Abstract:
Sustainability in manufacturing can be realized by developing a machining system,
that reduces consumption of resources for converting raw materials into useful product.
Moreover, it must produce waste that can directly be used by another production
system as an input material. Intentionally inducing vibration to make machining system
sustainable in this regard started from the work of Kumabe [2]. Based on the direction
of modulation with respect to workpiece motion, three distinct effective conditions
develop; Vibration Assisted Machining (VAM) having low amplitude and high frequency
vibration in the cutting velocity direction, Modulation Assisted Machining (MAM)
having high amplitude and low frequency vibration in tool feed direction and Elliptical
Vibration Assisted Machining (EVAM) possesing low amplitude and high frequency
vibration both in tool feed as well as cutting velocity directions. Vibration in machining
helps to increase the tool life and reduce overall cost of production. Moreover, it also
helps in improving tool chip contact conditions so as to improve surface finish. For
superimposing vibration to tool motion, the use of piezoelectric transducer device based
tool holder attachments has been reported and investigated. Imposition of oscillation
in machining reduces the cutting forces and burr suppression, which further decrease
the energy consumption and hence make the system energy efficient. Moreover, MAM
has been used to produce chips of required shape and size distribution, which can be
used by another production system as an input material without any post processing.
The austenitic stainless steel AISI 316 (316 SS) is considered as one of the difficultto-machine
materials due to its low thermal conductivity and high work-hardening
rate. Despite the fact that these steels are of great significance, still there exist some
technical gaps about their behavior during machining. During drilling, severity of
contact conditions at chip-tool interface plays a significant role in tool life and quality of
the hole produced. Different techniques such as different types of coatings, lubrication
systems and drilling strategies have been used for improving the conditions of tool-chip
interface. Glass fibre reinforced plastics (GFRP) can offer several promising mechanical
properties, which include high specific strength, stiffness and damping, along with low thermal expansion coefficient. These properties of laminates have made them to replace
metallic materials as structural elements in several defence and aerospace applications.
It has been reported that during the conventional drilling of GFRP, rejection rates are
on higher side due to the damage around the holes. Several measures to control such
damages have been investigated, which include proper tool material selection, tool
point design, use of optimized feed rates and cutting speeds, development of special
manufacturing strategies and modeling of cutting forces.
The scope of the present investigation has been chosen to evaluate the effect of tool-chip
contact disruption during modulation assisted drilling (MAD) of 316 SS and GFRP
on quality of the holes produced, cutting forces and tool wear. Moreover, in MAM
disruption of tool-chip contact during machining helps in formation of discontinuous
chips from the alloys, which otherwise produce continuous chips in conventional
machining. This capability of MAM has been investigated to produce controlled size
and shape chip particulates of brass. Furthermore, characteristic studies of these
particulates have been done to explore the effect of MAM on their properties.
A patented tool holder (TriboMAM) was retrofitted on the CNC lathe for centerline
drilling during drilling experiments. Piezoelectric sensor based dynamometer was
used for force and torque measurements. A roughness tester (Talysurf) was used for
surface roughness measurements. An optical microscope (Leica) was used to take
images of the surface produced using modulation and conventional drilling. Maximum
flank wear, (V Bmax), was measured by a tool maker’s microscope. The used drills
were inspected under SEM to establish the possible wear mechanism. It was observed
from the drilling force data that the effect of feed rate was remarkable on the thrust
force in conventional drilling (CD) as well as modulation assisted drilling (MAD).
With increase in feed rate, thrust force increased drastically. The effect of rotational
speed on the thrust force was found to be insignificant and no noticeable change was
observed in thrust force with increase in rotational speed during CD and MAD for
the investigated range of parameters. Moreover, mode of drilling has been observed
to be significant with regard to its influence on thrust force. As the mode of drilling
changed from CD to MAD, significant reduction in thrust force was observed. It was
observed from the results that the highest surface finish could be obtained in the case
of modulation assisted drilling. Whereas,the worst surface finish was produced in the case of conventional drilling. Modulation assisted drilling outperformed conventional
drilling in surface finish at almost every investigated feed and speed combinations. A
comparative analysis of the wear performance of tungsten carbide drills used in CD
and MAD indicated that the drills used in MAD were better in resisting tool wear than
those used in CD. The recorded percentage reduction in the tool wear of drill used in
MAD over the drill used in CD is about 44.4% for the cutting speed of 32.9 m/min
and feed of 0.015 mm/rev. However, at a higher feed of 0.03 mm/rev during MAD, a
catastrophic failure of drill occurred due to fracture of cutting edge. The impact-type
cyclic loading on cutting edge is believed to increase with the increase in value of
the feed. The direction of force acting on tool edge and the enhanced magnitude of
cyclic loading may be the reason for tool edge fracturing in MAD at higher feeds. An
in-depth analysis of SEM and optical micrographs of flank wear on the drills used in
MAD and CD revealed that the MAD effectively enhanced the cutting life of drills by
resisting adhesion wear and plastic deformation.
In the case of drilling experiments on GFRP, tool maker’s microscope was used to
measure delamination around the holes produced during CD and MAD. Moreover,
hole size was measured using a coordinate measuring machine (CMM). It has been
observed that damage due to delamination in GFRP laminates depended on the mode
of drilling, feed and rotational speed. Among them, the mode of drilling has been
observed to be the most significant factor for the drilling induced damage. Moreover,
the damage around hole was found to increase with speed and feed in CD. Holes with
less damage were produced in MAD at higher feed and speed. A maximum value
of delamination factor was found in CD at a speed of 2400 rpm and feed of 0.105
mm/rev. At the same drilling conditions with MAD, approximately 49% reduction in
delamination factor value was observed, which indicates the benefits of MAD over CD.
A reduction in the damage zone around holes may be attributed to the intermittent
contact breakage between tool and chip during MAD. It is believed that due to the
intermittent contact in MAD, instantaneous force becomes zero during each modulation
cycle, thus reducing average thrust force. Cutting force analysis showed that the effect
of feed rate is remarkable on the thrust force in CD as well as MAD and with increase
in feed rate, thrust force increased drastically. It is perceptible that an increase in
feed rate increased the section of sheared chip, so the GFRP resisted the rupture to a greater extent and it required larger efforts for the chip removal. The effect of
rotational speed on the thrust force during drilling of GFRP has been found to be
insignificant and no noticeable change was observed in thrust force with increase in
rotational speed during CD and MAD. Moreover, the mode of drilling has been found
to be a significant parameter for its influence on thrust force. As the mode of drilling
changed from CD to MAD, a significant reduction in thrust force was observed. It is
perceptible that the contact breakage in intermittent cutting during MAD helped in
zeroing the instantaneous thrust force. Zeroing of instantaneous thrust force further
reduced the mean thrust force value. ANOVA analysis for means value of output
response (hole size) showed that only feed was the significant parameter. Other two
parameters (mode of drilling and rotational speed) have been found to be insignificant.
Oversize of the hole was found to reduce with the increase in feed value. Holes with
less deviation could be produced in conventional drilling at higher feed and lower speed
values. Increase in feed has been found to limit the skidding motion of drill, which
may further have reduced the hole oversize. Empirical relation between delamination
factor and investigated parameters was established using nonlinear regression analysis.
For particulate production experiments a specially made tool of HSS was used. SEM
and Tool maker’s microscope were used to analyze the size and morphology of the
particulates. In MAM, modulation frequency (fm) and workpiece rotational frequency
(fw) determine the contact time of the tool with the workpiece and affect the resultant
particulate length. This is evident that, an increase in workpiece rotational frequency
requires increase in modulation frequency to create particulates of equivalent length.
Feed rate (h0) and modulation amplitude (A) describe the axial position of the tool at
any point of time, defining the chip thickness and cross-sectional shape of the resultant
particulates. Similarly, increased feed rates require increased modulation amplitudes
to ensure interrupted cutting and deformation of particulates. Any determination of
particulate morphology must account for each of these variables. In MAM, particulate
formation will occur as long as the modulation amplitude is sufficiently large for
undeformed chip thickness (s0) to reach zero during each cycle of the modulation and
frequency of modulation (fm) is not an integer multiple of frequency of workpiece
rotation (fw).
For deformation analysis of the bulk brass and chip particulates, X-ray diffraction (XRD) data was used. After obtaining X-ray patterns, line broadening analysis
was used to measure the level of deformation. In order to obtain internal strain,
Williamson-Hall method and for calculating crystallite size, Scherrer method were used.
Metallurgical studies of the bulk brass and chip particulates were done using optical
microscopy, SEM and EBSD, whereas for mechanical characterization, micro-hardness
and nano-hardness testers were used. The particulates of different shapes and sizes
ranging from 100 µm to 5 mm with aspect ratio of ∼ 10 were produced using different
modulation and machining conditions by MAM. Average shear strain for the chip
length ratio of 0.511 was found to be 2.32 for the particulates. Shear strain analysis
showed that the variation in deformation level in chip particulates produced at different
fm/fw ratio is less than 5%. It has also been found that the modulation parameter did
not affect the level of deformation in chip particulates. It has been observed that with
a decrease in chip particulate size, the crystallite size also decreased, while the internal
strain increased. With an increase in the value of fm/fw ratio, the chip lengths became
increasingly smaller; however, there was no noticeable difference in microstrain and
crystallite size of these chips.
In comparison to the bulk brass, the chips produced at different fm/fw ratios have
been found to have smaller crystallite size, however with increased microstrain. This
change in crystallite size and microstrain may be attributed to the severe plastic
deformation (SPD) taking place during MAM. This SPD may have increased the
defects in chip particulates, thereby changing the microstrain and the crystallite size of
the particulates. It has been observed that with decrease in particulate size, internal
strain increased and crystallite size decreased. The results of microstructural analysis
showed that there existed an ultrafine grained microstructure at the edge of chip
particulates, while the central area of the chip particulates had elongated and equiaxed
grained microstructure. EBSD analysis show that chip particulates have a refined
grain structure in comparison to the bulk brass. Texture analysis from pole figure and
misorientation plots showed the evolution of different texture in bulk brass and chip
particulates. The results of the nano-indentation showed that hardness and Young’s
modulus of chip particulates were higher, which may be attributed to the bimodal
ultrafine microstructure observed in the chip particulates.