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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4393
Influence of Heat Treatment on Internal Stresses and Non-
Homogeneity for A360 Aluminium Alloy Housing Component
Apurva P. Takle1, Rohit D. Pardeshi2, Shweta R. Dhavale3, Sagar B. Sakhare4, Chandrika Wagle5,
Vijay Natikar6
1Student & Moshi, Pune
2,3Student & Daund, Pune
4Student & Virgaon, Aurangabad
5Professor, Dept. of Mechanical Engineering, Dr. D. Y. Patil Institute of Technology, Pimpri, Maharashtra,India
6Senior Engineer, Dept. of Manufacturing Engineering, Sigma Electric Mfg. Corp.,Chakan Maharashtra ,India
---------------------------------------------------------------------***----------------------------------------------------------------------
Abstract - There are many factors that affects the dimensions
of the manufactured products, there can be defect in the
product’s manufacturing processes, material composition
leading to change in physical and chemical properties,
handling methods, etc. The purpose of this study is to
investigate the main causes of variation in the dimensions of
the A360 Aluminium alloy components and to provide a
solution for it. Six Sigma DMAIC approach is adopted as
methodology. Internal stresses and non homogeneity due to
entrapped gases were the root causes found. At elevated
temperatures the component tries to attain homogeneity and
relieve those internal stresses due to which variation in
dimension and geometry in thecomponentisbeenobserved. In
this paper, how adding of Heat Treatment in manufacturing
process affects and is beneficial for the component is
validated. Use of Process Capability index to indicate for the
long run of the process without any errors.
Key Words: Heat Treatment, Internal Stresses, Non-
Homogeneity, A360 Alloy, Defects .
1. INTRODUCTION
Material Properties of Aluminium Alloy A360
A360 is an aluminium alloywithexcellentpressuretightness
and fluidity. It has high silicon content and offers high
corrosion resistance as well as high strength, even at
elevated temperatures. It has more ductility than other
Aluminium Alloy
TABLE 1
Mechanical Properties
Material Aluminium
Alloy A360
Tensile Strength (MPa) 317
Yield Strength (MPa) 170
Shear Strength (MPa) 180
Hardness (HB) 75
TABLE 2
TABLE 3
Material Composition
Silicon 9-10%
Iron 1.3%
Copper 0.6%
Mg 0.35%
Mn 0.4-0.6%
Nickel 0.5%
Zinc 0.5%
Tin 0.15%
Others 0.25%
Aluminum Balance (85-87%)
1.2 Manufacturing Process Flow of the Component
High Pressure Die Casting
ↆ
Fettling
ↆ
Machining
ↆ
Pre-Treatment and Cleaning
ↆ
Powder Coating
ↆ
Curing
ↆ
Inspection
Physical Properties
Process Cold Chamber Die Casting
Density (g/cm3) 2.63
Melting Point (Average ±
500C)
577
Thermal Conductivity
(W/mK)
113
Coefficient of Thermal
Expansion (µm/mK)
21
Electrical Conductivity
(%IACS)
29
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4394
● High Pressure Die Casting
Die casting is a metal casting process that is characterized
by forcing molten metal under high pressure into a mold
cavity. The mold cavity is created using two hardened tool
steel dies which have been machined into shape and work
similarly to an injection mold during the process.
Most die castings are made from non-ferrous metals,
specifically zinc, copper, aluminium, magnesium, lead, and
tin-based alloys. The casting equipment and the metal dies
represent large capital costs and this tends to limit the
process to high-volume production. Manufacture of parts
using die casting is relatively simple, involving only four
main steps which keeps the incremental cost peritemlow.It
is especially suited for a large quantity of small- to medium-
sized castings, which is why die casting produces more
castings than any other casting process. Die castings are
characterized by a very good surface finish (by casting
standards) and dimensional consistency.
The high-pressure injection leads to a quick fill of the die,
which is required so the entire cavity fills before any part of
the casting solidifies. In this way, discontinuities areavoided.
This creates the problem of air entrapment. This problem is
minimized by including vents along the parting lines.
● Fettling
The complete process of cleaning of casting is called
Fettling process. The cleaningisdonemanuallyforsmall cast
products. It involves the removal of cores, gates, sprues,
runners, risers and chipping of any unnecessary projections
on the surface of the castings. After fettling castings goes
through glass beading process which is a metal cleaning
process that creates a clean, bright and uniform matte
texture. The glass beads are applied to a surface using low
air pressure. This process removesimpuritiespresenton the
metal surface.
● Machining
The process of removing metal from the workpiece is
called Machining process. Conventional method is used for
machining with the help of Brother 10 special purpose
machine. Operations performed on the castings are drilling,
boring, tapping, finishing.
● Pre-Treatment and Cleaning
Pre-Treatment is a surface preparation process prior to
powder coating. It includes removal of dirt, oil, grease,
surface impurities and the oxidationproductspresentonthe
surface by means of chemicals. The components are dipped
in different chemical baths of different concentrations.
Coating is done immediately after Pre-Treatment process
because the cleaned surface is in the highly reactive state
and it can get corroded quickly. After Pre-Treatment
masking is done to prevent painting on unwanted areas.
Sr.No. Bath Temp pH
1. Hot water Rins 60-70◦C 6-8
2. Degreasing Surtech
133
60-70◦C 9-10
3. Water Rins1 R.Temp 6-9
4. Water Rins2 R.Temp 6-8
5. Activation R.Temp 1-2
6. Water Rins1 R.Temp 4-5
7 Water Rins R.Temp 6-8
8. Passivation Surtech
650
R.Temp 2.5-4
9. DI Rins1 R.Temp 6-7
10 DI rins 2 R.Temp 6-7
Total Process Time 23 min 33 sec
● Powder Coating and Curing Process
After masking painting is done on the productusingspray
gun. Powder coating is a type of coating that is applied as a
free-flowing, dry powder. The main difference between a
conventional liquid paint and a powder coating is that the
powder coating does not require a solvent to keep the
binder and filler parts in a liquid suspension form. The
coating is typically applied electrostaticallyandisthencured
under heat to allow it to flow and form a "skin". The powder
may be a thermoplastic or a thermoset polymer. It is usually
used to create a hard finish that is tougherthanconventional
paint. Curing is the process in which components are passed
through curing oven. The Curingovenismaintainedat2000C
to 215oC. Curing Process
2. Problem Statement
Variation in Critical to Quality dimensionsanddistortionof
threads in components were observedwhichledtofailure of
pressure leak test and Go NO-Gauge during inspection on
large scale. The dimension varied were observed to be
exceeding the specification limit by 25-30 microns . As the
component is been used in explosive areas,itisimportantto
maintain the CTQ dimensions and threaded sections
3. Solution
After studying all the process parameter we found that
internal stresses and non-homogeneity being the root cause
of the problem. As the component is high pressure die
casted followed by low solidification time of 3 seconds
which led to generation of internal stresses and due these
stresses variation were observed at elevated temperature .
After studying the manufacturing process , referringvarious
research paper and reference books, it was found that Heat
Treatment is been used for attaining homogeneity and for
relieving of internal stresses . Heat Treatment is a Special
Process, the results of which cannot be predicted and hence
trial and error method is been optioned. We decided to
perform Heat Treatment on the components before
machining so that whatever the variation in the CTQ
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4395
dimensions will occur due to stress relieving will get
compensated in the machining process itself .
3.1 Modified Process Flow Chart
High Pressure Die Casting
ↆ
Fettling
ↆ
Heat Treatment
ↆ
Machining
ↆ
Pre-Treatment and Cleaning
ↆ
Powder Coating
ↆ
Curing
ↆ
Inspection
4. EXPERIMENT
For this we made 3 batches of 30 components each which
were heated for different temperatures and time duration.
We measured the CTQ dimensions after each process.
Fig 1- Convection HeatIng Oven for Components
BATCH No. HEAT TREATMENT
Time Temperature
Batch 1 4 hours 200oC
Batch 2 6 hours 200oC
Batch 3 6 hours 260oC
Table 4 – Temperature and time duration for Heat
Treatment
Quality Control Instruments used
1. Vernier Caliper for internal diameter
2. Air Plug Gauge
3. Go and no go Gauge for Threads
4.1 Dimensional Analysis
As the batches of componentsareheattreatedfordifferent
time and temperature . To check whether theheattreatment
has affected the components , it is investigatedwiththehelp
of dimensional analysis of those Critical to Quality
dimensions carried out with quality control instruments .
The graph plotted are for Heat Treatment , Machining , Pre-
Treatment and Curing Process ,
Final Inspection is for acceptance and Rejection of
components.
4.1.1 Batch 1 Dimensional Analysis
A) Heat Treatment
B) Machining , Pre-Treatment and Curing
4.1.2 Batch 2 Dimensional Analysis
A) Heat Treatment
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4396
B) Machining , Pre-Treatment and Curing
4.1.3 Batch 3 Dimensional Analysis
A) Heat Treatment
B) Machining , Pre-Treatment and Curing
5. RESULT
Batch 3 gave the best result, with lower variation in
dimensions , maintaining circularity and geometry of
threads.
Sr. No Dimension (mm) Final Dimension
Range (mm)
1 Ø72.55±0.05 72.55 – 72.59
2 Ø64.55±0.05 64.55 – 64.59
3 Ø50.385±0.015 50.385 – 50.389
6. CONCLUSION
Batch 3 which was heat treated for 6 hours at 2600C gave
the best result , with dimensional variation under
specified tolerance limit . NO failure in Gauge inspection
and pressure leak test were observed . 100% of the
components passed the gauge test.
REFERENCES
[1] Dr. Srihari G. Acharya “Design for productivity using
GD&T” , New Jersey’s Science & Technology University
[2] Mr. Bhavesh Mistry and Dr. P.M. George “Study and
Scope of DFMA and GD&T in Manufacturing Process-
Case study on dual plate check valve “,7th international
conference on advanced computingandcommunication
technologies - ICACCT 2013, At panipat, Haryana,
Volume: 4.
[3] Mr. Hemant Urdhwarshe “The Six Sigma approach“,
Symphony productivity journal, March 2000 and
Reproduced in Quality World March 2006.
[4] Mr. Franco Bonollo , Mr Nicola Gramegna and Mr. Giulio
Timelli “High Pressure Die Casting –Contradictions and
Challenges”, The journal of the Minerals, Metals &
Materials Society ISSN 1047-4838 Volume 67 No.5
[5] Dr. Laxaminarayan and Dr.A. Chennakesavareddy
“Influenece of Heat Treatment on mechanical behavior
of Aluminium 7075/silicon carbide composites
manufactured by casting process”, International
Conference on Advanced Materials and manufacturing
Technologies (AMMT) December 18-20, 2014
[6] M.S. Rahman , M.Z.H. Khan and M.F.I.A. Imam
“Influence of Heat Treatment on Fatigue and fracture
behavior of Aluminium Alloys”, Journal of Engineering
Science and Technology Vol.10 No. 6 (2015) 730-742
[7] Mr. Yerriswamy Wooluru and Dr. P. Nagesh
“The process capability analysis – A tool for process
performance meausres and matrices”, International
Journal of Quality Research 8(3) 399-416
BIOGRAPHIES
Name – Apurva P. Takle
Student of Mechanical Engineering
From Dr. D. Y. Patil Institute of
Technology , Pimpri- 18
Name – Rohit D. Pardeshi
Student of Mechanical Engineering
From Dr. D. Y. Patil Institute of
Technology , Pimpri- 18
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072
© 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4397
Name – Shweta R. Dhavale
Student of Mechanical Engineering
From Dr. D. Y. Patil Institute of
Technology , Pimpri- 18
Name – Sagar B. Sakhare
Student of Mechanical Engineering
From Dr. D. Y. Patil Institute of
Technology , Pimpri- 18

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IRJET- Influence of Heat Treatment on Internal Stresses and Non-Homogeneity for A360 Aluminium Alloy Housing Component

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4393 Influence of Heat Treatment on Internal Stresses and Non- Homogeneity for A360 Aluminium Alloy Housing Component Apurva P. Takle1, Rohit D. Pardeshi2, Shweta R. Dhavale3, Sagar B. Sakhare4, Chandrika Wagle5, Vijay Natikar6 1Student & Moshi, Pune 2,3Student & Daund, Pune 4Student & Virgaon, Aurangabad 5Professor, Dept. of Mechanical Engineering, Dr. D. Y. Patil Institute of Technology, Pimpri, Maharashtra,India 6Senior Engineer, Dept. of Manufacturing Engineering, Sigma Electric Mfg. Corp.,Chakan Maharashtra ,India ---------------------------------------------------------------------***---------------------------------------------------------------------- Abstract - There are many factors that affects the dimensions of the manufactured products, there can be defect in the product’s manufacturing processes, material composition leading to change in physical and chemical properties, handling methods, etc. The purpose of this study is to investigate the main causes of variation in the dimensions of the A360 Aluminium alloy components and to provide a solution for it. Six Sigma DMAIC approach is adopted as methodology. Internal stresses and non homogeneity due to entrapped gases were the root causes found. At elevated temperatures the component tries to attain homogeneity and relieve those internal stresses due to which variation in dimension and geometry in thecomponentisbeenobserved. In this paper, how adding of Heat Treatment in manufacturing process affects and is beneficial for the component is validated. Use of Process Capability index to indicate for the long run of the process without any errors. Key Words: Heat Treatment, Internal Stresses, Non- Homogeneity, A360 Alloy, Defects . 1. INTRODUCTION Material Properties of Aluminium Alloy A360 A360 is an aluminium alloywithexcellentpressuretightness and fluidity. It has high silicon content and offers high corrosion resistance as well as high strength, even at elevated temperatures. It has more ductility than other Aluminium Alloy TABLE 1 Mechanical Properties Material Aluminium Alloy A360 Tensile Strength (MPa) 317 Yield Strength (MPa) 170 Shear Strength (MPa) 180 Hardness (HB) 75 TABLE 2 TABLE 3 Material Composition Silicon 9-10% Iron 1.3% Copper 0.6% Mg 0.35% Mn 0.4-0.6% Nickel 0.5% Zinc 0.5% Tin 0.15% Others 0.25% Aluminum Balance (85-87%) 1.2 Manufacturing Process Flow of the Component High Pressure Die Casting ↆ Fettling ↆ Machining ↆ Pre-Treatment and Cleaning ↆ Powder Coating ↆ Curing ↆ Inspection Physical Properties Process Cold Chamber Die Casting Density (g/cm3) 2.63 Melting Point (Average ± 500C) 577 Thermal Conductivity (W/mK) 113 Coefficient of Thermal Expansion (µm/mK) 21 Electrical Conductivity (%IACS) 29
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4394 ● High Pressure Die Casting Die casting is a metal casting process that is characterized by forcing molten metal under high pressure into a mold cavity. The mold cavity is created using two hardened tool steel dies which have been machined into shape and work similarly to an injection mold during the process. Most die castings are made from non-ferrous metals, specifically zinc, copper, aluminium, magnesium, lead, and tin-based alloys. The casting equipment and the metal dies represent large capital costs and this tends to limit the process to high-volume production. Manufacture of parts using die casting is relatively simple, involving only four main steps which keeps the incremental cost peritemlow.It is especially suited for a large quantity of small- to medium- sized castings, which is why die casting produces more castings than any other casting process. Die castings are characterized by a very good surface finish (by casting standards) and dimensional consistency. The high-pressure injection leads to a quick fill of the die, which is required so the entire cavity fills before any part of the casting solidifies. In this way, discontinuities areavoided. This creates the problem of air entrapment. This problem is minimized by including vents along the parting lines. ● Fettling The complete process of cleaning of casting is called Fettling process. The cleaningisdonemanuallyforsmall cast products. It involves the removal of cores, gates, sprues, runners, risers and chipping of any unnecessary projections on the surface of the castings. After fettling castings goes through glass beading process which is a metal cleaning process that creates a clean, bright and uniform matte texture. The glass beads are applied to a surface using low air pressure. This process removesimpuritiespresenton the metal surface. ● Machining The process of removing metal from the workpiece is called Machining process. Conventional method is used for machining with the help of Brother 10 special purpose machine. Operations performed on the castings are drilling, boring, tapping, finishing. ● Pre-Treatment and Cleaning Pre-Treatment is a surface preparation process prior to powder coating. It includes removal of dirt, oil, grease, surface impurities and the oxidationproductspresentonthe surface by means of chemicals. The components are dipped in different chemical baths of different concentrations. Coating is done immediately after Pre-Treatment process because the cleaned surface is in the highly reactive state and it can get corroded quickly. After Pre-Treatment masking is done to prevent painting on unwanted areas. Sr.No. Bath Temp pH 1. Hot water Rins 60-70◦C 6-8 2. Degreasing Surtech 133 60-70◦C 9-10 3. Water Rins1 R.Temp 6-9 4. Water Rins2 R.Temp 6-8 5. Activation R.Temp 1-2 6. Water Rins1 R.Temp 4-5 7 Water Rins R.Temp 6-8 8. Passivation Surtech 650 R.Temp 2.5-4 9. DI Rins1 R.Temp 6-7 10 DI rins 2 R.Temp 6-7 Total Process Time 23 min 33 sec ● Powder Coating and Curing Process After masking painting is done on the productusingspray gun. Powder coating is a type of coating that is applied as a free-flowing, dry powder. The main difference between a conventional liquid paint and a powder coating is that the powder coating does not require a solvent to keep the binder and filler parts in a liquid suspension form. The coating is typically applied electrostaticallyandisthencured under heat to allow it to flow and form a "skin". The powder may be a thermoplastic or a thermoset polymer. It is usually used to create a hard finish that is tougherthanconventional paint. Curing is the process in which components are passed through curing oven. The Curingovenismaintainedat2000C to 215oC. Curing Process 2. Problem Statement Variation in Critical to Quality dimensionsanddistortionof threads in components were observedwhichledtofailure of pressure leak test and Go NO-Gauge during inspection on large scale. The dimension varied were observed to be exceeding the specification limit by 25-30 microns . As the component is been used in explosive areas,itisimportantto maintain the CTQ dimensions and threaded sections 3. Solution After studying all the process parameter we found that internal stresses and non-homogeneity being the root cause of the problem. As the component is high pressure die casted followed by low solidification time of 3 seconds which led to generation of internal stresses and due these stresses variation were observed at elevated temperature . After studying the manufacturing process , referringvarious research paper and reference books, it was found that Heat Treatment is been used for attaining homogeneity and for relieving of internal stresses . Heat Treatment is a Special Process, the results of which cannot be predicted and hence trial and error method is been optioned. We decided to perform Heat Treatment on the components before machining so that whatever the variation in the CTQ
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4395 dimensions will occur due to stress relieving will get compensated in the machining process itself . 3.1 Modified Process Flow Chart High Pressure Die Casting ↆ Fettling ↆ Heat Treatment ↆ Machining ↆ Pre-Treatment and Cleaning ↆ Powder Coating ↆ Curing ↆ Inspection 4. EXPERIMENT For this we made 3 batches of 30 components each which were heated for different temperatures and time duration. We measured the CTQ dimensions after each process. Fig 1- Convection HeatIng Oven for Components BATCH No. HEAT TREATMENT Time Temperature Batch 1 4 hours 200oC Batch 2 6 hours 200oC Batch 3 6 hours 260oC Table 4 – Temperature and time duration for Heat Treatment Quality Control Instruments used 1. Vernier Caliper for internal diameter 2. Air Plug Gauge 3. Go and no go Gauge for Threads 4.1 Dimensional Analysis As the batches of componentsareheattreatedfordifferent time and temperature . To check whether theheattreatment has affected the components , it is investigatedwiththehelp of dimensional analysis of those Critical to Quality dimensions carried out with quality control instruments . The graph plotted are for Heat Treatment , Machining , Pre- Treatment and Curing Process , Final Inspection is for acceptance and Rejection of components. 4.1.1 Batch 1 Dimensional Analysis A) Heat Treatment B) Machining , Pre-Treatment and Curing 4.1.2 Batch 2 Dimensional Analysis A) Heat Treatment
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4396 B) Machining , Pre-Treatment and Curing 4.1.3 Batch 3 Dimensional Analysis A) Heat Treatment B) Machining , Pre-Treatment and Curing 5. RESULT Batch 3 gave the best result, with lower variation in dimensions , maintaining circularity and geometry of threads. Sr. No Dimension (mm) Final Dimension Range (mm) 1 Ø72.55±0.05 72.55 – 72.59 2 Ø64.55±0.05 64.55 – 64.59 3 Ø50.385±0.015 50.385 – 50.389 6. CONCLUSION Batch 3 which was heat treated for 6 hours at 2600C gave the best result , with dimensional variation under specified tolerance limit . NO failure in Gauge inspection and pressure leak test were observed . 100% of the components passed the gauge test. REFERENCES [1] Dr. Srihari G. Acharya “Design for productivity using GD&T” , New Jersey’s Science & Technology University [2] Mr. Bhavesh Mistry and Dr. P.M. George “Study and Scope of DFMA and GD&T in Manufacturing Process- Case study on dual plate check valve “,7th international conference on advanced computingandcommunication technologies - ICACCT 2013, At panipat, Haryana, Volume: 4. [3] Mr. Hemant Urdhwarshe “The Six Sigma approach“, Symphony productivity journal, March 2000 and Reproduced in Quality World March 2006. [4] Mr. Franco Bonollo , Mr Nicola Gramegna and Mr. Giulio Timelli “High Pressure Die Casting –Contradictions and Challenges”, The journal of the Minerals, Metals & Materials Society ISSN 1047-4838 Volume 67 No.5 [5] Dr. Laxaminarayan and Dr.A. Chennakesavareddy “Influenece of Heat Treatment on mechanical behavior of Aluminium 7075/silicon carbide composites manufactured by casting process”, International Conference on Advanced Materials and manufacturing Technologies (AMMT) December 18-20, 2014 [6] M.S. Rahman , M.Z.H. Khan and M.F.I.A. Imam “Influence of Heat Treatment on Fatigue and fracture behavior of Aluminium Alloys”, Journal of Engineering Science and Technology Vol.10 No. 6 (2015) 730-742 [7] Mr. Yerriswamy Wooluru and Dr. P. Nagesh “The process capability analysis – A tool for process performance meausres and matrices”, International Journal of Quality Research 8(3) 399-416 BIOGRAPHIES Name – Apurva P. Takle Student of Mechanical Engineering From Dr. D. Y. Patil Institute of Technology , Pimpri- 18 Name – Rohit D. Pardeshi Student of Mechanical Engineering From Dr. D. Y. Patil Institute of Technology , Pimpri- 18
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 06 Issue: 04 | Apr 2019 www.irjet.net p-ISSN: 2395-0072 © 2019, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 4397 Name – Shweta R. Dhavale Student of Mechanical Engineering From Dr. D. Y. Patil Institute of Technology , Pimpri- 18 Name – Sagar B. Sakhare Student of Mechanical Engineering From Dr. D. Y. Patil Institute of Technology , Pimpri- 18