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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072
Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1508
INVESTIGATION AND NUMERICAL ANALYSIS OF MILLING CUTTER
1PG Student, Department of mechanical Engineering, Bhilai Institute of Technology, DURG, Chhattisgarh, India
2Associate Professor, Department of mechanical Engineering, Bhilai Institute of Technology, DURG, Chhattisgarh
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - milling is a reliable method to recreate the
down graded structures, and parts. Yet, -milling still defies
some huge challenges, tormenting further arrangement of
this development. The most noticeable aroundthemisstress
formation. Stress made along the finishededgesandsurfaces
in - milling activity have gigantic impact at surface quality
and conduct of the finished parts and structures. One of the
methods to minimize stress formation in milling is by
enhancing the geometry of the device The principle point of
the examination work is to show finite element analysis of
flat end mill cutters used in milling by fluctuating the
geometry of the tools. Stress formation simulation has been
carried out while varying the tool geometry. The outcomeof
the research will be a static finite element analysis of stress
formed during -milling which can help in determining tool
life and a detailed dynamic analysis of stressformedduring-
milling operation in AlSi 1045 which can benefit the
aerospace industry in various ways. The outcome obtained
during the investigation may be used for furtherresearchfor
stress minimization through tool optimization and process
control.
Key Words: Milling, Stress formation in milling, Finite
element analysis, End mill cutter, Geometry of tool, AlSi
1045, Optimization.
1.INTRODUCTION
The manufacturing of extensive range of parts and items in
different fields, such asin automobile, airplanes, biomedical
equipment’s, and electrical and electronic gadgets requires
appropriate tolerance fit for appropriate coupling and
working of items. An assortment of activities like drilling,
boring, turning, grooving, EDM and ECM slicing are used to
manufacture and complete parts. A standout amongst the
most well-known and essential type of machining is the
milling cutting, in which material is removed from the work
piece as little chips by encouraging it into a turningshaperto
make the desirable shape. Milling is regularly usedtodeliver
parts that are not pivotally symmetric and have different
highlights, for example, gaps, spaces, pockets,andeventhree
dimensional surface shapes.
1.1 Analytical Modeling of Mill cutter
The examination of the advance of cutting powers in any
machining technique is significantly key for fitting,
organizing and control of machining process and for the
upgrade of the slicing conditions to limit generation costs
and times. Cutting power examination accept a basic part in
investigation of the diverse characteristics of a machining
procedure, viz. the dynamic strength, arranging accuracy of
the instrument with respect to the work piece, brutality of
the machined surface and structure missteps of the
machined segment, et cetera.
In most-end-preparing tasks, the cutting gadget estimation
contrasts from and uneasiness assortment on the humble
shaft of the cutting device is considerably higherthanthaton
a normal scale instrument, whichunquestionablycurtailsthe
instrument'slife (Li et al. [2007]). The apparatusescan even
break if the cutting conditions are not picked in likemanner.
Hence, a correct estimation of the cutting forces of - end-
processing accept a basic part in controlling theassuranceof
cutting conditions with a particular ultimate objective to
fiscally secure high machining quality and certification as
long an instrument life as could be normal the situation
being what it is. At level, we can't acknowledge that edge
sweep impactsly affects cutting forces. Weule et al [2001]
found that the roundnessof a front line is more basic atscale
machining. As the traverse of an instrument diminishes, the
sharpness of the device can't be updated respectably
because of stipulations in the mechanical get together
creation methodologiesand lessening in the basicideaofthe
instrument. Thusly, the feed per tooth in - preparing might
be for all goalsand reason unclear to or even shy of what the
forefront traverse due to the obliged reach of approach
parameters for a stable machining scale with the technique.
Yuan et al. [1996] chipped away at ultraprecision machining
to decide least chip thickness. Kim et al [2004] probably
affirmed that when the feed per tooth is essentially
indistinguishable with the edge span of the mechanical
assembly, as is every now and again the case in - processing
approaches, the chip forming philosophy gets intermittent
and the acknowledged appreciation that a chip is confined
with every tooth pass is not any more genuine. As
demonstrated by their model, the base chip thickness of
variousunions of gadgets and work piece materialsmightbe
assessed centered around easily achievable cutting power
data.
1.2 Analysis of Milling Cutter
The milling cutter is a symmetrical body subsequently the
examination is done thinking about a solitary tooth of the
cutter. Here, the examination is done for the situation of 5
diverse axle speeds going from 50 to 2000 rpm.The loads at
these rates are computed and the comparing Stresses
following up on the tooth are found. Stress and distortion of
the cutter at speed 50 rpm to 200rpm are obtained.
Indrajeet Rajpoot1, Mrs Shabana Naz Siddique2
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072
Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1509
FEA comprises of utilizing a PC model of a material or
design that is pushed and examined for particularoutcomes.
It is utilized as a part of the advancement of new item
configuration to check potential imperfections and in
existing item refinement. The framework can put various
heaps of a model to mimic genuine circumstances that the
item could be understanding.
Architects all through the business enhance item outlines
with FEA programming from ANSYS. Unequivocal Dynamics
with ANSYS expected for vast disfigurement recreations
where inactivity powers are predominant Used to reenact
Machining, quick framing, affect and so on
1.3 Model Validation
An experimental result is taken from the literature for the
simulation validation. A large number of theoretical and
experimental studies on surface profile and roughness of
machined products have been reported. These studies show
that cutting conditions, tool wear, the material properties of
tool and workpiece, as well as cutting/process parameters
significantly influence the surface finish of machined parts.
Therefore, it is of particular importance that the numerical
analysis is an attractive alternative for evaluating residual
stresses allowing substitute the application of high-cost
experimental methods. On the other hand, some of the
computationalresults do not correlate withtheexperimental
findings. In summary, despite the fact that there existsalarge
variety of different analytical, numerical and experimental
techniques, currently, there is no proven analytical model
enabling to reliably predict the residual stresses that arise in
the course of cutting operations.
For guaranteeing dependability ofthe createdFEmodelit
must be checked againsttrialdatawhichincorporatessizesof
the deliberate cutting force. Cutting force is a parameter
which is also evaluated for the structural design of machine
tools, selectionof optimum cutting parameters, the design of
workpiece-holding fixtures, tool stress analysis, spindle
bearingdesign, andthereal-timemonitoringoftoolwearand
breakage. This study proposes an FE model for a case of the
milling process. The milling operation is performed
by using end–milling tool – a cutting tool of complex
geometry that is used for machiningofsurfaces.Therefore,an
FE model was constructed for performing mesoscopic
analysis of the milling process in terms of the removed
material cut cross-section. Cutting forces were evaluated
during experimental testing, while the effect of the cutting
force on a single cuttinginsert wasdetermined by meansofa
transformation matrix.
Furthermore, it was confirmed with respect to material
deformation that it is necessary to apply several criteria for
verification of the FE model. Therefore, numerical analysis
was carried out by using dynamic material characteristics
taken from the available literature sources, meanwhile,
dynamicmaterial deformation constantswereacquiredfrom
the performed turning experiments.
Table -1: Validation between Experimental and FEA
N
o.
V
(m/mi
n)
𝑓𝑧(mm/
z)
π‘Žπ‘(m
m)
π‘Žπ‘’(m
m)
Experimental FEA
𝜎π‘₯(MP
a)
πœŽπ‘¦(M
Pa
𝜎π‘₯(MP
a)
πœŽπ‘¦(M
Pa
1. 314 0.06 3 6 64.83 55.37 71.80 53.36
2. 502 0.06 4 10 63.56 45.49 65.68 46.10
3. 628 0.06 5 12 59.18 44.83 63.38 43.22
4. 942 0.06 6 8 57.57 30.85 53.26 35.07
Cutting speed of in m/min, feed rate of mm/z, and depth of
cut and width of cut were in mm.
1.4 Meshing
Meshing can be done by using tetrahedral or hexahedral
elements. More the no. of nodes in the element type, the
greater is the accuracy of the results obtained. Tetrahedral
meshing is a powerful cross-section routine and is a less
demanding method for the lattice. Be that as it may, direct
tetrahedral componentsperform inadequatelyinissueswith
versatility, almost incompressible materials, and intense
bowing.
Hexahedral components, then again, give more precise
outcomes than tetrahedral components, in the event of
complex structures. They additionally think about lesser
measure of approximations. Be that as it may, hexahedral
components confront troubles at corners of
parts/components. Additionally, programmed work age is
regularly not plausible for building numerous three
dimensional hexahedral meshes.
Meshing and analysisof the milling operation havebeen
carried out using ANSYS 18.2 software. The mesh generated
for the end mill cutters in this work is a tetrahedral mesh.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072
Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1510
Figure -1: Meshing of milling cutters
Figure-2: Meshing of Workpiece
2. ANALYSIS AND RESULTS
So as to watch pressure arrangement and chip stream
component in a virtual situation, an unequivocal
investigation must be done on the apparatus and workpiece
collaboration. In this paper, we have accomplished a similar
utilizing ANSYS programming. Two distinctive two
woodwind end plants have been utilized fordynamiclimited
component investigation. Lager has been utilized for doing
the examination. Reference outline for the apparatusisbeen
Langrangian and that for the workpiece is been Eulerian.
Fig -3: Stresses on Shell End Mill Cutter at (00, 100& 200)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072
Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1511
Table 2: - Stresses on Shell End Mill Cutter
Keeping in mind the end goal to get required cooperation
between the two bodies, the required body communication
limitations among them must be characterized
appropriately. Since the covetedoutcomeisthereproduction
of machining task, the contact between the instrument and
the work piece must be frictional in nature. At the point
when the device keeps running over the work piece, the
erosion produces warm vitality. The chip conveys the
warmth from the work piece and discharges it in nature.Soa
frictional contact is characterized between the apparatus
and the work piece. The static coefficient of grating iskeptto
be 0.39 and the dynamic coefficient of contact is kept to be
0.32 (Raczy et al.).
The work piece is settled from three countenances. The two
side countenances are given zero level ofopportunityasthey
are compelled utilizing mechanical installations while
machining. The lower surface is given zero level of
opportunity as they are held utilizing vacuum installations.
The device is furnished with a precise speed of 20,000 rpm
(Campos et al. [2013]). In the information factors,
instrument is furnished with a direct speed, which speaksto
the feed rate of our machining activity. The feed rate in our
setup is settled to be 500 mm/sec (Campos et al. [2013]).
The end time determines the no. of emphasess to be
performed by the solver and educates the solver when to
stop the procedure. Since the work piece is 20 mm long, and
the feed rate is 500 mm/sec, an end time of 0.05 seconds
was picked with the goal that the whole instrument length
can be canvassed in the reproduction. The aggregate time
taken keeping in mind the end goal to understand is 120
hours.
No. V
(m/min)
𝑓𝑧(mm/z) π‘Žπ‘(mm) π‘Žπ‘’(mm) Rack Angle
0 degree 10 degree 20 degree
𝜎π‘₯(MPa) 𝜎y(MPa) 𝜎π‘₯(MPa) πœŽπ‘¦(MPa) 𝜎x(MPa) πœŽπ‘¦(MPa)
1. 314 0.06 18 5 171.65 124.78 154.92 90.54 85.65 55.65
2. 502 0.06 20 6 249.65 159.65 179.46 126.10 113.87 63.87
3. 628 0.06 22 8 256.19 176.19 214.56 132.12 150.17 70.17
4. 942 0.06 24 10 267.31 207.31 228.31 142.51 148.51 82.51
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072
Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1512
Figure-4: Stresses on Flat End Mill Cutter at (60, 80& 100)
in the case of two flute micro end mills
Table 3: - Stresses on Flat End Mill Cutter of two flute
micro end mills
No. V (m/min) 𝑓𝑧(mm/z) π‘Žπ‘(mm) π‘Žπ‘’(mm) Rack Angle
6 degree 8 degree 10 degree
𝜎π‘₯(MPa) 𝜎y(MPa) 𝜎π‘₯(MPa) πœŽπ‘¦(MPa) 𝜎x(MPa) πœŽπ‘¦(MPa)
1. 314 0.06 18 5 110.33 81.25 95.17 68.23 93.07 66.12
2. 502 0.06 20 6 99.49 71.03 82.50 56.72 80.08 54.30
3. 628 0.06 22 8 98.84 69.10 79.53 53.50 76.56 50.54
4. 942 0.06 24 10 92.72 63.15 71.08 46.29 67.64 42.84
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072
Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1513
Figure-5: Stresses on Flat End Mill Cutter at (60, 80& 100)
in the case of two flute micro end mills
Table-4: Stresses on Flat End Mill Cutter of two flute
micro end mills
Figure-6: Stresses on Shell End Mill Cutter at (60, 80&
100) in the case of four flute micro end mills.
3. CONCLUSIONS-
Stress formation is a major hindrance to good surface finish
in case of both macro and milling. However, stressformation
in case of milling is of greater importance than in case of
conventional milling as stress formed in the former case are
of sub-meter size and distressing processes are expensive,
and sometimes impossible. Hence, stress minimizationisthe
only way of obtaining good surface finish in structures.
To minimize formation of stressin case of milling, either the
cutting conditions or the tool geometry can be optimized. In
this work, tool geometry improvement has been tried to be
accomplished by performing FE analysis on tools with
different setsof rake and relief angles, for both two fluteand
four flute end mills and for Shell end mills. The results of the
finite analysis of the shell and flat end milling tools offer the
conclusion that in the given cutting conditions, the least
amount of Von Mises stress generated in case of a shell end
mill at 10o and 20o, two flute flat end mill cutter is for a
cutter having rake angle 8ΒΊ and relief angles of 6ΒΊ and thatin
the case of four flute end mill cutter is for a cutter having
rake angle 6ΒΊ and relief angle 8ΒΊ.
FE dynamic analysis of the tool-chip interaction
in the milling process as performed and stress formation
process was simulated using ANSYS software. It shows
that as the rack angle increases stresses decrease.
4. REFERENCES
[1] Afazov, S.M., Ratchev, S.M. and Segal, J., Modelling and
simulation of -milling cutting forces, Journal of
Materials Processing Technology, Vol.210, pp. 2154-
2162 (2010).
[2] Alrabii SA, An experimental study of stress formation
in drilling and slot-end milling operations, Journal of
Engineering, 15(4) (2009) 4219- 4240.
[3] Ávila M, Gardner J, Reich-Weiser C, Tripathi S,
Vijayaraghavan A, Dornfeld D. Strategies for Stress
Minimization and Cleanability in Aerospace and
Automotive Manufacturing. SAE Transactions Journal
of Aerospace, 114 (1), pp. 1073-1082 (2006).
[4] Bao WY, Tansel IN, Modeling -end-milling operations.
Part I: analytical cutting force model, International
Journal of Machine Tools & Manufacture, 40 (2000)
2155-2173.
No. V
(m/min)
𝑓𝑧(mm/z) π‘Žπ‘(mm) π‘Žπ‘’(mm) Rack Angle
6 degree 8 degree 10 degree
𝜎π‘₯(MPa) 𝜎y(MPa) 𝜎π‘₯(MPa) πœŽπ‘¦(MPa) 𝜎x(MPa) πœŽπ‘¦(MPa)
1. 314 0.06 18 5 110.33 81.25 95.17 68.23 93.07 66.12
2. 502 0.06 20 6 99.49 71.03 82.50 56.72 80.08 54.30
3. 628 0.06 22 8 98.84 69.10 79.53 53.50 76.56 50.54
4. 942 0.06 24 10 92.72 63.15 71.08 46.29 67.64 42.84

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Numerical Analysis of Milling Cutter Stress

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072 Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1508 INVESTIGATION AND NUMERICAL ANALYSIS OF MILLING CUTTER 1PG Student, Department of mechanical Engineering, Bhilai Institute of Technology, DURG, Chhattisgarh, India 2Associate Professor, Department of mechanical Engineering, Bhilai Institute of Technology, DURG, Chhattisgarh ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - milling is a reliable method to recreate the down graded structures, and parts. Yet, -milling still defies some huge challenges, tormenting further arrangement of this development. The most noticeable aroundthemisstress formation. Stress made along the finishededgesandsurfaces in - milling activity have gigantic impact at surface quality and conduct of the finished parts and structures. One of the methods to minimize stress formation in milling is by enhancing the geometry of the device The principle point of the examination work is to show finite element analysis of flat end mill cutters used in milling by fluctuating the geometry of the tools. Stress formation simulation has been carried out while varying the tool geometry. The outcomeof the research will be a static finite element analysis of stress formed during -milling which can help in determining tool life and a detailed dynamic analysis of stressformedduring- milling operation in AlSi 1045 which can benefit the aerospace industry in various ways. The outcome obtained during the investigation may be used for furtherresearchfor stress minimization through tool optimization and process control. Key Words: Milling, Stress formation in milling, Finite element analysis, End mill cutter, Geometry of tool, AlSi 1045, Optimization. 1.INTRODUCTION The manufacturing of extensive range of parts and items in different fields, such asin automobile, airplanes, biomedical equipment’s, and electrical and electronic gadgets requires appropriate tolerance fit for appropriate coupling and working of items. An assortment of activities like drilling, boring, turning, grooving, EDM and ECM slicing are used to manufacture and complete parts. A standout amongst the most well-known and essential type of machining is the milling cutting, in which material is removed from the work piece as little chips by encouraging it into a turningshaperto make the desirable shape. Milling is regularly usedtodeliver parts that are not pivotally symmetric and have different highlights, for example, gaps, spaces, pockets,andeventhree dimensional surface shapes. 1.1 Analytical Modeling of Mill cutter The examination of the advance of cutting powers in any machining technique is significantly key for fitting, organizing and control of machining process and for the upgrade of the slicing conditions to limit generation costs and times. Cutting power examination accept a basic part in investigation of the diverse characteristics of a machining procedure, viz. the dynamic strength, arranging accuracy of the instrument with respect to the work piece, brutality of the machined surface and structure missteps of the machined segment, et cetera. In most-end-preparing tasks, the cutting gadget estimation contrasts from and uneasiness assortment on the humble shaft of the cutting device is considerably higherthanthaton a normal scale instrument, whichunquestionablycurtailsthe instrument'slife (Li et al. [2007]). The apparatusescan even break if the cutting conditions are not picked in likemanner. Hence, a correct estimation of the cutting forces of - end- processing accept a basic part in controlling theassuranceof cutting conditions with a particular ultimate objective to fiscally secure high machining quality and certification as long an instrument life as could be normal the situation being what it is. At level, we can't acknowledge that edge sweep impactsly affects cutting forces. Weule et al [2001] found that the roundnessof a front line is more basic atscale machining. As the traverse of an instrument diminishes, the sharpness of the device can't be updated respectably because of stipulations in the mechanical get together creation methodologiesand lessening in the basicideaofthe instrument. Thusly, the feed per tooth in - preparing might be for all goalsand reason unclear to or even shy of what the forefront traverse due to the obliged reach of approach parameters for a stable machining scale with the technique. Yuan et al. [1996] chipped away at ultraprecision machining to decide least chip thickness. Kim et al [2004] probably affirmed that when the feed per tooth is essentially indistinguishable with the edge span of the mechanical assembly, as is every now and again the case in - processing approaches, the chip forming philosophy gets intermittent and the acknowledged appreciation that a chip is confined with every tooth pass is not any more genuine. As demonstrated by their model, the base chip thickness of variousunions of gadgets and work piece materialsmightbe assessed centered around easily achievable cutting power data. 1.2 Analysis of Milling Cutter The milling cutter is a symmetrical body subsequently the examination is done thinking about a solitary tooth of the cutter. Here, the examination is done for the situation of 5 diverse axle speeds going from 50 to 2000 rpm.The loads at these rates are computed and the comparing Stresses following up on the tooth are found. Stress and distortion of the cutter at speed 50 rpm to 200rpm are obtained. Indrajeet Rajpoot1, Mrs Shabana Naz Siddique2
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072 Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1509 FEA comprises of utilizing a PC model of a material or design that is pushed and examined for particularoutcomes. It is utilized as a part of the advancement of new item configuration to check potential imperfections and in existing item refinement. The framework can put various heaps of a model to mimic genuine circumstances that the item could be understanding. Architects all through the business enhance item outlines with FEA programming from ANSYS. Unequivocal Dynamics with ANSYS expected for vast disfigurement recreations where inactivity powers are predominant Used to reenact Machining, quick framing, affect and so on 1.3 Model Validation An experimental result is taken from the literature for the simulation validation. A large number of theoretical and experimental studies on surface profile and roughness of machined products have been reported. These studies show that cutting conditions, tool wear, the material properties of tool and workpiece, as well as cutting/process parameters significantly influence the surface finish of machined parts. Therefore, it is of particular importance that the numerical analysis is an attractive alternative for evaluating residual stresses allowing substitute the application of high-cost experimental methods. On the other hand, some of the computationalresults do not correlate withtheexperimental findings. In summary, despite the fact that there existsalarge variety of different analytical, numerical and experimental techniques, currently, there is no proven analytical model enabling to reliably predict the residual stresses that arise in the course of cutting operations. For guaranteeing dependability ofthe createdFEmodelit must be checked againsttrialdatawhichincorporatessizesof the deliberate cutting force. Cutting force is a parameter which is also evaluated for the structural design of machine tools, selectionof optimum cutting parameters, the design of workpiece-holding fixtures, tool stress analysis, spindle bearingdesign, andthereal-timemonitoringoftoolwearand breakage. This study proposes an FE model for a case of the milling process. The milling operation is performed by using end–milling tool – a cutting tool of complex geometry that is used for machiningofsurfaces.Therefore,an FE model was constructed for performing mesoscopic analysis of the milling process in terms of the removed material cut cross-section. Cutting forces were evaluated during experimental testing, while the effect of the cutting force on a single cuttinginsert wasdetermined by meansofa transformation matrix. Furthermore, it was confirmed with respect to material deformation that it is necessary to apply several criteria for verification of the FE model. Therefore, numerical analysis was carried out by using dynamic material characteristics taken from the available literature sources, meanwhile, dynamicmaterial deformation constantswereacquiredfrom the performed turning experiments. Table -1: Validation between Experimental and FEA N o. V (m/mi n) 𝑓𝑧(mm/ z) π‘Žπ‘(m m) π‘Žπ‘’(m m) Experimental FEA 𝜎π‘₯(MP a) πœŽπ‘¦(M Pa 𝜎π‘₯(MP a) πœŽπ‘¦(M Pa 1. 314 0.06 3 6 64.83 55.37 71.80 53.36 2. 502 0.06 4 10 63.56 45.49 65.68 46.10 3. 628 0.06 5 12 59.18 44.83 63.38 43.22 4. 942 0.06 6 8 57.57 30.85 53.26 35.07 Cutting speed of in m/min, feed rate of mm/z, and depth of cut and width of cut were in mm. 1.4 Meshing Meshing can be done by using tetrahedral or hexahedral elements. More the no. of nodes in the element type, the greater is the accuracy of the results obtained. Tetrahedral meshing is a powerful cross-section routine and is a less demanding method for the lattice. Be that as it may, direct tetrahedral componentsperform inadequatelyinissueswith versatility, almost incompressible materials, and intense bowing. Hexahedral components, then again, give more precise outcomes than tetrahedral components, in the event of complex structures. They additionally think about lesser measure of approximations. Be that as it may, hexahedral components confront troubles at corners of parts/components. Additionally, programmed work age is regularly not plausible for building numerous three dimensional hexahedral meshes. Meshing and analysisof the milling operation havebeen carried out using ANSYS 18.2 software. The mesh generated for the end mill cutters in this work is a tetrahedral mesh.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072 Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1510 Figure -1: Meshing of milling cutters Figure-2: Meshing of Workpiece 2. ANALYSIS AND RESULTS So as to watch pressure arrangement and chip stream component in a virtual situation, an unequivocal investigation must be done on the apparatus and workpiece collaboration. In this paper, we have accomplished a similar utilizing ANSYS programming. Two distinctive two woodwind end plants have been utilized fordynamiclimited component investigation. Lager has been utilized for doing the examination. Reference outline for the apparatusisbeen Langrangian and that for the workpiece is been Eulerian. Fig -3: Stresses on Shell End Mill Cutter at (00, 100& 200)
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072 Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1511 Table 2: - Stresses on Shell End Mill Cutter Keeping in mind the end goal to get required cooperation between the two bodies, the required body communication limitations among them must be characterized appropriately. Since the covetedoutcomeisthereproduction of machining task, the contact between the instrument and the work piece must be frictional in nature. At the point when the device keeps running over the work piece, the erosion produces warm vitality. The chip conveys the warmth from the work piece and discharges it in nature.Soa frictional contact is characterized between the apparatus and the work piece. The static coefficient of grating iskeptto be 0.39 and the dynamic coefficient of contact is kept to be 0.32 (Raczy et al.). The work piece is settled from three countenances. The two side countenances are given zero level ofopportunityasthey are compelled utilizing mechanical installations while machining. The lower surface is given zero level of opportunity as they are held utilizing vacuum installations. The device is furnished with a precise speed of 20,000 rpm (Campos et al. [2013]). In the information factors, instrument is furnished with a direct speed, which speaksto the feed rate of our machining activity. The feed rate in our setup is settled to be 500 mm/sec (Campos et al. [2013]). The end time determines the no. of emphasess to be performed by the solver and educates the solver when to stop the procedure. Since the work piece is 20 mm long, and the feed rate is 500 mm/sec, an end time of 0.05 seconds was picked with the goal that the whole instrument length can be canvassed in the reproduction. The aggregate time taken keeping in mind the end goal to understand is 120 hours. No. V (m/min) 𝑓𝑧(mm/z) π‘Žπ‘(mm) π‘Žπ‘’(mm) Rack Angle 0 degree 10 degree 20 degree 𝜎π‘₯(MPa) 𝜎y(MPa) 𝜎π‘₯(MPa) πœŽπ‘¦(MPa) 𝜎x(MPa) πœŽπ‘¦(MPa) 1. 314 0.06 18 5 171.65 124.78 154.92 90.54 85.65 55.65 2. 502 0.06 20 6 249.65 159.65 179.46 126.10 113.87 63.87 3. 628 0.06 22 8 256.19 176.19 214.56 132.12 150.17 70.17 4. 942 0.06 24 10 267.31 207.31 228.31 142.51 148.51 82.51
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072 Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1512 Figure-4: Stresses on Flat End Mill Cutter at (60, 80& 100) in the case of two flute micro end mills Table 3: - Stresses on Flat End Mill Cutter of two flute micro end mills No. V (m/min) 𝑓𝑧(mm/z) π‘Žπ‘(mm) π‘Žπ‘’(mm) Rack Angle 6 degree 8 degree 10 degree 𝜎π‘₯(MPa) 𝜎y(MPa) 𝜎π‘₯(MPa) πœŽπ‘¦(MPa) 𝜎x(MPa) πœŽπ‘¦(MPa) 1. 314 0.06 18 5 110.33 81.25 95.17 68.23 93.07 66.12 2. 502 0.06 20 6 99.49 71.03 82.50 56.72 80.08 54.30 3. 628 0.06 22 8 98.84 69.10 79.53 53.50 76.56 50.54 4. 942 0.06 24 10 92.72 63.15 71.08 46.29 67.64 42.84
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 06 | June -2018 www.irjet.net p-ISSN: 2395-0072 Β© 2018, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1513 Figure-5: Stresses on Flat End Mill Cutter at (60, 80& 100) in the case of two flute micro end mills Table-4: Stresses on Flat End Mill Cutter of two flute micro end mills Figure-6: Stresses on Shell End Mill Cutter at (60, 80& 100) in the case of four flute micro end mills. 3. CONCLUSIONS- Stress formation is a major hindrance to good surface finish in case of both macro and milling. However, stressformation in case of milling is of greater importance than in case of conventional milling as stress formed in the former case are of sub-meter size and distressing processes are expensive, and sometimes impossible. Hence, stress minimizationisthe only way of obtaining good surface finish in structures. To minimize formation of stressin case of milling, either the cutting conditions or the tool geometry can be optimized. In this work, tool geometry improvement has been tried to be accomplished by performing FE analysis on tools with different setsof rake and relief angles, for both two fluteand four flute end mills and for Shell end mills. The results of the finite analysis of the shell and flat end milling tools offer the conclusion that in the given cutting conditions, the least amount of Von Mises stress generated in case of a shell end mill at 10o and 20o, two flute flat end mill cutter is for a cutter having rake angle 8ΒΊ and relief angles of 6ΒΊ and thatin the case of four flute end mill cutter is for a cutter having rake angle 6ΒΊ and relief angle 8ΒΊ. FE dynamic analysis of the tool-chip interaction in the milling process as performed and stress formation process was simulated using ANSYS software. It shows that as the rack angle increases stresses decrease. 4. REFERENCES [1] Afazov, S.M., Ratchev, S.M. and Segal, J., Modelling and simulation of -milling cutting forces, Journal of Materials Processing Technology, Vol.210, pp. 2154- 2162 (2010). [2] Alrabii SA, An experimental study of stress formation in drilling and slot-end milling operations, Journal of Engineering, 15(4) (2009) 4219- 4240. [3] Ávila M, Gardner J, Reich-Weiser C, Tripathi S, Vijayaraghavan A, Dornfeld D. Strategies for Stress Minimization and Cleanability in Aerospace and Automotive Manufacturing. SAE Transactions Journal of Aerospace, 114 (1), pp. 1073-1082 (2006). [4] Bao WY, Tansel IN, Modeling -end-milling operations. Part I: analytical cutting force model, International Journal of Machine Tools & Manufacture, 40 (2000) 2155-2173. No. V (m/min) 𝑓𝑧(mm/z) π‘Žπ‘(mm) π‘Žπ‘’(mm) Rack Angle 6 degree 8 degree 10 degree 𝜎π‘₯(MPa) 𝜎y(MPa) 𝜎π‘₯(MPa) πœŽπ‘¦(MPa) 𝜎x(MPa) πœŽπ‘¦(MPa) 1. 314 0.06 18 5 110.33 81.25 95.17 68.23 93.07 66.12 2. 502 0.06 20 6 99.49 71.03 82.50 56.72 80.08 54.30 3. 628 0.06 22 8 98.84 69.10 79.53 53.50 76.56 50.54 4. 942 0.06 24 10 92.72 63.15 71.08 46.29 67.64 42.84