by the geometrical values of the surface such as surface
roughness (for example, Ra andRt), and the physical properties
such as residual stresses, hardness and structure of the surface
layers. Residual stress strongly affects the fatigue life of a
component. Brinksmeier et al. [2] give a good overview of
the subject of residual stresses. In their article, a comprehen-
sive description is given of different machining operations
and how they create different residual stress. The difference
in stresses created by different operations also affects the
performance of a machined component. Mittal and Liu [3,4]
present a more focused study on the effects of hard turning
on residual stress. Their work is divided into two parts. In the
first part, they show how different machining parameters in
hard turning affect residual stress. In the second part, they
describe a method to achieve optimal pre-stress in a com-
ponent to maximize fatigue life in a rolling contact. Their
work is groundbreaking in the sense that it suggests machin-
ing parameters should be optimised towards enhancing
fatigue life of the machined component.
Another interesting publication is Matsumoto et al. [5],
who conclude that hard turning produces compressive resi-
dual stresses that contribute to a long fatigue life. They also
determine that edge geometry is the dominant factor decid-
ing the residual stress profile. Similarly, Abrao and Aspin-
wall [6] report that hard turned components improve fatigue
life compared to ground components. Furthermore Fujimoto
and Ohhata [7] reports fatigue life improvements of 3–7
times. A possibility to enhance product life would add to the
list of previously discussed advantages of hard turning. In
addition, for demanding applications where performance is
Journal of Materials Processing Technology 128 (2002) 318–323
* Corresponding author.
0924-0136/02/$ – see front matter # 2002 Elsevier Science B.V. All rights reserved.
PII: S 0 9 2 4 - 0 1 3 6 ( 0 2 ) 0 0 4 7 2 - 7
critical, hard turning could provide increased protection
from rolling contact failure.
However, most of the prior studies on the effect of hard
turning on residual stress have been performed on 52 100, a
through-hardened bearing steel. There seems to be no work
done on the residual stress pattern from the hard turning of
bainite steel. Thus, an interesting research question is how
the bainitic heat-treated bainite will affect the results.
Changing the cutting speed is one of the most common
and easily done changes in the turning process. Therefore it
is of interest to know how this adjustment affects the surface
integrity. In this paper, the change of surface integrity when
adjusting the cutting speed while hard turning bainite steel
will be presented, in terms of residual stress, surface rough-
ness and microstructure.
2. Experimental procedure
Machining, residual stress measurements and the surface
roughness measurements were performed at Chalmers Uni-
versity of Technology, Gothenburg, Sweden. The micro-
structure was evaluated at SKF, Gothenburg, Sweden.
2.1. Machining conditions
Machining was done on a 2-axis lathe. The material of the
test rings was hardened steel B8 according to ISO 683-17.
Prior to the hard turning operation, the parts had been soft
turned and bainitic heat-treated to a hardness of HRC 58.
The chemical composition of bainite steel can be found in
Table 1. A 3-jaw chuck was used for the chucking. The outer
diameter of the rings was 310 mm, the inner diameter was
170 mm, and the width of the rings was 65 mm. The
operation performed was a facing operation with a depth
of cut of 0.1 mm from the inner diameter to the outer
diameter. The feed rate was kept to be 0.1 mm/rev for
all samples. The cutting speed was adjusted from 50 to
999 m/min for the test samples. All tests were performed
without coolant.
A CBN 100 insert constructed of cubic boron nitride
(CBN) and supplied by SECO was chosen for the test.
The full tool description is TNGN 110308-01015 CBN
100. The tool holder used for the tests had a �68 of rake
angle. Before each cut, the insert was changed to eliminate
the effect of tool wear.
2.2. Residual stress measurement
Residual stresses were measured with the X-ray diffrac-
tion method. Used equipment was a portable stress analyser
from Stresstech, Finland. A chromium tube calibrated on
ferrite was used to measure the {2 1 1} peak of steel. The
X-ray was generated using 35 kV and 7 mA. After several
test to evaluate the exposure time from 5 to 120 s it was
concluded that 15 s was enough to ensure good peak shapes.
The collimator size used was 2 mm, the calculation method
was cross correlation and the elastic constant applied in the
calculation was 204 GPa. In order to obtain the residual
stress beneath the surface, the material was chemically
etched away. Seven different measuring points were taken
along the depth profile. The stresses were evaluated both in
the feed and the speed direction.
2.3. Surface roughness measurement
The measurements were performed with a stylus probe
measurement equipment. The equipment is a Surfascan 3D,
and was delivered by Somicronic, France. The measured
surface size was 2 mm � 2 mm. The maximum height of the
profile (Rt) was measured.
2.4. Microstructure analysis
The samples were carefully sectioned in order to not
induce any transformation of the structure due to heat.
The samples were then mounted in a phenolic compound,
and ground and polished to a mirror-like surface with
different grit and diamond pastes. The next step was washing
and nital etching. Finally, the samples were inspected using a
100� to 1850� microscope.
3. Results
The results are presented in three different sections. First,
the evaluation of the residual stresses is presented. Second,
the surface roughness measurements are shown. Third, the
microstructure is presented. Combined, they provide a com-
plete picture of the surface integrity of the test samples.
3.1. Residual stress
Tables 2 and 3 show all measured values of residual stress.
When analysing the values, the following results were
obtained. On all samples, the compressive stresses increased
below the surface. Maximum compressive stress found
was 10–20 mm below the surface. A concentration of the
samples had a maximum around 10 mm. The maximum
value differed from �297 MPa on the sample with cutting
speed 50 m/min to �775 MPa on the sample with cutting
speed at 230 m/min. At a depth of 100 mm all samples
showed compressive stresses of less than �200 MPa.
Table 1
Chemical composition of steel B8 according to ISO 683-17
C 1.00
Mn 0.80
Si 0.50
Cr 2.0
Mo 0.60
Ni 0.10
Cu 0.15
M. Jacobson et al. / Journal of Materials Processing Technology 128 (2002) 318–323 319
It can also be concluded that the cutting speed effect
the amount of residual stress generated in hard turning. In
Figs. 1 and 2, the cutting speeds from 50 to 230 m/min are
compared. In Figs. 3 and 4 the cutting speeds from 230 to
999 m/min are compared. All other cutting conditions and
the cutting speed is kept constant. Figs. 1–4 clearly show
that the compressive residual stress reach a maximum at
around 230 m/min. Both measuring directions, speed and
feed direction show the same pattern.
3.2. Surface roughness
Due to the particular geometry of lathe machining, there
is a direct relationship between turning parameters and
the roughness of the machined surfaces. For the theoretical
Table 2
Residual stress (MPa) measured in speed direction at cutting speeds from 50 to 999 m/min
Depth (mm) Cutting speed (m/min)
50 80 110 170 230 290 500 999
0 �179 166 87 247 255 46 350 299
10 �245 �507 �605 �627 �775 �659 �542 �393
20 �319 �393 �420 �690 �570 �326 �252 �160
30 �178 �253 �274 �526 �326 �176 �126 �105
50 �84 �157 �146 �238 �140 �167 �121 �123
70 �74 �143 �135 �150 �51 �191 �101 �122
100 �79 �127 �161 �106 �54 �154 �139 �134
Table 3
Residual stress (MPa) measured in feed direction at cutting speeds from 50 to 999 m/min
Depth (mm) Cutting speed (m/min)
50 80 110 170 230 290 500 999
0 �203 �71 �165 �159 �131 �231 �22 �25
10 �297 �430 �508 �636 �680 �515 �387 �297
20 �297 �318 �360 �606 �415 �275 �185 �111
30 �213 �218 �215 �404 �252 �192 �133 �91
50 �177 �164 �159 �246 �110 �163 �149 �72
70 �102 �157 �128 �133 �123 �209 �170 �110
100 �111 �144 �133 �167 �72 �145 �171 �100
Fig. 1. Residual stress at cutting speeds from 50 to 230 m/min.
Fig. 2. Residual stress at cutting speeds from 50 to 230 m/min.
Fig. 3. Residual stress at cutting speeds from 230 to 999 m/min.
320 M. Jacobson et al. / Journal of Materials Processing Technology 128 (2002) 318–323
calculation of Rt the following formula from Capello et al.
[8] was used:
Rt �f 2
8re(1)
where Rt is the surface roughness from top to bottom, f the
feed rate, and re the tool nose radius.
The theoretical surface roughness from Eq. (1) was then
compared with the measured values (Table 4) and displayed
in Fig. 5. The Rt parameter was found to differ with the
cutting speed. Fig. 5 clearly shows how the surface rough-
ness reaches a minimum at the cutting speed of 170 m/min.
Fig. 6 shows how the surface looks when using the
optimum cutting speed of 170 m/min. The 3D illustra-
tions provide a good picture of how the surfaces look.
The feedmarks can be clearly seen. This 3D pictures did
not show any extremes in the sense that material is missing
or that there are high-ploughed hills.
3.3. Microstructure
The structure of the test samples was evaluated. In Figs. 7
and 8 the photos of the microstructure can be seen. Fig. 7
Fig. 4. Residual stress at cutting speeds from 230 to 999 m/min.
Table 4
Surface roughness (Rt) measured in feed direction at cutting speeds from
50 to 999 m/min
Cutting speed (m/min) Rt
50 2.8
80 2.7
110 2
170 1.7
230 1.9
290 2.6
500 3.9
999 4.5
Fig. 5. Surface roughness at cutting speeds from 50 to 999 m/min.
Fig. 6. 3D picture of surface, cutting speed 170 m/min.
Fig. 7. Microstructure at surface, cutting speed 50 m/min (1850�).
Fig. 8. Microstructure at surface, cutting speed 50 m/min (1850�).
M. Jacobson et al. / Journal of Materials Processing Technology 128 (2002) 318–323 321
shows no alteration to the surface. However on the same test
samples thin layer of changed structure could be found, see
Fig. 8. This white layer was less then 1 mm deep when using
cutting speed at 50 m/min. This type of transformed surface
was approximately found on less then 5% of the surface. The
reason for evaluating the test sample from 50 m/min was that
it showed the highest compressive stress values. It is there-
fore believed that the lower speed gives less heat and less
transformation of the surface layer. The white layer normally
gives tensile stress.
4. Discussion
The surface generated by hard turning bainite steel
depends on the machining conditions. This study has shown
how the cutting speed affect residual stresses. This study is a
small part of a bigger investigation on how different machin-
ing parameters affect the result generated in hard turning.
More then 100 residual stress profiles have been measured
with different machining parameters. This larger study
support that the cutting speed has this effect on residual
stress generated. The amount of error on an individual
sample deviates, depending on how well aligned the sample
is with the X-ray diffraction equipment. An average of
�20 MPa on the measured value is the normal error. The
stylus probe measurement equipment used for roughness
measurement showed stable results for roughness measure-
ments. The tests were conducted with machines and tools
used for normal production. The purpose was to test with
conditions as close as possible to normal production.
Results presented in this study are valuable since they
show that compressive residual stress can be generated when
bainite steel is hard turned. It is also clear that the amount of
compressive stresses generated can be altered depending on
the cutting speed. When residual stress is generated there is
an effect from both the heat generated and mechanical work
going in to the surface and subsurface. When increasing
cutting speed one also increase the strain rate in the process
which gives more mechanical work in to the process, leading
to compressive stress. When increasing the cutting speed
more heat is introduced in the process, which has a tendency
to produce tensile stress at the surface. This could explain
why the compressive stress first increase then later decrease
while increasing the cutting speed. The two opposing phe-
nomena counteract to create the final result.
The amount of residual stress that is beneficial for
improving bearing fatigue life differs with each application.
For a theoretical case Broszeit et al. [9] concluded that the
minimum equivalent stress maximum occurs when the
residual stress is �0.21 of the maximum Hertzian contact
pressure. Schreiber et al. [10] have a more practical
approach. In their study, they introduced different degrees
of residual stress by using different time periods when cold-
working bearing balls. The cold-worked balls were then
assembled into a 6206 deep groove ball bearing. After
assembly, a rolling contact fatigue test was performed.
The rig used a Hertzian contact pressure of 3500 MPa. This
more practical approach resulted in the conclusion that an
optimum of residual stress is achieved at around �600 to
�1000 MPa. Liu and Mittal [4] also concluded that in order
for a residual stress profile to have a favourable effect, at
every point on the service stress profile the residual stress
must be of the same sign as the service stress. Also, the
magnitude of the residual stress should be less than or equal
to twice the magnitude of the service stress. Service stress in
rolling contact is primarily compressive in nature. There-
fore, for the initial residual stresses to be beneficial, they also
must be compressive.
Bearing this in mind, it is clear that hard turning of bainite
steel can be favourable in terms of improving fatigue life.
The measured values fall in the range mentioned above, and
can be altered to suit different applications.
The equation for Rt (Eq. (1)) only accounts for the
geometric portion of the roughness. The geometric rough-
ness and secondary roughness have been well described by
Capello et al. [8]. The real surface finish is a combination of
the geometric roughness and the secondary roughness
derived from the plastic flow of the material, the removal
process, the tool wear, the tool, and workpiece chatter
among others. The equation is useful for medium and high
levels of surface roughness, since the geometric portion
dominates the roughness value. For lower levels of rough-
ness, the model systematically underestimates the real sur-
face roughness, because in this case the secondary roughness
becomes more significant than geometric roughness. When
analysing the surface it becomes clear that when the cutting
speed is low, too low temperature is reached in the cutting
zone and the material is hard to cut. On the other hand if the
cutting speed is to high the amount of heat generated makes
the material soft enough to escape the cutting edge. When
cutting with 170 m/min the right temperature is reached and
roughness depends only on the geometric roughness. The
surface roughness value Rt then fits Eq. (1) well.
A white layer is a result of microstructure alteration. It is
called a white layer because it resists standard etchants and is
white under an optical microscope. In addition, white layers
often produce tensile stresses at the surface. An interesting
question is however this very thin layer has a detrimental
effect on fatigue life. White layer produced in grinding and
in hard turning is not the same thing, this is well described by
Konig et al. [11].
With the information available concerning the surface
integrity, there is indication that hard turning of bainite steel
is a possible process. An interesting next step would be to
perform a fatigue test with hard turned components. Mittal
and Liu [3] have already shown that an extremely good
surface finish can be obtained with hard turning. The
robustness of the process also must be documented. Konig
et al. [12] showed how the surface of a 52 100 component at
first is compressive, but soon turns to tensile when tool wear
appears.
322 M. Jacobson et al. / Journal of Materials Processing Technology 128 (2002) 318–323
5. Conclusions
Tests were conducted to find the effect of hard turning on
the surface integrity of bainite steel. The outcomes were
reported as residual stress, surface roughness and micro-
structure analysis. From the analysis of experimental data
and discussions, the following conclusions can be drawn:
� Hard turned bainite steel consistently shows the same
residual stress profile along the depth. The amount of
compressive stress increases to a maximum of �775 MPa
around 10 mm below the surface. At a depth of 100 mm,
the effect from hard turning on residual stress is small.
� The cutting speed clearly affects the amount of residual
stress generated in hard turning. Maximum compressive
stress is generated at a cutting speed of 230 m/min.
� The level of compressive residual stress produced is,
considering the literature, at the right level to have a
positive effect on rolling fatigue life.
� The cutting speed affects the surface roughness. At a
speed of 170 m/min a minimum Rt value is found. This
correlates well with the surface roughness that can be
predicted from Eq. (1).
� The microstructure analysis showed little or no alteration
to the surface or subsurface.
Acknowledgements
The authors would like to thank SECO and SKF. The
authors is also grateful for the funding received from Vinnova.
References
[1] M. Field, J. Kahles, Review of surface integrity of machined
components, Ann. CIRP 20 (2) (1971) 153–163.
[2] E. Brinksmeier, J.J. Cammett, P. Leskovar, J. Peters, H.K. Tonshoff,
Residual stresses-measurements and causes in machining processes,
Ann. CIRP 31 (1982) 491–510.
[3] S. Mittal, C.R. Liu, A method of modelling residual stresses in
superfinish hard turning, Wear 218 (1998) 21–33.
[4] C.R. Liu, S. Mittal, Optimal pre-stressing the surface of a component
by superfinish hard turning for maximum fatigue life in rolling
contact, Wear 219 (1998) 128–140.
[5] Y. Matsumoto, F. Hashimoto, G. Lahoti, Surface integrity generated
by precision hard turning, Ann. CIRP 48 (1) (1999) 59–62.
[6] A.M. Abrao, D.K. Aspinwall, The surface integrity of turned and
ground hardened bearing steel, Wear 196 (1996) 279–284.
[7] Y. Fujimoto, O. Ohhata, Providing Residual Stress by Machining
after Heat-treatment, Elsevier, Amsterdam, 1992, pp. 1350–
1355.
[8] E. Capello, P. Davoli, G. Bassanini, A. Bisi, Residual stresses
and surface roughness in turning, J. Eng. Mater. Technol. 3 (1999)
346–351.
[9] E. Broszeit, Th. Preussler, M. Wagner, O. Zweirlein, Stress hypo-
theses and material stresses in Hertzian contacts, Z. Werkstofftech. 17
(1986) 238–246.
[10] E. Schreiber, W. Simon, H.-W. Zoch, Work hardening of ball
surfaces, ASTM Special Technical Publication, Symposium on
Creative Use of Bearing Steels, no. 1195 (1993) 81–92.
[11] W. Konig, A. Berktold, J. Liermann, N. Winands, Top-quality
components not only by grinding, Ind. Diam. Rev. 54 (562) (1994)
127–132.
[12] W. Konig, A. Berktold, K.-F. Koch, Turning versus grinding—a
comparison of surface integrity aspects and attainable accuracies,
Ann. CIRP 42 (1993) 39–43.
M. Jacobson et al. / Journal of Materials Processing Technology 128 (2002) 318–323 323