International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1429
DESIGN AND ANALYSIS OF PROGRESSIVE TOOL FOR U-BRACKET OF
POWER METER CABINET
Narayan Chouhan1, N Manjunath Gowda2, Satish Kumar S3
1M.Tech Student, Dept. of studies in mechanical Engg, UBDTCE, Davangere, Karnataka, India
2Assistant Professor, Dept. of studies in mechanical Engg, UBDTCE, Davangere, Karnataka, India
3Partner, Elite Insulators, Mallashettyhalli (Davangere dist), Karnataka, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract -In the present situation, the production of U-
brackets are made with a new raw material and in a two
different tools, each tool requires press machines which leads
to the usage of more resources and considerable financialloss
thus the industry stopped the production of U-brackets and
given out sources for the production. The present U-bracket
components can be done using scrap material which is
sufficiently available in industry and it has not all used forany
other production. Considering all these criteria, the existing
tools can be simplified with a single progressive tool so that
usage of more resources can be simplified and can be done
using scrap material and raw material cost will be saved. In
this work a three stage progressive tool hasbeen designedand
analyzed the stresses and deformation for different parts of
progressive tool like top plate, bottom plate, dieplate, stripper
plate and guide pillar. A progressive tool performs two or
more operations at different stages in a single strokeofram to
produce the part as the strip moves through the die. Modeling
is carried out in SOLID EDGE VERSION 20 and simulation is
carried out in ANSYS WORKBENCH 18.1 and result obtained
from analysis is validated with manual calculations. The
designed tool will help the industry to manufacture the part
rather than outsourcing andhencesavesmoney. 30Tavailable
mechanical press can be used with newly designed tool as the
press capacity is greater than the required.
Key Words: Progressive tool, U-Bracket, Scrap material,
Raw material, Press capacity
1. INTRODUCTION
In recent day’s different kinds of sheet metal
developing processes were using in sheet metal product
manufacturing companies. These sheet metal developing
processes have been using for manufacturing various
sections of airplanes, vehicles and ships etc. by using the
complicated devices discovered from modern innovations.
With the ever growing knowledge ofscienceandtechnology,
the progressive tool design process has become more
precise to satisfy the demand of moreproductivity,low price
and better exactness. For a better improvement, the more
delicate design development of today has not replaced the
need for basic sheet forming of dies and process. The
popularity of sheet metal stamping process is due to its high
productivity, ease in manufacturing of intricate shapes and
will be done at lower cost. The parts manufactured from the
sheet metal have well good-looking qualities, better
dimension accuracy, light weight and higher strength.
For a better improvement, the more delicate design
development of today has not replaced the need for basic
sheet forming of dies and process. The popularity of sheet
metal stamping process is due to its high productivity, ease
in manufacturing of intricate shapes and will be done at
lower cost. The parts manufactured from the sheet metal
have well good-looking qualities,betterdimensionaccuracy,
light weight and higher strength.
2. COMPONENT DATA
Component Name: U-Bracket
Material: CRCA Steel
Thickness: 0.8mm
Shear strength: 36 Kg/mm2
Tempered Grade: Cold Rolled
Fig -1: Solid model of component
U-bracket is a small component usedinthemetercabinetsto
fix the domestic power meters. The 2D drawing is received
from the industry.
3. PROBLEM STATEMENT
 Currently for window cutting operation of the top
box, the material of dimension100×90mmhasbeen
wasting as scrap material and decreasing the
productivity.
 The industry used separatetwoseparatepresstools
and machines for each sheet metal operations of U-
bracket thus stopped productionandoutsourcingit.
 New stamping tools like progressive tools which
produce well superior quality and consistent parts
with enormous amounthasnotcompletelyinstalled
where ever its requirement meet.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1430
 By analyzing the recorded problems it came to
know that the problems became an obstacle to the
production improvement.
3.1 Objectives of Work
 To know the source of causes of less productivity in
Elite Insulators and propose the possible of
improvement in present production line.
 Collecting geometrical details which describe size,
shape and additional description of the component
(U-bracket).
 Modification of tool to use the available scrap
material.
 Suggesting the new tool as progressive tool.
4. METHODOLOGY
Fig -2: Methodology Adopted
5. MODELING AND MATERIAL SELECTION
5.1 3D Model of Progressive Tool
Fig -3: Progressive Tool Assembly
Fig -4: Strip Layout
5.2 2D Drawings of Progressive tool and component
Fig -5: Section view of progressive tool
Fig -6: Component Drawing
5.3 Mechanical Properties of Tool Materials
Table -1: Mechanical properties
Property Mild steel
(st-42)
HCHC steel
(D2 steel)
EN-31
Steel
Mass Density
(Kg/m3) 7850 7700 7700
Yield strength
(Mpa) 250 1532 450
Ultimate
Tensile
Strength (mpa)
460 1320 750
Possion’s ratio 0.303 0.3 0.3
Shear
modulus(Gpa) 78 79 86
Young’s
Modulus(Mpa)
210000 210000 215000
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1431
6. DESIGN CALCULATIONS
6.1 Strip layout Development
Scrap Bridge (B) = (1 to 1.25)t
B=1mm
Margin (M) = (1.25 to 1.5).t
M=1.5mm
Area of Blank (component) = 22×87 =1914mm
No. of Rows = 1
Pitch=Advance of die = L+B, where L = Length of blank
=24mm
Economy Factor = (blank size area × No. of rows)/ (Strip
breadth × Pitch) ×100
Economy Factor = 92.46%
% of strip used = ×100
=88.61%
% of scrap = 100-88.61 = 11.31%
6.2 Die clearance and Tool Life
Die clearance = thickness of work piece× suggested %
For steel, Die clearance = (2.5 - 5%) t, where t=thickness of
sheet
Min. Die clearance = 0.02mm
Max. Die clearance = 0.04mm
Max clearance can cause burr and min clearance cause
repeated reshaping of die and tool life decreases.
For better tool life, the die clearance has an
optimum average value. Optimum valuecanbecalculatedby
averaging the min and max die clearances.
Optimum clearance = 0.02+0.04/2 = 0.03mm
6.3 Force calculations
Shearing force
Fsh = L×t×fs
Where Fsh = shear force or cutting force in tons
fs = shear strength in Kg/mm2
L = cutting length in mm
t= thickness of sheet = 0.8mm
At stage 1, pitch punch
Cutting length L1 = 54mm
At stage 2, parting with embossing
Cutting length L2 = 171mm
At stage 3, small cut-off
Cutting Lengt L3 = 20mm
Total cutting length L = L1+L2+L3 =245mm
Fsh = 7056Kgf
Fsh = 7056×0.6 (for safety purpose 60% additional force is
added)
Fsh = 4233.3Kgf
Fsh1 = 7056+4233.3 = 11529.6 Kgf
Again 20% of force is added to make the tool theoretically
strong
Fsh2 = 11529.6×0.2 = 2305.92 Kgf
Total shearing force = Fsh1+Fsh2 = 13835.52 =14000 Kgf
= 14T
Stripping Force
Stripping force = 15% of shear force
= 0.15×14 = 2.1T
Total Force (F) = stripping Force+ Shearing Force
` = 14+2.1+2.1 = 16.1T
6.4 Press Capacity
The total press capacity is 125% more than the total force
calculated therefore
Pc = total tonnage×1.25
= 20.125T
6.5 Stress and deflection calculation for different
elements of Progressive tool
a) Die Plate
Die plate is considered as a fixed beam. The shoe deflection
is computed from strength of material concept for fixed
beam. Equation for deflection is given by
δ =
Where,
F=80% of shearing force = 109834.4N
E - Young’s modulus = 2.1×105N/mm2
I- Moment of inertia of plate in mm4
L- Least distance b/w successive fasteners=45.6mm
Width, B = 167mm and thickness, H = 38mm
F = 109834.4 N
I =
I = 763635.33 mm4
δ= 0.0003382mm
Stress generated in the die plate is given by, σ =
Where A = B×H = 167×38 = 6346mm2
σ =17.304 N/mm2
b) Bottom Plate
Bottom plate is supported by number of parallel blocks
hence we consider it as a simply supported beam. Using
strength of materials, the deflection for simply supported
beam with concentrated load, deflection equation is given
below
δ = , F = 80% shearing force =109834.4N
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1432
B = 287mm and H = 30mm
L = 62mm
I = 645750 mm4
δ = 0.0040215mm
σ = = 6.172 N/mm2
C) Top Plate
For analysis top plate is considered as a simply supported
beam with concentrated load acting on it. The equation is
given by
δ = , where F=80%shearing force = 109834.4N
B = 287mm and H = 35mm
L = 60mm
I = = 1025427.083mm4
δ =0.0022952mm
σ = = 10.93N/mm2
D) Stripper Plate
Assuming stripper plate to be a fixed beam, the deflection
and stress calculation is done by adopting SOM concept as
F = 20% shearing force = 27458.6 N
B = 167mm and H = 24mm
L = 60mm
F = 20% shearing force = 27458.6 N
I = = 192384mm4
δ = = 0.0007468mm
σ = = 6.850N/mm2
E) Guide Pillar
Considering guide pillar as a cantilever beam with
load acting vertically on it and guide pillar is considered as
one side fixed and another side for freecolumnconstruction.
From strength of material, for column construction of one
side is fixed and another side is free type.
Load acting on guide pillar = 80% shearing force =
109834.4N
Load per pillar P = = 54917N
Crippling load Pc =
Where, E = 2.15×105 N/mm2
Diameter of pillar = d = 28mm
Pillar length = l = 150mm
I = = 30175.768 mm4
Pc = 482708.54 N < 54917N
Since applied load is less than the crippling load therefore
applied load is harmless for design.
A = = 615.83mm2
δ = = = 0.0636969 mm
σ = = 89.9N/mm2
7. FINITE ELEMENT ANALYSIS
Finite element analysis was carried out in Ansys
workbench 18.1. For analysis of tool,thefivemajor elements
of tool were chosen based on the maximum loading
conditions. This helps to predict real condition of tool
components in the operation. This helps to eliminate
traditional way of validatingtheresultsbymakingprototype
model and also saves time and money.
Meshing Condition
Table-2: Meshing Conditions
Parameters Chosen
Physical preference Mechanical
Element used Solid 185
Element shape Tetra hadron(Default)
Element size Default
Mesh type Medium size mesh
Analysis is done on die plate, bottom plate, top plate, and
stripper plate and guide pillar. The results obtained from
analysis is given below
i) Die Plate: for Die Plate D2 steel is chosen
Fig-7: Total deformation of Die Plate
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1433
Fig-8: Equivalent stresses on Die Plate
ii) Bottom Plate: For bottom plate Mild steel is used
Fig-9: Total deformation of bottom Plate
Fig-10: Equivalent stresses on bottom Plate
iii) Top Plate
Fig-11: Total deformation of Top Plate
Fig-12: Equivalent stresses on Top Plate
iv) Stripper Plate: For Stripper plate EN-31 steel isused for
Analysis
Fig-13: Total deformation of Stripper Plate
Fig-14: Equivalent stresses on die Plate
v) Guide Pillar
Fig-15: Total Deformation of Guide Pillar
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1434
Fig-16: Equivalent stresses on Guide Pillar
8. RESULT AND DISCUSSION
The following Table- 3 shows the results of the cost analysis
done for the raw materials and scrap materials which has
been wasting and not using for any other purposes.
Table-3: Cost Analysis of Material for U-Bracket
Raw Material
waste
Cost in Rs Scrap Waste Cost in
Rs
Raw material
per Kg
57 Scrap
material per
Kg
25
130Kg Raw
material per
day
7410 130 scrap per
day
3250
Raw material
per month (26
days)
192660 Scrap per
month
84500
Total direct Loss per month 108162
Table- 4 shows the U-bracket component cost analysis and
savings done by use of new designed tool
Table-4: Cost analysis of component
Description Cost
Present cost of component Rs.2
New component raw material cost per
piece
0.32 paise
Processing cost for new component 0.50 paise
Savings per component Rs.1.18
Table 5 and table 6 show the results obtained by ANSYS and
theoretical calculations are made for different components
of the progressive tool and results are compared with the
Ansys Result
Table- 4: Deformation Result
Components Ansys Result Theoretical Result
Deformation
in mm
Deformation in mm
Die plate 0.00093685 0.0003382
Top Plate 0.00035361 0.0040215
Bottom Plate 0.001256 0.0022952
Stripper
Plate
0.00014901 0.0007468
Guide Pillar 0.076174 0.0636969
Table-4: Stress Result
Components Yield
strength
(Mpa)
Ansys
Result
Theoretical
Result
Stress in
Mpa
Stress in
Mpa
Die Plate 1532 15.52 17.304
Top Plate 250 4.0376 6.172
Bottom Plate 250 12.19 10.93
Stripper Plate 450 3.4116 6.850
Guide Pillar 450 96.9 89.5
9. CONCLUSION
Progressive die is a cost-effective method to produce sheet
metal parts with different characteristics which include
strength, toughness and abrasion resistance, by the use of
newly designed progressive tool it is possible to overcome
the financial losses facing by the industry and Rs. 1, 08, 162
can be saved per month and also with this tool thecostofthe
component per piece is saved by Rs. 1.18. FEA analysis done
for different parts and it is seen that resultsareinacceptable
range and stress values obtained are less then yieldstrength
of material and Deformations obtained from manual
calculations closely match withAnsysresultsandweresmall
in the range of recommended deformation. Bed size of
mechanical press is 558×358 and tool dimension is
287×228mm therefore designed progressive tool perfectly
fits onto the bed of mechanical press.
REFERENCES
[1] Gashaw Desie and YONAS Mitiku Degu,“ProgressiveDie
Design for Engineering and Science (IJES), volume 3,
issue 3, Pages 75-85, 2014.
[2] Sunil Kumar and Lokeswar Patnaik, “Design and
Analysis of Four stage Progressive Tool for House-
wiring Wire Clip”, CVR Journal of Science and
Technology, Volume13, December 2017.
[3] Ch. Mastanamma, K. Prasada Rao, Dr. M. Venkateswara
Rao, “International Journal of EngineeringResearchand
Technology (IJERT)”, Volume 6, August-2012.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1435
[4] M Subrahmanyam, A Mokhalingam, “International
Journal of Engineering Research and Technology
(IJERT)”, Volume 5, Issue 06, June-2016.
[5] Gaurav C Rathode, Samadhan Adlinge, Dr. D N Raut,
“International Journal of Engineering Research and
Technology (IJERT)’, ISSN : 2278-0181.
[6] Prabhakar Purushothaman, Prashant Thankachan,
“American Journal of Mechanical and Industrial
Engineering”, October -2016; 1(3): 31-37 pages.
[7] Kassahun Nigussie Asfew, Wassihum Yimer Amdie,
“International Journal of Industrial and Manufacturing
Systems Engineering”, Volume 2(3), 2017, pages 19-23
[8] Cyril Donaldson, George H LeCain, V C Goold, Tool
Design 4th edition, Tata McGraw – Hill.
[9] Prakash H. Joshi, Press Tools Design and Construction,
A.H. Wheeler and Co. Ltd, 411, Surya Kiran, K.G. Marg,
New Delhi.

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IRJET- Design and Analysis of Progressive Tool for U-Bracket of Power Meter Cabinet

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1429 DESIGN AND ANALYSIS OF PROGRESSIVE TOOL FOR U-BRACKET OF POWER METER CABINET Narayan Chouhan1, N Manjunath Gowda2, Satish Kumar S3 1M.Tech Student, Dept. of studies in mechanical Engg, UBDTCE, Davangere, Karnataka, India 2Assistant Professor, Dept. of studies in mechanical Engg, UBDTCE, Davangere, Karnataka, India 3Partner, Elite Insulators, Mallashettyhalli (Davangere dist), Karnataka, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract -In the present situation, the production of U- brackets are made with a new raw material and in a two different tools, each tool requires press machines which leads to the usage of more resources and considerable financialloss thus the industry stopped the production of U-brackets and given out sources for the production. The present U-bracket components can be done using scrap material which is sufficiently available in industry and it has not all used forany other production. Considering all these criteria, the existing tools can be simplified with a single progressive tool so that usage of more resources can be simplified and can be done using scrap material and raw material cost will be saved. In this work a three stage progressive tool hasbeen designedand analyzed the stresses and deformation for different parts of progressive tool like top plate, bottom plate, dieplate, stripper plate and guide pillar. A progressive tool performs two or more operations at different stages in a single strokeofram to produce the part as the strip moves through the die. Modeling is carried out in SOLID EDGE VERSION 20 and simulation is carried out in ANSYS WORKBENCH 18.1 and result obtained from analysis is validated with manual calculations. The designed tool will help the industry to manufacture the part rather than outsourcing andhencesavesmoney. 30Tavailable mechanical press can be used with newly designed tool as the press capacity is greater than the required. Key Words: Progressive tool, U-Bracket, Scrap material, Raw material, Press capacity 1. INTRODUCTION In recent day’s different kinds of sheet metal developing processes were using in sheet metal product manufacturing companies. These sheet metal developing processes have been using for manufacturing various sections of airplanes, vehicles and ships etc. by using the complicated devices discovered from modern innovations. With the ever growing knowledge ofscienceandtechnology, the progressive tool design process has become more precise to satisfy the demand of moreproductivity,low price and better exactness. For a better improvement, the more delicate design development of today has not replaced the need for basic sheet forming of dies and process. The popularity of sheet metal stamping process is due to its high productivity, ease in manufacturing of intricate shapes and will be done at lower cost. The parts manufactured from the sheet metal have well good-looking qualities, better dimension accuracy, light weight and higher strength. For a better improvement, the more delicate design development of today has not replaced the need for basic sheet forming of dies and process. The popularity of sheet metal stamping process is due to its high productivity, ease in manufacturing of intricate shapes and will be done at lower cost. The parts manufactured from the sheet metal have well good-looking qualities,betterdimensionaccuracy, light weight and higher strength. 2. COMPONENT DATA Component Name: U-Bracket Material: CRCA Steel Thickness: 0.8mm Shear strength: 36 Kg/mm2 Tempered Grade: Cold Rolled Fig -1: Solid model of component U-bracket is a small component usedinthemetercabinetsto fix the domestic power meters. The 2D drawing is received from the industry. 3. PROBLEM STATEMENT  Currently for window cutting operation of the top box, the material of dimension100×90mmhasbeen wasting as scrap material and decreasing the productivity.  The industry used separatetwoseparatepresstools and machines for each sheet metal operations of U- bracket thus stopped productionandoutsourcingit.  New stamping tools like progressive tools which produce well superior quality and consistent parts with enormous amounthasnotcompletelyinstalled where ever its requirement meet.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1430  By analyzing the recorded problems it came to know that the problems became an obstacle to the production improvement. 3.1 Objectives of Work  To know the source of causes of less productivity in Elite Insulators and propose the possible of improvement in present production line.  Collecting geometrical details which describe size, shape and additional description of the component (U-bracket).  Modification of tool to use the available scrap material.  Suggesting the new tool as progressive tool. 4. METHODOLOGY Fig -2: Methodology Adopted 5. MODELING AND MATERIAL SELECTION 5.1 3D Model of Progressive Tool Fig -3: Progressive Tool Assembly Fig -4: Strip Layout 5.2 2D Drawings of Progressive tool and component Fig -5: Section view of progressive tool Fig -6: Component Drawing 5.3 Mechanical Properties of Tool Materials Table -1: Mechanical properties Property Mild steel (st-42) HCHC steel (D2 steel) EN-31 Steel Mass Density (Kg/m3) 7850 7700 7700 Yield strength (Mpa) 250 1532 450 Ultimate Tensile Strength (mpa) 460 1320 750 Possion’s ratio 0.303 0.3 0.3 Shear modulus(Gpa) 78 79 86 Young’s Modulus(Mpa) 210000 210000 215000
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1431 6. DESIGN CALCULATIONS 6.1 Strip layout Development Scrap Bridge (B) = (1 to 1.25)t B=1mm Margin (M) = (1.25 to 1.5).t M=1.5mm Area of Blank (component) = 22×87 =1914mm No. of Rows = 1 Pitch=Advance of die = L+B, where L = Length of blank =24mm Economy Factor = (blank size area × No. of rows)/ (Strip breadth × Pitch) ×100 Economy Factor = 92.46% % of strip used = ×100 =88.61% % of scrap = 100-88.61 = 11.31% 6.2 Die clearance and Tool Life Die clearance = thickness of work piece× suggested % For steel, Die clearance = (2.5 - 5%) t, where t=thickness of sheet Min. Die clearance = 0.02mm Max. Die clearance = 0.04mm Max clearance can cause burr and min clearance cause repeated reshaping of die and tool life decreases. For better tool life, the die clearance has an optimum average value. Optimum valuecanbecalculatedby averaging the min and max die clearances. Optimum clearance = 0.02+0.04/2 = 0.03mm 6.3 Force calculations Shearing force Fsh = L×t×fs Where Fsh = shear force or cutting force in tons fs = shear strength in Kg/mm2 L = cutting length in mm t= thickness of sheet = 0.8mm At stage 1, pitch punch Cutting length L1 = 54mm At stage 2, parting with embossing Cutting length L2 = 171mm At stage 3, small cut-off Cutting Lengt L3 = 20mm Total cutting length L = L1+L2+L3 =245mm Fsh = 7056Kgf Fsh = 7056×0.6 (for safety purpose 60% additional force is added) Fsh = 4233.3Kgf Fsh1 = 7056+4233.3 = 11529.6 Kgf Again 20% of force is added to make the tool theoretically strong Fsh2 = 11529.6×0.2 = 2305.92 Kgf Total shearing force = Fsh1+Fsh2 = 13835.52 =14000 Kgf = 14T Stripping Force Stripping force = 15% of shear force = 0.15×14 = 2.1T Total Force (F) = stripping Force+ Shearing Force ` = 14+2.1+2.1 = 16.1T 6.4 Press Capacity The total press capacity is 125% more than the total force calculated therefore Pc = total tonnage×1.25 = 20.125T 6.5 Stress and deflection calculation for different elements of Progressive tool a) Die Plate Die plate is considered as a fixed beam. The shoe deflection is computed from strength of material concept for fixed beam. Equation for deflection is given by δ = Where, F=80% of shearing force = 109834.4N E - Young’s modulus = 2.1×105N/mm2 I- Moment of inertia of plate in mm4 L- Least distance b/w successive fasteners=45.6mm Width, B = 167mm and thickness, H = 38mm F = 109834.4 N I = I = 763635.33 mm4 δ= 0.0003382mm Stress generated in the die plate is given by, σ = Where A = B×H = 167×38 = 6346mm2 σ =17.304 N/mm2 b) Bottom Plate Bottom plate is supported by number of parallel blocks hence we consider it as a simply supported beam. Using strength of materials, the deflection for simply supported beam with concentrated load, deflection equation is given below δ = , F = 80% shearing force =109834.4N
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1432 B = 287mm and H = 30mm L = 62mm I = 645750 mm4 δ = 0.0040215mm σ = = 6.172 N/mm2 C) Top Plate For analysis top plate is considered as a simply supported beam with concentrated load acting on it. The equation is given by δ = , where F=80%shearing force = 109834.4N B = 287mm and H = 35mm L = 60mm I = = 1025427.083mm4 δ =0.0022952mm σ = = 10.93N/mm2 D) Stripper Plate Assuming stripper plate to be a fixed beam, the deflection and stress calculation is done by adopting SOM concept as F = 20% shearing force = 27458.6 N B = 167mm and H = 24mm L = 60mm F = 20% shearing force = 27458.6 N I = = 192384mm4 δ = = 0.0007468mm σ = = 6.850N/mm2 E) Guide Pillar Considering guide pillar as a cantilever beam with load acting vertically on it and guide pillar is considered as one side fixed and another side for freecolumnconstruction. From strength of material, for column construction of one side is fixed and another side is free type. Load acting on guide pillar = 80% shearing force = 109834.4N Load per pillar P = = 54917N Crippling load Pc = Where, E = 2.15×105 N/mm2 Diameter of pillar = d = 28mm Pillar length = l = 150mm I = = 30175.768 mm4 Pc = 482708.54 N < 54917N Since applied load is less than the crippling load therefore applied load is harmless for design. A = = 615.83mm2 δ = = = 0.0636969 mm σ = = 89.9N/mm2 7. FINITE ELEMENT ANALYSIS Finite element analysis was carried out in Ansys workbench 18.1. For analysis of tool,thefivemajor elements of tool were chosen based on the maximum loading conditions. This helps to predict real condition of tool components in the operation. This helps to eliminate traditional way of validatingtheresultsbymakingprototype model and also saves time and money. Meshing Condition Table-2: Meshing Conditions Parameters Chosen Physical preference Mechanical Element used Solid 185 Element shape Tetra hadron(Default) Element size Default Mesh type Medium size mesh Analysis is done on die plate, bottom plate, top plate, and stripper plate and guide pillar. The results obtained from analysis is given below i) Die Plate: for Die Plate D2 steel is chosen Fig-7: Total deformation of Die Plate
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1433 Fig-8: Equivalent stresses on Die Plate ii) Bottom Plate: For bottom plate Mild steel is used Fig-9: Total deformation of bottom Plate Fig-10: Equivalent stresses on bottom Plate iii) Top Plate Fig-11: Total deformation of Top Plate Fig-12: Equivalent stresses on Top Plate iv) Stripper Plate: For Stripper plate EN-31 steel isused for Analysis Fig-13: Total deformation of Stripper Plate Fig-14: Equivalent stresses on die Plate v) Guide Pillar Fig-15: Total Deformation of Guide Pillar
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1434 Fig-16: Equivalent stresses on Guide Pillar 8. RESULT AND DISCUSSION The following Table- 3 shows the results of the cost analysis done for the raw materials and scrap materials which has been wasting and not using for any other purposes. Table-3: Cost Analysis of Material for U-Bracket Raw Material waste Cost in Rs Scrap Waste Cost in Rs Raw material per Kg 57 Scrap material per Kg 25 130Kg Raw material per day 7410 130 scrap per day 3250 Raw material per month (26 days) 192660 Scrap per month 84500 Total direct Loss per month 108162 Table- 4 shows the U-bracket component cost analysis and savings done by use of new designed tool Table-4: Cost analysis of component Description Cost Present cost of component Rs.2 New component raw material cost per piece 0.32 paise Processing cost for new component 0.50 paise Savings per component Rs.1.18 Table 5 and table 6 show the results obtained by ANSYS and theoretical calculations are made for different components of the progressive tool and results are compared with the Ansys Result Table- 4: Deformation Result Components Ansys Result Theoretical Result Deformation in mm Deformation in mm Die plate 0.00093685 0.0003382 Top Plate 0.00035361 0.0040215 Bottom Plate 0.001256 0.0022952 Stripper Plate 0.00014901 0.0007468 Guide Pillar 0.076174 0.0636969 Table-4: Stress Result Components Yield strength (Mpa) Ansys Result Theoretical Result Stress in Mpa Stress in Mpa Die Plate 1532 15.52 17.304 Top Plate 250 4.0376 6.172 Bottom Plate 250 12.19 10.93 Stripper Plate 450 3.4116 6.850 Guide Pillar 450 96.9 89.5 9. CONCLUSION Progressive die is a cost-effective method to produce sheet metal parts with different characteristics which include strength, toughness and abrasion resistance, by the use of newly designed progressive tool it is possible to overcome the financial losses facing by the industry and Rs. 1, 08, 162 can be saved per month and also with this tool thecostofthe component per piece is saved by Rs. 1.18. FEA analysis done for different parts and it is seen that resultsareinacceptable range and stress values obtained are less then yieldstrength of material and Deformations obtained from manual calculations closely match withAnsysresultsandweresmall in the range of recommended deformation. Bed size of mechanical press is 558×358 and tool dimension is 287×228mm therefore designed progressive tool perfectly fits onto the bed of mechanical press. REFERENCES [1] Gashaw Desie and YONAS Mitiku Degu,“ProgressiveDie Design for Engineering and Science (IJES), volume 3, issue 3, Pages 75-85, 2014. [2] Sunil Kumar and Lokeswar Patnaik, “Design and Analysis of Four stage Progressive Tool for House- wiring Wire Clip”, CVR Journal of Science and Technology, Volume13, December 2017. [3] Ch. Mastanamma, K. Prasada Rao, Dr. M. Venkateswara Rao, “International Journal of EngineeringResearchand Technology (IJERT)”, Volume 6, August-2012.
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 09 | Sep 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.34 | ISO 9001:2008 Certified Journal | Page 1435 [4] M Subrahmanyam, A Mokhalingam, “International Journal of Engineering Research and Technology (IJERT)”, Volume 5, Issue 06, June-2016. [5] Gaurav C Rathode, Samadhan Adlinge, Dr. D N Raut, “International Journal of Engineering Research and Technology (IJERT)’, ISSN : 2278-0181. [6] Prabhakar Purushothaman, Prashant Thankachan, “American Journal of Mechanical and Industrial Engineering”, October -2016; 1(3): 31-37 pages. [7] Kassahun Nigussie Asfew, Wassihum Yimer Amdie, “International Journal of Industrial and Manufacturing Systems Engineering”, Volume 2(3), 2017, pages 19-23 [8] Cyril Donaldson, George H LeCain, V C Goold, Tool Design 4th edition, Tata McGraw – Hill. [9] Prakash H. Joshi, Press Tools Design and Construction, A.H. Wheeler and Co. Ltd, 411, Surya Kiran, K.G. Marg, New Delhi.