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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 181
EXPERIMENTAL AND SIMULATION STUDIES ON CGP PROCESSED
CuZn37 BRASS ALLOY USING SEMI-CIRCULAR GROOVE CORRUGATED
DIES
Rahul S1, Dr. Shantharaja M2, Deepak Singh G3, Tajuddin Yazdani4
1,3P.G. Scholar, Department of Mechanical Engineering, University Visvesvaraya College of Engineering, Bengaluru
– 560001, Karnataka, India
2Associate Professor, Department of Mechanical Engineering, University Visvesvaraya College of Engineering,
Bengaluru – 560001, Karnataka, India
4Professor, Department of Mechanical Engineering, HKBK college of Engineering, Bengaluru – 560045,
Karnataka, India
------------------------------------------------------------------------***-------------------------------------------------------------------------
Abstract – Constrained Groove Pressing (CGP) is an
intense plastic straining technique for the fabrication of
plate and sheet samples with ultrafine grained structures
without changing their initial dimensions. In this research,
experimental and simulation analysis was done to
investigate the plastic deformation behavior of CuZn37
brass alloy sheet using Semi-circular groove corrugated
dies. The effective strain has been increased from 0.6442
to 2.9431 at the end of 5th pass in the simulation software
(AFDEX). The BHN has been increased from 95.4 to 202.01
until 4th pass and decreased to 194.30 in the 5th pass
experimentally and from 91.25 to 200 until 4th pass and
decreased to 195.52 in the 5th pass in the simulation.
Key Words: Severe Plastic Deformation, CGP, Grain
refinement, Brinell hardness
1. INTRODUCTION
Severe plastic deformation (SPD) is one of the
top-down approaches to fabricate UFG and NS materials
based on applying the repetitive shear strains to the
metallic materials with literally no change in their
exterior dimensions. Up to now, the SPD concept has
been employed to achieve UFG/NS materials in the
laboratory scale. However, in some cases, the SPD is
adopted toward industrial scales production. Among the
various SPD techniques proposed most of the methods
are intended for processing bulk materials; very few
methods like Accumulative Roll Bonding[1,2],
Constrained Groove Pressing (CGP) [3,4], and Repetitive
Corrugation and Straightening (RCS) [5,6] are capable of
processing sheet materials. CGP process was invented
recently and it is promising method for producing fine
grain sheet material for structural applications. In the
CGP process, a work-piece is repetitively bent and
straightened without significantly changing the cross-
section geometry of the work-piece, during which large
plastic strains are imparted into the materials, which
leads to the refinement of microstructure. In this present
study mechanical behavior (Brinell hardness, effective
strain and microstructure) were predicted through
experimental and simulation analysis.
Adviser for metal Forming Process Design
Expert (AFDEX) is a general-purpose metal forming
simulator, which meets the following requirements for
intelligent Bulk-Metal- Forming Simulation (BMFS).
Currently, AFDEX is theoretically based on the rigid or
elasto-thermoviscoplastic finite element method. AFDEX
2D and AFDEX 2D/DIE use quadrilateral finite elements.
AFDEX 3D, AFDEX 3D/OPEN, and AFDEX 3D/DIE employ
tetrahedral elements. AFDEX 2D/DIE and AFDEX 3D/DIE
are integrated die structural analysis programs that
accompany the respective BMF simulators, AFDEX 2D
and AFDEX 3D. AFDEX MAT provides users with highly
accurate true stress-strain curves for the materials in use
at room or elevated temperature [7].
2. PREPARATION OF DIES AND SPECIMEN
2.1 SPECIMEN USED
In the present study, material selected for the
investigation is CuZn37 Brass alloy Sheet. The chemical
composition of the test material is mentioned in the
Table 1.
Contents Cu Ni Pb Fe Sn Al Zn
Percentage
62 -
65.5
≤
0.30
≤
0.1
≤
0.1
≤
0.1
≤
0.05
Balance
The material to be forged is CuZn37 Brass alloy
having maximum yield strength 183 MPa, thickness of
the test specimens to be forged is 1mm and cross
sectional area of the test specimens to be forged is
70x70mm².
2.2 SPECIFICATIONS OF DIES
In order to achieve the CGP on Brass test
specimen, semi-circular groove corrugated and flat dies
Table 1: Chemical composition of CuZn37 Brass Alloy
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 182
are used in the present research work. SOLIDWORKS
was used for modelling of the dies according to design
specifications. Technical specifications of the die are
cross sectional area of semi-circular groove corrugated
die is 120x120 mm², Radius of the corrugated groves is 5
mm, depth of the groove is 4 mm, Cross sectional area of
upper flat die is 110x110 mm² and lower flat die is
130x130 mm², die material used is mild steel, overall
tolerance of the geometry is ±1mm.
3. EXPERIMENTAL PROCEDURE
The basic parameters considered for the SPD
are strain rate for compression of test specimen,
thickness of the test specimen and number of passes.
The specimens were processed at room temperature
from one to five passes. The Fig 1 (a,b) shows the
assembly of corrugated and flat dies. The CGP process
consists of four presses and the process was carried out
using UTM (Universal Testing Machine) which has a
capacity of 40 Tonnes with a pressing speed of
0.5mm/min.
During the first press, the flat sheet of CuZn37
Brass alloy became corrugated using corrugated dies.
For second press, flat die was used to flatten the
corrugated sheet. For third press the flattened sheet is
rotated by 90° and corrugated by corrugated dies. For
fourth press, again the flattened die was used to flatten
the corrugated sheet. Thus, four presses are considered
as one pass of the sheet. By repeating the corrugation
and straightening process, a large amount of plastic
strain can be accumulated in the work piece. Similarly,
the process was repeated up to five passes and further
processing was not done due to decrease in Brinell
hardness. Higher strain was achieved at the end of five
passes.
Three-dimensional, plane-strain, Rigid–plastic
FEM simulations of the CGP processing have been
carried out using the commercial finite element
software, AFDEX. In the simulation, the dies can be
assumed as rigid bodies, since their strength is much
higher than the workpiece material. Manual meshing
was used to accommodate deformation during the
simulations. The Workpiece is meshed with Tetrahedral
element during simulation. After meshing the model
consists of 10898 nodes and 46240 elements. A self
adaptive step length was used for the process to carry on
the simulations. The friction between the workpiece and
the die used was sticking, which was present in the
library of the software.
3.1 Microstructure analysis
An analysis of the fine structures of the before
and after CGP pressed Brass alloys are prepared as per
the requirements. Microstructure study was carried out
using Inverted Optical Microscope with a magnification
of 800X. The test specimens were cut into to a size of
10mm x 10mm. The specimens were mounted using
Bakelite powder. Prior to microstructure analysis, the
surface preparation was made using polishing machine
with different grades of Silicon Carbide papers and the
etchant was used to exhibit the microstructure of the
polished specimens. The chemical composition of the
Etchant used is 4g- +10ml-HCL+40ml-0.
3.2 Brinell Hardness
The Brinell Hardness (BHN) of the test
specimens were calculated according to ASTM E-10
using ball indenter of diameter 2.5mm, with a load of
187.5 kgf and a loading period of 30 seconds. For
obtaining reliable results, the measurements of the
hardness was performed on all the specimens in 20
different locations and average of eight nearer values
was considered as final hardness value.
4. RESULTS AND DISCUSSION
The experimental corrugation and flattening
CGP process are shown in the Fig 2 (a, b).
Fig 1 (a): Assembly of upper and lower
semi-circular groove corrugated dies
Fig 1 (b): Assembly of upper and
lower flat dies
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 183
The images of the specimen obtained during
experimental process at the end of each pass are shown
in the Fig 3. The images of the specimen with different
presses obtained in the simulation software (AFDEX) are
shown in the Fig 4.
The CGP process of corrugating and
straightening was continued up to 20 presses in the
simulation software.
Fig 2 (a): Corrugation CGP process using
semi-circular groove corrugated dies
Fig 2 (b): Flattening CGP process
using flat dies
1st pass 2nd Pass
3rd Pass 4th Pass
5th Pass
Fig 3: Images of the specimen with different passes
Press 4
Press 3
Press 2
Press 1
Fig 4: Images obtained in simulation with different
presses passes
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 184
4.1 Microstructural analysis of specimens
subjected to CGP
(a) Parent material
b) After 2 passes
(c) After 4 passes
Fig 5: Optical images of CuZn37 Brass alloy for different
passes
The Fig 5 shows grain boundaries of Cuzn37
brass alloy without CGP process. After 2 passes of CGP,
CuZn37 brass alloy resulted in the formation of non
uniform sub grains that vary substantially which
indicates the presence of dislocation cell structure as
observed in Fig 5 (b). From Fig 5 (c), it is evident that the
brass alloy in this region has undergone quite large
amount of plastic deformation. From the Fig 5 (a-c), the
detailed observation reveals the dislocation behaviour
relating to the low angle sub grain boundaries formation,
led to the development of a deformed substructure, thus
converting coarse grain structure in to fine grain
structure.
4.2 Effective strain distribution of different
passes of CGP process
Fig 6: Effective strain distribution of different passes of
CGP process
From the Fig 6, it can be seen that, in each pass
the effective strain is not much varied throughout the
material, which shows that the material is homogenous.
4.3 Average Effective strain distribution of
different passes of CGP process
From the Fig 7, it can be seen that the effective
strain induced in the material is gradually increased
after every pass, due to refinement of the grains after
each pass and also due to stress concentration effects at
Fig 7: Average Effective strain distribution of
different passes of CGP process
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 185
the inclined regions. The total effective strain induced
after five cycles of CGP process is 2.94.
4.4 Comparison of average Brinell hardness in
different passes
90
110
130
150
170
190
210
230
0 1 2 3 4 5
BHN
Number of Passes
Theoretical
Hardness
Simulation
Hardness
From the Fig 8, it can be seen that the Brinell
hardness values in both i.e., simulation and theoretical
result values has been increased up to the 4th pass
which is actually due to the strain hardening effect and it
has decreased in the 5th pass due to the grain
refinement effect and it has reached its ultimate stress
point.
5. CONCLUSIONS
 The semi-circular groove corrugated dies and
flat dies were used for the CGP process in which
two corrugation and two straightening process
was done and considered as one pass. The brass
alloy (CuZn37) was pressed up to five passes.
Simulation was also done for the same number
of passes using AFDEX software.
 The CGP process produces high quality
nanostructured materials, where, the quality of
surface roughness improves with the increasing
number of passes. Also, this process is
concerned with producing metals and alloys
capable of controlling nanosized grains, and free
from defects such as porosity, cracks, or other
atomic scale defects that are known to
compromise properties.
 Hardness (BHN) increased in the first four
passes in both theoretical (95.4 to 202.01) and
simulation (91.25 to 200) and then trend has
been decreased slightly at the fifth pass in both
theoretical (194.30) and simulation (195.52).
Greater refinement of brass alloy microstructure
and further increase in strength is expected to
occur with large number of executed passes.
 The effective strain has been increased in
CuZn37 brass alloy sheet after every CGP
process from 0.66442 to 2.9431 after 5 passes,
during the simulation in AFDEX software. This is
because of large plastic deformation in the
original grain structure of metals, develops a
microstructure on a much smaller scale.
Extended dense dislocation walls separating
regions of relatively low dislocation densities,
between these regions lattice misorientations
develop with increasing strain.
 Microstructure analysis of CuZn37 brass alloy
resulted in the formation of non uniform sub
grains that vary substantially which indicates
the presence of dislocation cell structure. With
increased number of passes, it led to the
development of a deformed substructure, thus
converting coarse grain structure in to fine grain
structure.
ACKNOWLEDGEMENT
I would like to thank Siddesha H S, Associate Professor,
Department of Mechanical Engineering, ACS college of
Engineering, Bengaluru, for their guidance and support
towards the completion of this work and Dr. Ramesh C,
Associate Professor, Department of Mechanical
Engineering, RajaRajeshwari college of Engineering,
Bengaluru, for providing access to Universal Testing
Machine and for their support.
REFERENCES
[1] V.M. Segal (1995) , “Materials processing by
simple shear”, Mater. Sci. Eng. A197 157–164.
[2] N. Tsuji, K. Shiotsuki, H. Utsunomiya and Y. Saito,
in Proceedings of the international symposium
on “Towards innovation in Superplasticity”,
Transtech publications.
[3] Krishnaiah A, Chakkingal U, Venugopal P(2005),
Production of ultrafine grain sizes in aluminium
sheets by severe plastic deformation using the
technique of groove pressing. Scripta Mater;
52:122933.
[4] Z. Horita, M. Furukawa, K. Oh-Ishi, M. Nemoto,
T.G. Langdon, in: T. Saki, H.G. Suzuki (Eds.)
(1999), “Proceeding of the fourth International
Conference on Recystallization and Related
Phenomena”, Japan Institute of Metals, Japan, p.
301.
[5] J. Gill Sevillano, P. van Houtte, E. Aernoudt, Prog.
Mater. Sci. 25 (1980) 69.
Fig 8: Average Brinell hardness of different passes of
CGP processes
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 186
[6] S. V. Dobatkin, “Severe Plastic Deformation of
Steels: Structure, Properties and Techniques” in
Investigation and Applications of Severe Plastic
Deformation,Ed. by T. C. Lowe and R. Valiev
(Kluwer, Netherlands), 3 (2000) 13-22.
[7] http://www.afdex.com/content/introduction.

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  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 181 EXPERIMENTAL AND SIMULATION STUDIES ON CGP PROCESSED CuZn37 BRASS ALLOY USING SEMI-CIRCULAR GROOVE CORRUGATED DIES Rahul S1, Dr. Shantharaja M2, Deepak Singh G3, Tajuddin Yazdani4 1,3P.G. Scholar, Department of Mechanical Engineering, University Visvesvaraya College of Engineering, Bengaluru – 560001, Karnataka, India 2Associate Professor, Department of Mechanical Engineering, University Visvesvaraya College of Engineering, Bengaluru – 560001, Karnataka, India 4Professor, Department of Mechanical Engineering, HKBK college of Engineering, Bengaluru – 560045, Karnataka, India ------------------------------------------------------------------------***------------------------------------------------------------------------- Abstract – Constrained Groove Pressing (CGP) is an intense plastic straining technique for the fabrication of plate and sheet samples with ultrafine grained structures without changing their initial dimensions. In this research, experimental and simulation analysis was done to investigate the plastic deformation behavior of CuZn37 brass alloy sheet using Semi-circular groove corrugated dies. The effective strain has been increased from 0.6442 to 2.9431 at the end of 5th pass in the simulation software (AFDEX). The BHN has been increased from 95.4 to 202.01 until 4th pass and decreased to 194.30 in the 5th pass experimentally and from 91.25 to 200 until 4th pass and decreased to 195.52 in the 5th pass in the simulation. Key Words: Severe Plastic Deformation, CGP, Grain refinement, Brinell hardness 1. INTRODUCTION Severe plastic deformation (SPD) is one of the top-down approaches to fabricate UFG and NS materials based on applying the repetitive shear strains to the metallic materials with literally no change in their exterior dimensions. Up to now, the SPD concept has been employed to achieve UFG/NS materials in the laboratory scale. However, in some cases, the SPD is adopted toward industrial scales production. Among the various SPD techniques proposed most of the methods are intended for processing bulk materials; very few methods like Accumulative Roll Bonding[1,2], Constrained Groove Pressing (CGP) [3,4], and Repetitive Corrugation and Straightening (RCS) [5,6] are capable of processing sheet materials. CGP process was invented recently and it is promising method for producing fine grain sheet material for structural applications. In the CGP process, a work-piece is repetitively bent and straightened without significantly changing the cross- section geometry of the work-piece, during which large plastic strains are imparted into the materials, which leads to the refinement of microstructure. In this present study mechanical behavior (Brinell hardness, effective strain and microstructure) were predicted through experimental and simulation analysis. Adviser for metal Forming Process Design Expert (AFDEX) is a general-purpose metal forming simulator, which meets the following requirements for intelligent Bulk-Metal- Forming Simulation (BMFS). Currently, AFDEX is theoretically based on the rigid or elasto-thermoviscoplastic finite element method. AFDEX 2D and AFDEX 2D/DIE use quadrilateral finite elements. AFDEX 3D, AFDEX 3D/OPEN, and AFDEX 3D/DIE employ tetrahedral elements. AFDEX 2D/DIE and AFDEX 3D/DIE are integrated die structural analysis programs that accompany the respective BMF simulators, AFDEX 2D and AFDEX 3D. AFDEX MAT provides users with highly accurate true stress-strain curves for the materials in use at room or elevated temperature [7]. 2. PREPARATION OF DIES AND SPECIMEN 2.1 SPECIMEN USED In the present study, material selected for the investigation is CuZn37 Brass alloy Sheet. The chemical composition of the test material is mentioned in the Table 1. Contents Cu Ni Pb Fe Sn Al Zn Percentage 62 - 65.5 ≤ 0.30 ≤ 0.1 ≤ 0.1 ≤ 0.1 ≤ 0.05 Balance The material to be forged is CuZn37 Brass alloy having maximum yield strength 183 MPa, thickness of the test specimens to be forged is 1mm and cross sectional area of the test specimens to be forged is 70x70mm². 2.2 SPECIFICATIONS OF DIES In order to achieve the CGP on Brass test specimen, semi-circular groove corrugated and flat dies Table 1: Chemical composition of CuZn37 Brass Alloy
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 182 are used in the present research work. SOLIDWORKS was used for modelling of the dies according to design specifications. Technical specifications of the die are cross sectional area of semi-circular groove corrugated die is 120x120 mm², Radius of the corrugated groves is 5 mm, depth of the groove is 4 mm, Cross sectional area of upper flat die is 110x110 mm² and lower flat die is 130x130 mm², die material used is mild steel, overall tolerance of the geometry is ±1mm. 3. EXPERIMENTAL PROCEDURE The basic parameters considered for the SPD are strain rate for compression of test specimen, thickness of the test specimen and number of passes. The specimens were processed at room temperature from one to five passes. The Fig 1 (a,b) shows the assembly of corrugated and flat dies. The CGP process consists of four presses and the process was carried out using UTM (Universal Testing Machine) which has a capacity of 40 Tonnes with a pressing speed of 0.5mm/min. During the first press, the flat sheet of CuZn37 Brass alloy became corrugated using corrugated dies. For second press, flat die was used to flatten the corrugated sheet. For third press the flattened sheet is rotated by 90° and corrugated by corrugated dies. For fourth press, again the flattened die was used to flatten the corrugated sheet. Thus, four presses are considered as one pass of the sheet. By repeating the corrugation and straightening process, a large amount of plastic strain can be accumulated in the work piece. Similarly, the process was repeated up to five passes and further processing was not done due to decrease in Brinell hardness. Higher strain was achieved at the end of five passes. Three-dimensional, plane-strain, Rigid–plastic FEM simulations of the CGP processing have been carried out using the commercial finite element software, AFDEX. In the simulation, the dies can be assumed as rigid bodies, since their strength is much higher than the workpiece material. Manual meshing was used to accommodate deformation during the simulations. The Workpiece is meshed with Tetrahedral element during simulation. After meshing the model consists of 10898 nodes and 46240 elements. A self adaptive step length was used for the process to carry on the simulations. The friction between the workpiece and the die used was sticking, which was present in the library of the software. 3.1 Microstructure analysis An analysis of the fine structures of the before and after CGP pressed Brass alloys are prepared as per the requirements. Microstructure study was carried out using Inverted Optical Microscope with a magnification of 800X. The test specimens were cut into to a size of 10mm x 10mm. The specimens were mounted using Bakelite powder. Prior to microstructure analysis, the surface preparation was made using polishing machine with different grades of Silicon Carbide papers and the etchant was used to exhibit the microstructure of the polished specimens. The chemical composition of the Etchant used is 4g- +10ml-HCL+40ml-0. 3.2 Brinell Hardness The Brinell Hardness (BHN) of the test specimens were calculated according to ASTM E-10 using ball indenter of diameter 2.5mm, with a load of 187.5 kgf and a loading period of 30 seconds. For obtaining reliable results, the measurements of the hardness was performed on all the specimens in 20 different locations and average of eight nearer values was considered as final hardness value. 4. RESULTS AND DISCUSSION The experimental corrugation and flattening CGP process are shown in the Fig 2 (a, b). Fig 1 (a): Assembly of upper and lower semi-circular groove corrugated dies Fig 1 (b): Assembly of upper and lower flat dies
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 183 The images of the specimen obtained during experimental process at the end of each pass are shown in the Fig 3. The images of the specimen with different presses obtained in the simulation software (AFDEX) are shown in the Fig 4. The CGP process of corrugating and straightening was continued up to 20 presses in the simulation software. Fig 2 (a): Corrugation CGP process using semi-circular groove corrugated dies Fig 2 (b): Flattening CGP process using flat dies 1st pass 2nd Pass 3rd Pass 4th Pass 5th Pass Fig 3: Images of the specimen with different passes Press 4 Press 3 Press 2 Press 1 Fig 4: Images obtained in simulation with different presses passes
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 184 4.1 Microstructural analysis of specimens subjected to CGP (a) Parent material b) After 2 passes (c) After 4 passes Fig 5: Optical images of CuZn37 Brass alloy for different passes The Fig 5 shows grain boundaries of Cuzn37 brass alloy without CGP process. After 2 passes of CGP, CuZn37 brass alloy resulted in the formation of non uniform sub grains that vary substantially which indicates the presence of dislocation cell structure as observed in Fig 5 (b). From Fig 5 (c), it is evident that the brass alloy in this region has undergone quite large amount of plastic deformation. From the Fig 5 (a-c), the detailed observation reveals the dislocation behaviour relating to the low angle sub grain boundaries formation, led to the development of a deformed substructure, thus converting coarse grain structure in to fine grain structure. 4.2 Effective strain distribution of different passes of CGP process Fig 6: Effective strain distribution of different passes of CGP process From the Fig 6, it can be seen that, in each pass the effective strain is not much varied throughout the material, which shows that the material is homogenous. 4.3 Average Effective strain distribution of different passes of CGP process From the Fig 7, it can be seen that the effective strain induced in the material is gradually increased after every pass, due to refinement of the grains after each pass and also due to stress concentration effects at Fig 7: Average Effective strain distribution of different passes of CGP process
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 185 the inclined regions. The total effective strain induced after five cycles of CGP process is 2.94. 4.4 Comparison of average Brinell hardness in different passes 90 110 130 150 170 190 210 230 0 1 2 3 4 5 BHN Number of Passes Theoretical Hardness Simulation Hardness From the Fig 8, it can be seen that the Brinell hardness values in both i.e., simulation and theoretical result values has been increased up to the 4th pass which is actually due to the strain hardening effect and it has decreased in the 5th pass due to the grain refinement effect and it has reached its ultimate stress point. 5. CONCLUSIONS  The semi-circular groove corrugated dies and flat dies were used for the CGP process in which two corrugation and two straightening process was done and considered as one pass. The brass alloy (CuZn37) was pressed up to five passes. Simulation was also done for the same number of passes using AFDEX software.  The CGP process produces high quality nanostructured materials, where, the quality of surface roughness improves with the increasing number of passes. Also, this process is concerned with producing metals and alloys capable of controlling nanosized grains, and free from defects such as porosity, cracks, or other atomic scale defects that are known to compromise properties.  Hardness (BHN) increased in the first four passes in both theoretical (95.4 to 202.01) and simulation (91.25 to 200) and then trend has been decreased slightly at the fifth pass in both theoretical (194.30) and simulation (195.52). Greater refinement of brass alloy microstructure and further increase in strength is expected to occur with large number of executed passes.  The effective strain has been increased in CuZn37 brass alloy sheet after every CGP process from 0.66442 to 2.9431 after 5 passes, during the simulation in AFDEX software. This is because of large plastic deformation in the original grain structure of metals, develops a microstructure on a much smaller scale. Extended dense dislocation walls separating regions of relatively low dislocation densities, between these regions lattice misorientations develop with increasing strain.  Microstructure analysis of CuZn37 brass alloy resulted in the formation of non uniform sub grains that vary substantially which indicates the presence of dislocation cell structure. With increased number of passes, it led to the development of a deformed substructure, thus converting coarse grain structure in to fine grain structure. ACKNOWLEDGEMENT I would like to thank Siddesha H S, Associate Professor, Department of Mechanical Engineering, ACS college of Engineering, Bengaluru, for their guidance and support towards the completion of this work and Dr. Ramesh C, Associate Professor, Department of Mechanical Engineering, RajaRajeshwari college of Engineering, Bengaluru, for providing access to Universal Testing Machine and for their support. REFERENCES [1] V.M. Segal (1995) , “Materials processing by simple shear”, Mater. Sci. Eng. A197 157–164. [2] N. Tsuji, K. Shiotsuki, H. Utsunomiya and Y. Saito, in Proceedings of the international symposium on “Towards innovation in Superplasticity”, Transtech publications. [3] Krishnaiah A, Chakkingal U, Venugopal P(2005), Production of ultrafine grain sizes in aluminium sheets by severe plastic deformation using the technique of groove pressing. Scripta Mater; 52:122933. [4] Z. Horita, M. Furukawa, K. Oh-Ishi, M. Nemoto, T.G. Langdon, in: T. Saki, H.G. Suzuki (Eds.) (1999), “Proceeding of the fourth International Conference on Recystallization and Related Phenomena”, Japan Institute of Metals, Japan, p. 301. [5] J. Gill Sevillano, P. van Houtte, E. Aernoudt, Prog. Mater. Sci. 25 (1980) 69. Fig 8: Average Brinell hardness of different passes of CGP processes
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 10 | Oct 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 186 [6] S. V. Dobatkin, “Severe Plastic Deformation of Steels: Structure, Properties and Techniques” in Investigation and Applications of Severe Plastic Deformation,Ed. by T. C. Lowe and R. Valiev (Kluwer, Netherlands), 3 (2000) 13-22. [7] http://www.afdex.com/content/introduction.