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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1311
DESIGN, THERMAL ANALYSIS AND OPTIMIZATION OF A PISTON USING
ANSYS
Shahanwaz Adam Havale1, Prof. Santosh Wankhade2
1M.E. Student, Dept. of Mechanical Engineering, Y.T.I.E.T., Maharashtra, India
2 Assistant Professor, Dept. of Mechanical Engineering, Y.T.I.E.T., Maharashtra, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - As the main heating part in the engine, piston
works for a long time in high temperature and high load
environment. The piston has the characteristics of large
heating area and poor heat dissipation, so the thermal load is
the most serious problem. This thesis presents a numerical
method using thermos-mechanical decoupled FEM (Finite
Element Method) to calculate the thermal stress only caused
by the uneven temperature distribution. Inthis work, themain
emphasis is placed on the study of thermal behavior of
functionally graded materials obtained by means of using a
commercial code ANSYS on aluminum alloy piston surfaces.
The analysis is carried out to reduce the stress concentration
on the upper end of the piston i.e. (piston head/crown and
piston skirt and sleeve). With using computer-aided design,
SolidWorks software the structural model of a piston will be
developed. Furthermore, the finite element analysis is done
using Computer Aided Simulation software ANSYS.
Key Words: Piston, Aluminium Alloy, Stress, Thermos-
mechanical decoupled FEM, ANSYS
1. INTRODUCTION
Automobile components are in great demand these days
because of increased use of automobiles. The increased
demand is due to improved performanceandreducedcostof
these components. R&D and testing engineers should
develop critical components in shortest possible time to
minimize launch time for new products. This necessitates
understanding of new technologies and quick absorption in
the development of new products.
A piston is a component of reciprocatingIC-engines.
It is the moving component that is contained by a cylinder
and is made gas-tight by piston rings. In an engine, its
purpose is to transfer force from expanding gas in the
cylinder to the crankshaft via a pistonrodand/orconnecting
rod. As an important part in an engine, piston endures the
cyclic gas pressure and the inertial forces at work, and this
working condition may cause the fatigue damage of piston,
such as piston side wear, piston head/crown cracks and so
on. The investigations indicate that the greatest stress
appears on the upper end of the piston and stress
concentration is one of the mainly reason for fatigue failure.
On the other hand, pistonoverheating-seizurecanonlyoccur
when something burns or scrapes away the oil film that
exists between the piston and the cylinder wall.
1.1 Problem Statement
Based on the literature survey performed, venture
into this research is motivated by the fact that Pistons are
required to havehighperformancecharacteristicsandbetter
precision as they are supposed to sustain high temperature
and stresses. Piston skirt may appear deformation at work,
which usually causes crack on the upper end of piston head.
Due to the deformation, the greatest stress concentration is
caused on the upper end of piston, the situation becomes
more serious when the stiffness of the piston is not enough,
and the crack generally appeared at the point A which may
gradually extend and even cause splitting along the piston
vertical. The stress distribution on the piston mainly
depends on the deformation of piston. Therefore, inorder to
reduce the stress concentration, the piston crown should
have enough stiffness to reduce the deformation.
Exponential analysis of piston is hectic andnotvery
precise work. Exact theoretical analysis of piston
characteristics is very difficult. With the use of high speed
computers and the numerical techniques,the pistonanalysis
can be made using CAE. That’s why stress analysis is to be
performed using simulation software. Thus, the FEA will be
carried out for standard piston model used in diesel engine
and optimisation of the same will be carried out.
1.2 Objective
The main objective of the presentwork istofindout
and suggest optimum material for piston based on quality
and economy considering material weight and dimensional
issues at the same time. After generating an accurate finite
element model, a strategyfor theoptimization workflow was
defined. Target of the optimization wastoreachatminimum
thermal stresses in the piston.
The proposed work included following steps:
 Study of literature review of variouswork reported.
 The piston is designed according to the procedure
and specification which are giveninmachinedesign
and data hand books.
 CAD model of Piston is created using various tools
in SolidWorks.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1312
 FE analysis of the above geometry for different
loading and boundary conditions is done as
o Gas Pressure at top of the Piston (3MPa)
o Temperature at the top of the Piston
(200°C- 300°C).
o Heat transfer Coefficient (5E-6 W/mm oC.)
o Frictionless Supports.
 Comparison of the result obtained in above step for
different materials.
 Choosing the optimum designbasedonthematerial
and other parameter.
2. LITERATURE REVIEW
Dipayan Sinha, Susenjit Sarkar and Samar Chandra Mandal
[1] (June 2017) presented the study of Thermo-Mechanical
Analysis of a Piston with Different Thermal Barrier Coating
Configuration. In the present work a piston has been
analyzed numerically with FEA software named ANSYS
Workbench to evaluate its thermos-mechanical capability
under a predefined thermal and structural load. To enhance
the performance of the engine, weight of the piston has been
kept minimum by optimizing different dimensions. Yaohui
Lu, Xing Zhang, Penglin Xiang, Dawei Dong [2] (Nov. 2016)
presented the study of Analysis of Thermal Temperature
Fieldsand Thermal Stress under Steady Temperaturefieldof
Diesel Engine Piston. This paper tries to present a new
calculation method for the theoretical design of the piston.
Vaishali R. Nimbarte, Prof. S.D. Khamankar [3] (Aug 2015)
presented the study of stress analysis of piston using
pressure load and thermal load. The main objective of this
research work is to investigate and analyze the stress
distribution of piston atactual engine condition.Inthispaper
pressure analysis, thermal analysis and thermo-mechanical
analysis is done. The parameter used for the analysis is
operating gas pressure, temperatureandmaterialproperties
of piston. Muhammet Cerit*, Mehmet Coban [4] (2014)
presented the study of Temperature and thermal stress
analyses of a ceramic-coated aluminum alloy pistonusedina
diesel engine. The goal of this paper is to determine both
temperature and thermal stress distributions in a
plasmasprayed magnesia-stabilized zirconia coating on an
aluminum piston crown to improve the performance of a
diesel engine. R. Bhagat, Y. M. Jibhakate [5] (Aug-2012)
presented the study of Thermal Analysis and Optimizationof
I.C. Engine Piston Using finite Element Method. This paper
describes the stress distribution of the seizure on pistonfour
stroke engines by using FEA. The finite element analysis is
performed by using computer aided design (CAD) software.
The main objective is to investigate and analyze the thermal
stress distribution of piston at the real engine condition
during combustion process. The paper describes the mesh
optimization with using finite element analysis technique to
predict the higher stress and critical region on the
component.
3. ANALYTICAL CALCULATIONS
Analytical calculations are done for cast iron piston. For
doing analytical calculation material properties and
dimensional information should be known and so all the
parameters consider for design of piston are calculated by
using one analytical problem.
3.1 Procedure for Piston Design
The procedure for piston designs consists of the following
steps:
a. Thickness of piston head ( )
b. Heat flows through the piston head (H)
c. Radial thickness of the ring ( )
d. Axial thickness of the ring ( )
e. Width of the top land ( )
f. Width of other ring lands ( )
TABLE -1: DESIGN SPECIFICATION FOR PISTON
SR.
NO.
DESCRIPTION NOTATION UNIT
VALUE
ARRIVED
VALUE
USED
1
Length of
Piston
L Mm -- 75
2
Outside
diameter of
Piston
D Mm -- 84
3
Thickness of
Piston Head
Mm 7.75 10
4
Radial
thickness of
the ring
Mm 2.84 4
5
Axial
thickness of
the ring
Mm 4 4
6
Maximum
Thickness of
barrel
Mm 11.42 12
7
Width of the
top land
Mm 12 12
8
Width of
other ring
lands
Mm 4 4
4. MATERIAL SELECTION
Pistons are produced from cast or forged, high-temperature
resistantaluminumsilicon alloys. Therearethreebasictypes
of aluminum piston alloys. The standard piston alloy is a
eutectic Al-12%Si alloy containing in addition approx. 1%
each of Cu, Ni and Mg. Special eutectic alloys have been
developed for improved strength at high temperatures.
Hypereutectic alloys with 18 and 24% Si provide lower
thermal expansion and wear, but have lower strength (see
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1313
tabled property data on the following pages). In practice, the
supplier of aluminum pistons use a wide range of further
optimized alloy compositions, but generally based on these
basic alloy types. The majority of pistons are produced by
gravity die casting. Optimized alloy compositions and a
properly controlled solidification conditions allow the
production of pistons with low weight and high structural
strength.
5. FINITE ELEMENT METHOD
5.1 Introduction
Finite ElementMethod(FEM)isa computer-based numerical
technique for calculating the Strength and behavior of
engineering structures. It can be used to calculatedeflection,
stress, vibration, Buckling behavior and many other
phenomena. In the finite element method, a structure is
broken down into many small simple blocks or elements.
The behavior of an individual element can be describedwith
a relatively simple set of equations. Just as the set of
elements would be joined together to build the whole
structure, the equation describing the behaviors of the
individual elements are joined into an extremely large set of
equations that describe the behavior of the whole structure.
The computer can solve this set of simultaneous equations.
From the solution, the computer extracts the behaviorofthe
individual elements. From this, it can get the stress and
deflection of all the parts of the structure. The stresses will
be compared to allowed values of stress for the materials to
be used, to see if the structure is strong enough.
5.2 Basic steps in FEM
 Discretization of the structure
 Selection of proper interpolation or displacement
model
 Derivation of element stiffness matrices and load
vectors
 Solution for the unknown nodal displacements
 Computational of elemental stress and strains
5.3 Optimization using FEA
Optimization of an engineering design is an improvement of
a proposed design that results in the best properties for
minimum cost. One of the simplest examples is determining
the shape of a fence that will enclose the most area. If the
fence can be any shape, but only a certain amount of fencing
is available, then a circle will enclose the most area with the
given amount of fencing. In order to minimize the amount of
steel used in manufacturing a cylindrical tin can a certain
relationship between the diameter of the can and the height
of the can is found. This will enclose a volume with the least
amount of steel used for the surface area.
5.4 Techniques for stress analysis
Stress Analysis as the name implies, stress analysis is the
complete and comprehensive study of specimen under
consideration. The main objective of stress analysis is to
keep the working stresses within its limits forevaluatingthe
factor for economical design criteria and to improve the
product quality. Material characteristics can be predicted
successfully through stress analysis. The techniques for
stress analysis can be stated as follows
 Analytical techniques
 Experimental techniques
 Numerical Techniques
 Element Used in Finite Element Method
6. MESHING & BOUNDARY CONDITIONS
Steady-state thermal stress analyses are executed to study
the thermal stress effect of on the piston of various
materials. The variations of temperatureandthermal stress
on the piston are investigated for three materials named as
Eutectic Alloy, hyper Eutectic alloy and Special Eutectic
alloy. Thermal stress analyses are performed by using the
general-purpose package software ANSYS, produced by
ANSYS Inc.
6.1 Meshing
Before starting Finite element analysis, other factors must
be determined first. These factors are discussed as follows.
6.1.1 Choice of element
For meshing purpose solid element has been
selected. This type of element is usedtomeshsolidmodel in
ANSYS. These volumes could be created in the ANSYS pre-
processor or imported from a CAD system. Hexahedral
elements (bricks) can be used to mesh regularly shaped
rectangular type volumes, while tetrahedral element can
used to mesh any volume three or four node points in a
plane and experience bending deformation whenloadedby
forces transverse to their surfaces.Therearedifferenttypes
of solid element used in ANSYSfordifferentcondition. Some
of the elements are shown in table
TABLE -2: ELEMENT TYPE FOR STRUCTURAL ANALYSIS
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1314
6.1.2 Discretization of element
In every analysis, very first step is to import geometry to
the ANSYS environment. Discretizethemodel intoelements
and nodes. ANSYS workbench is selected for meshing.
Automatic selection is done in ANSYS workbench in which
solid element is selected. The piston is meshed into
elements count 162329 and nodes 261533. Mesh of piston
as shown in Fig. 1
Fig -1: Meshing of piston
6.2 Boundary Conditions
6.2.1 Frictionless support at Piston Pin location
The small end of connecting rod attaches to the piston pin,
gudgeon pin or wrist pin, which is currently most often
press fit into the connecting rod but can swivel in the
piston, a "floating wrist pin" design. Piston is connected to
the connecting rod with the help of piston pin in such a way
that it allows linear sliding of piston inside the cylinder and
also allows to freely rotate. This boundary condition is
achieved by using Frictionless support at the locationofthe
piston pin as shown in Fig. 2
Fig -2: Frictionless Support
6.2.2 Pressure
Combustion of gases in the combustion chamber exerts
pressure on the head of the pistonduringpowerstroke.The
pressure force will be taken as boundary condition in
structural analysis. Frictionlesssupporthasgivenatsurface
of pin hole. Because the piston will move from TDC to BDC
with the help of fixed support at pin hole. So, whatever the
load is applying on piston due to gas explosion that force
causes to failure of piston pin (inducing bending stresses).
Pressure acting on piston = 3 N/mm2 as shown in Fig.3
Fig -3: Gas Pressure on the head of the piston
6.2.3 Temperature
Along the axis of the piston, the temperature distribution is
symmetrical. The temperature of the piston top surface is
relatively high, especially at the center and the edge of the
combustion chamber, meanwhile the temperature of piston
skirt is relatively low. The maximum surface temperature of
the piston (300oC) appears at the edge of the piston
combustion chamber because the pistontopexperiencesthe
highest thermal load and the edge of combustion chamber is
subjected constantly to high temperature values of gas. The
lowest temperature of the piston is 200oC andappearsat the
bottom of the piston skirt. The lower crankcasetemperature
and the presence of cooling oil also cause this phenomenon.
Fig -4: Temperature value for reference point on piston
7. RESULTS
After applying the complete mechanical load and thermal
load (steady-state temperaturefield),thedistributionofthe
thermo mechanical stress is shown below
7.1 Thermal mechanical coupling stress on the
piston
According to the thermal mechanical coupling analysis
results, it can be seen that the distribution of the thermal
mechanical coupling stress is minimum in Hyper Eutectic
Alloy.
The maximum stress is higher (97.90 MPa) for Eutectic
Alloy (AISi12 CuMgNi) and appears in the pin hole region.
However, this is not likely to cause structural damage or
plastic deformation, since the stress is farlessthantheyield
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1315
limit (230 MPa) of piston material. The piston meets the
strength requirements of the structure.
The maximum stress is medium (94.07 MPa) for Special
Eutectic Alloy (AISi18 CuMgNi) and appears in the pin hole
region. However, this is not likely to cause structural
damage or plastic deformation, since the stress is far less
than the yield limit (280 MPa) of piston material.
The maximum stress is lower (90.78 MPa) for Hyper
Eutectic Alloy (AISi12 Cu4Ni2Mg) and appears in the pin
hole region. However, this is not likely to cause structural
damage or plastic deformation, since the stress is far less
than the yield limit (200 MPa) of piston material.
Fig -5: Thermal mechanical coupling stress on the piston
for Eutectic Material
Fig -6: Thermal mechanical coupling stress on the piston
for Special Eutectic Material
Fig -7: Thermal mechanical coupling stress on the piston
for Hyper Eutectic Material
Eutectic
Hyper
Eutectic
Special
Eutectic
Stress 97.9 90.78 94.07
97.9
90.78
94.07
86
88
90
92
94
96
98
100
EquivalentStress(MPAS)
Thermo-Mechanical
Stress
Stress
Chart -1: Thermal mechanical coupling stress on the
piston
7.2 Thermal mechanical coupling strain on the
piston
According to the thermal mechanical coupling analysis
results, the distribution of the thermal mechanical coupling
strain is minimum in Special Eutectic Alloy.
The maximum strain is higher (1.3396 mm/mm) for
Eutectic Alloy and appears in the pin hole region. However,
this is not likely to cause structural damage or plastic
deformation. The maximum strain is medium (1.249
mm/mm) for special Eutectic Alloy and appears in the pin
hole region. However, this is not likely to cause structural
damage or plastic deformation.
The maximum strain is lower (1.255 mm/mm) for Hyper
Eutectic Alloy and appears in the pin hole region. However,
this is not likely to cause structural damage or plastic
deformation.
Fig -8: Thermal mechanical coupling strain on the piston
for Eutectic Material
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1316
Fig -9: Thermal mechanical coupling strain on the piston
for Special Eutectic Material
Fig -10: Thermal mechanical coupling strain on the piston
for Hyper Eutectic Material
Eutectic
Hyper
Eutectic
Special
Eutectic
Strain 1.339 1.255 1.249
1.339
1.255
1.249
1.2
1.25
1.3
1.35
EquivalentElasticStrain(mm/mm)
Thermo-Mechanical
Strain
Strain
Chart -2: Thermal mechanical coupling strain on the
piston
7.3 Heat Flux on the piston
According to the thermal analysisresults,thedistribution of
the heat flow rate intensity is maximum in Eutectic Alloy.
Fig -11: Heat Flux on the piston for Eutectic material
Fig -12: Heat Flux on the piston for Special Eutectic
material
Fig -13: Heat Flux on the piston for Hyper Eutectic
material
Eutectic
Hyper
Eutectic
Special
Eutectic
Heat Flux 5.3 4.79 4.9
5.3
4.79
4.9
4.4
4.6
4.8
5
5.2
5.4
Heatflux(w/mm2)
Heat Flux on the
Piston
Heat Flux
Chart -3: Heat flux on the piston
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1317
8. CONCLUSION
The thermal stress field only caused by the uneven
temperature distribution was obtained in this study. To
simulate the stress field, the steady-state temperature field
was calculated. In thermal stress analysis, the overall
constraint of the piston is achieved by fixing piston pin,
which is consistent with the actual working condition of the
piston. After all the works that have been done before, the
simulation results of thermal stress are obtained properly.
This thesis tries to put forward a thermal mechanical
decoupling method, which is used to simulate the thermal
stress field only caused by the uneven temperature
distribution when piston works. The basic conclusions are
presented below:
 The temperature distributiononthepistoncrownis
relatively complex; the highest temperature
appears in combustion chamber bottom, while
temperature at the edge of combustion chamber is
quite high too, but no more than the material
allowable range. The temperature on piston ring is
not high, since the external heatdissipatingcapacity
is small leading to small heating load. The overall
temperature of the piston skirt is low and the
thermal load is low as well.
 In this thesis, a new constraint method is proposed
in piston thermal stress analysis. The overall
constraint of the piston is achieved by fixing piston
pin with frictionless support, since the pin can
indirectly constraints the piston by the contact
between them, which is consistent with the actual
working condition of the piston.
 It can be seen that the distribution of the thermal
mechanical coupling stress is minimum in Hyper
Eutectic Alloy. But for Special Eutectic Alloy
(AISi18 CuMgNi) the maximum stress is medium
(94.07 MPa) as compared to other two alloys.
However, this is not likely to cause structural
damage or plastic deformation, since the stress is
far less than the yield limit (280 MPa) of piston
material.
 According to the thermal mechanical coupling
analysis results, the distribution of the thermal
mechanical coupling strain is minimum in Special
Eutectic Alloy.
 The distribution of the heat flow rate intensity is
maximum in Eutectic Alloy. For hyper eutectic
alloy it is 4.9 W/mm2 which is also near to eutectic
alloy.
 Comparing all above points (Point-4 to 6) It is
observed that the Special Eutectic alloy (AISi18
CuMgNi) is best suitable material for the piston.
9. REFRENCES
[1] Dipayan Sinha, Susenjit Sarkar and Samar Chandra
Mandal “Thermo Mechanical Analysis of a Piston with
Different Thermal Barrier Coating Configuration”
International Journal of EngineeringTrendsandTechnology
(IJETT) – Volume 48 Number 6 June 2017
[2] Yaohui Lu, Xing Zhang, Penglin Xiang, Dawei Dong
“Analysis of Thermal TemperatureFieldsandThermal Stress
under Steady Temperature field of Diesel Engine Piston”
Applied Thermal Engineering (2016)
[3] Vaishali R. Nimbarte, Prof. S.D. Khamankar “Stress
Analysis Of Piston Using Pressure Load And Thermal Load”
IPASJ International Journal of Mechanical Engineering
(IIJME) Volume 3, Issue 8, August 2015
[4] Muhammet Cerit*, Mehmet Coban “Temperature and
thermal stress analyses of a ceramic-coated aluminum alloy
piston used in a diesel engine” International Journal of
Thermal Sciences 77 (2014) 11-18
[5] R. Bhagat, Y. M. Jibhakate “Thermal Analysis And
Optimization Of I.C. Engine Piston Using finite Element
Method” International Journal of Modern Engineering
Research (IJMER) Vol.2, Issue.4, July-Aug 2012 pp-2919-
2921

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Design, Thermal Analysis and Optimization of a Piston using Ansys

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1311 DESIGN, THERMAL ANALYSIS AND OPTIMIZATION OF A PISTON USING ANSYS Shahanwaz Adam Havale1, Prof. Santosh Wankhade2 1M.E. Student, Dept. of Mechanical Engineering, Y.T.I.E.T., Maharashtra, India 2 Assistant Professor, Dept. of Mechanical Engineering, Y.T.I.E.T., Maharashtra, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - As the main heating part in the engine, piston works for a long time in high temperature and high load environment. The piston has the characteristics of large heating area and poor heat dissipation, so the thermal load is the most serious problem. This thesis presents a numerical method using thermos-mechanical decoupled FEM (Finite Element Method) to calculate the thermal stress only caused by the uneven temperature distribution. Inthis work, themain emphasis is placed on the study of thermal behavior of functionally graded materials obtained by means of using a commercial code ANSYS on aluminum alloy piston surfaces. The analysis is carried out to reduce the stress concentration on the upper end of the piston i.e. (piston head/crown and piston skirt and sleeve). With using computer-aided design, SolidWorks software the structural model of a piston will be developed. Furthermore, the finite element analysis is done using Computer Aided Simulation software ANSYS. Key Words: Piston, Aluminium Alloy, Stress, Thermos- mechanical decoupled FEM, ANSYS 1. INTRODUCTION Automobile components are in great demand these days because of increased use of automobiles. The increased demand is due to improved performanceandreducedcostof these components. R&D and testing engineers should develop critical components in shortest possible time to minimize launch time for new products. This necessitates understanding of new technologies and quick absorption in the development of new products. A piston is a component of reciprocatingIC-engines. It is the moving component that is contained by a cylinder and is made gas-tight by piston rings. In an engine, its purpose is to transfer force from expanding gas in the cylinder to the crankshaft via a pistonrodand/orconnecting rod. As an important part in an engine, piston endures the cyclic gas pressure and the inertial forces at work, and this working condition may cause the fatigue damage of piston, such as piston side wear, piston head/crown cracks and so on. The investigations indicate that the greatest stress appears on the upper end of the piston and stress concentration is one of the mainly reason for fatigue failure. On the other hand, pistonoverheating-seizurecanonlyoccur when something burns or scrapes away the oil film that exists between the piston and the cylinder wall. 1.1 Problem Statement Based on the literature survey performed, venture into this research is motivated by the fact that Pistons are required to havehighperformancecharacteristicsandbetter precision as they are supposed to sustain high temperature and stresses. Piston skirt may appear deformation at work, which usually causes crack on the upper end of piston head. Due to the deformation, the greatest stress concentration is caused on the upper end of piston, the situation becomes more serious when the stiffness of the piston is not enough, and the crack generally appeared at the point A which may gradually extend and even cause splitting along the piston vertical. The stress distribution on the piston mainly depends on the deformation of piston. Therefore, inorder to reduce the stress concentration, the piston crown should have enough stiffness to reduce the deformation. Exponential analysis of piston is hectic andnotvery precise work. Exact theoretical analysis of piston characteristics is very difficult. With the use of high speed computers and the numerical techniques,the pistonanalysis can be made using CAE. That’s why stress analysis is to be performed using simulation software. Thus, the FEA will be carried out for standard piston model used in diesel engine and optimisation of the same will be carried out. 1.2 Objective The main objective of the presentwork istofindout and suggest optimum material for piston based on quality and economy considering material weight and dimensional issues at the same time. After generating an accurate finite element model, a strategyfor theoptimization workflow was defined. Target of the optimization wastoreachatminimum thermal stresses in the piston. The proposed work included following steps:  Study of literature review of variouswork reported.  The piston is designed according to the procedure and specification which are giveninmachinedesign and data hand books.  CAD model of Piston is created using various tools in SolidWorks.
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1312  FE analysis of the above geometry for different loading and boundary conditions is done as o Gas Pressure at top of the Piston (3MPa) o Temperature at the top of the Piston (200°C- 300°C). o Heat transfer Coefficient (5E-6 W/mm oC.) o Frictionless Supports.  Comparison of the result obtained in above step for different materials.  Choosing the optimum designbasedonthematerial and other parameter. 2. LITERATURE REVIEW Dipayan Sinha, Susenjit Sarkar and Samar Chandra Mandal [1] (June 2017) presented the study of Thermo-Mechanical Analysis of a Piston with Different Thermal Barrier Coating Configuration. In the present work a piston has been analyzed numerically with FEA software named ANSYS Workbench to evaluate its thermos-mechanical capability under a predefined thermal and structural load. To enhance the performance of the engine, weight of the piston has been kept minimum by optimizing different dimensions. Yaohui Lu, Xing Zhang, Penglin Xiang, Dawei Dong [2] (Nov. 2016) presented the study of Analysis of Thermal Temperature Fieldsand Thermal Stress under Steady Temperaturefieldof Diesel Engine Piston. This paper tries to present a new calculation method for the theoretical design of the piston. Vaishali R. Nimbarte, Prof. S.D. Khamankar [3] (Aug 2015) presented the study of stress analysis of piston using pressure load and thermal load. The main objective of this research work is to investigate and analyze the stress distribution of piston atactual engine condition.Inthispaper pressure analysis, thermal analysis and thermo-mechanical analysis is done. The parameter used for the analysis is operating gas pressure, temperatureandmaterialproperties of piston. Muhammet Cerit*, Mehmet Coban [4] (2014) presented the study of Temperature and thermal stress analyses of a ceramic-coated aluminum alloy pistonusedina diesel engine. The goal of this paper is to determine both temperature and thermal stress distributions in a plasmasprayed magnesia-stabilized zirconia coating on an aluminum piston crown to improve the performance of a diesel engine. R. Bhagat, Y. M. Jibhakate [5] (Aug-2012) presented the study of Thermal Analysis and Optimizationof I.C. Engine Piston Using finite Element Method. This paper describes the stress distribution of the seizure on pistonfour stroke engines by using FEA. The finite element analysis is performed by using computer aided design (CAD) software. The main objective is to investigate and analyze the thermal stress distribution of piston at the real engine condition during combustion process. The paper describes the mesh optimization with using finite element analysis technique to predict the higher stress and critical region on the component. 3. ANALYTICAL CALCULATIONS Analytical calculations are done for cast iron piston. For doing analytical calculation material properties and dimensional information should be known and so all the parameters consider for design of piston are calculated by using one analytical problem. 3.1 Procedure for Piston Design The procedure for piston designs consists of the following steps: a. Thickness of piston head ( ) b. Heat flows through the piston head (H) c. Radial thickness of the ring ( ) d. Axial thickness of the ring ( ) e. Width of the top land ( ) f. Width of other ring lands ( ) TABLE -1: DESIGN SPECIFICATION FOR PISTON SR. NO. DESCRIPTION NOTATION UNIT VALUE ARRIVED VALUE USED 1 Length of Piston L Mm -- 75 2 Outside diameter of Piston D Mm -- 84 3 Thickness of Piston Head Mm 7.75 10 4 Radial thickness of the ring Mm 2.84 4 5 Axial thickness of the ring Mm 4 4 6 Maximum Thickness of barrel Mm 11.42 12 7 Width of the top land Mm 12 12 8 Width of other ring lands Mm 4 4 4. MATERIAL SELECTION Pistons are produced from cast or forged, high-temperature resistantaluminumsilicon alloys. Therearethreebasictypes of aluminum piston alloys. The standard piston alloy is a eutectic Al-12%Si alloy containing in addition approx. 1% each of Cu, Ni and Mg. Special eutectic alloys have been developed for improved strength at high temperatures. Hypereutectic alloys with 18 and 24% Si provide lower thermal expansion and wear, but have lower strength (see
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1313 tabled property data on the following pages). In practice, the supplier of aluminum pistons use a wide range of further optimized alloy compositions, but generally based on these basic alloy types. The majority of pistons are produced by gravity die casting. Optimized alloy compositions and a properly controlled solidification conditions allow the production of pistons with low weight and high structural strength. 5. FINITE ELEMENT METHOD 5.1 Introduction Finite ElementMethod(FEM)isa computer-based numerical technique for calculating the Strength and behavior of engineering structures. It can be used to calculatedeflection, stress, vibration, Buckling behavior and many other phenomena. In the finite element method, a structure is broken down into many small simple blocks or elements. The behavior of an individual element can be describedwith a relatively simple set of equations. Just as the set of elements would be joined together to build the whole structure, the equation describing the behaviors of the individual elements are joined into an extremely large set of equations that describe the behavior of the whole structure. The computer can solve this set of simultaneous equations. From the solution, the computer extracts the behaviorofthe individual elements. From this, it can get the stress and deflection of all the parts of the structure. The stresses will be compared to allowed values of stress for the materials to be used, to see if the structure is strong enough. 5.2 Basic steps in FEM  Discretization of the structure  Selection of proper interpolation or displacement model  Derivation of element stiffness matrices and load vectors  Solution for the unknown nodal displacements  Computational of elemental stress and strains 5.3 Optimization using FEA Optimization of an engineering design is an improvement of a proposed design that results in the best properties for minimum cost. One of the simplest examples is determining the shape of a fence that will enclose the most area. If the fence can be any shape, but only a certain amount of fencing is available, then a circle will enclose the most area with the given amount of fencing. In order to minimize the amount of steel used in manufacturing a cylindrical tin can a certain relationship between the diameter of the can and the height of the can is found. This will enclose a volume with the least amount of steel used for the surface area. 5.4 Techniques for stress analysis Stress Analysis as the name implies, stress analysis is the complete and comprehensive study of specimen under consideration. The main objective of stress analysis is to keep the working stresses within its limits forevaluatingthe factor for economical design criteria and to improve the product quality. Material characteristics can be predicted successfully through stress analysis. The techniques for stress analysis can be stated as follows  Analytical techniques  Experimental techniques  Numerical Techniques  Element Used in Finite Element Method 6. MESHING & BOUNDARY CONDITIONS Steady-state thermal stress analyses are executed to study the thermal stress effect of on the piston of various materials. The variations of temperatureandthermal stress on the piston are investigated for three materials named as Eutectic Alloy, hyper Eutectic alloy and Special Eutectic alloy. Thermal stress analyses are performed by using the general-purpose package software ANSYS, produced by ANSYS Inc. 6.1 Meshing Before starting Finite element analysis, other factors must be determined first. These factors are discussed as follows. 6.1.1 Choice of element For meshing purpose solid element has been selected. This type of element is usedtomeshsolidmodel in ANSYS. These volumes could be created in the ANSYS pre- processor or imported from a CAD system. Hexahedral elements (bricks) can be used to mesh regularly shaped rectangular type volumes, while tetrahedral element can used to mesh any volume three or four node points in a plane and experience bending deformation whenloadedby forces transverse to their surfaces.Therearedifferenttypes of solid element used in ANSYSfordifferentcondition. Some of the elements are shown in table TABLE -2: ELEMENT TYPE FOR STRUCTURAL ANALYSIS
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1314 6.1.2 Discretization of element In every analysis, very first step is to import geometry to the ANSYS environment. Discretizethemodel intoelements and nodes. ANSYS workbench is selected for meshing. Automatic selection is done in ANSYS workbench in which solid element is selected. The piston is meshed into elements count 162329 and nodes 261533. Mesh of piston as shown in Fig. 1 Fig -1: Meshing of piston 6.2 Boundary Conditions 6.2.1 Frictionless support at Piston Pin location The small end of connecting rod attaches to the piston pin, gudgeon pin or wrist pin, which is currently most often press fit into the connecting rod but can swivel in the piston, a "floating wrist pin" design. Piston is connected to the connecting rod with the help of piston pin in such a way that it allows linear sliding of piston inside the cylinder and also allows to freely rotate. This boundary condition is achieved by using Frictionless support at the locationofthe piston pin as shown in Fig. 2 Fig -2: Frictionless Support 6.2.2 Pressure Combustion of gases in the combustion chamber exerts pressure on the head of the pistonduringpowerstroke.The pressure force will be taken as boundary condition in structural analysis. Frictionlesssupporthasgivenatsurface of pin hole. Because the piston will move from TDC to BDC with the help of fixed support at pin hole. So, whatever the load is applying on piston due to gas explosion that force causes to failure of piston pin (inducing bending stresses). Pressure acting on piston = 3 N/mm2 as shown in Fig.3 Fig -3: Gas Pressure on the head of the piston 6.2.3 Temperature Along the axis of the piston, the temperature distribution is symmetrical. The temperature of the piston top surface is relatively high, especially at the center and the edge of the combustion chamber, meanwhile the temperature of piston skirt is relatively low. The maximum surface temperature of the piston (300oC) appears at the edge of the piston combustion chamber because the pistontopexperiencesthe highest thermal load and the edge of combustion chamber is subjected constantly to high temperature values of gas. The lowest temperature of the piston is 200oC andappearsat the bottom of the piston skirt. The lower crankcasetemperature and the presence of cooling oil also cause this phenomenon. Fig -4: Temperature value for reference point on piston 7. RESULTS After applying the complete mechanical load and thermal load (steady-state temperaturefield),thedistributionofthe thermo mechanical stress is shown below 7.1 Thermal mechanical coupling stress on the piston According to the thermal mechanical coupling analysis results, it can be seen that the distribution of the thermal mechanical coupling stress is minimum in Hyper Eutectic Alloy. The maximum stress is higher (97.90 MPa) for Eutectic Alloy (AISi12 CuMgNi) and appears in the pin hole region. However, this is not likely to cause structural damage or plastic deformation, since the stress is farlessthantheyield
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1315 limit (230 MPa) of piston material. The piston meets the strength requirements of the structure. The maximum stress is medium (94.07 MPa) for Special Eutectic Alloy (AISi18 CuMgNi) and appears in the pin hole region. However, this is not likely to cause structural damage or plastic deformation, since the stress is far less than the yield limit (280 MPa) of piston material. The maximum stress is lower (90.78 MPa) for Hyper Eutectic Alloy (AISi12 Cu4Ni2Mg) and appears in the pin hole region. However, this is not likely to cause structural damage or plastic deformation, since the stress is far less than the yield limit (200 MPa) of piston material. Fig -5: Thermal mechanical coupling stress on the piston for Eutectic Material Fig -6: Thermal mechanical coupling stress on the piston for Special Eutectic Material Fig -7: Thermal mechanical coupling stress on the piston for Hyper Eutectic Material Eutectic Hyper Eutectic Special Eutectic Stress 97.9 90.78 94.07 97.9 90.78 94.07 86 88 90 92 94 96 98 100 EquivalentStress(MPAS) Thermo-Mechanical Stress Stress Chart -1: Thermal mechanical coupling stress on the piston 7.2 Thermal mechanical coupling strain on the piston According to the thermal mechanical coupling analysis results, the distribution of the thermal mechanical coupling strain is minimum in Special Eutectic Alloy. The maximum strain is higher (1.3396 mm/mm) for Eutectic Alloy and appears in the pin hole region. However, this is not likely to cause structural damage or plastic deformation. The maximum strain is medium (1.249 mm/mm) for special Eutectic Alloy and appears in the pin hole region. However, this is not likely to cause structural damage or plastic deformation. The maximum strain is lower (1.255 mm/mm) for Hyper Eutectic Alloy and appears in the pin hole region. However, this is not likely to cause structural damage or plastic deformation. Fig -8: Thermal mechanical coupling strain on the piston for Eutectic Material
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1316 Fig -9: Thermal mechanical coupling strain on the piston for Special Eutectic Material Fig -10: Thermal mechanical coupling strain on the piston for Hyper Eutectic Material Eutectic Hyper Eutectic Special Eutectic Strain 1.339 1.255 1.249 1.339 1.255 1.249 1.2 1.25 1.3 1.35 EquivalentElasticStrain(mm/mm) Thermo-Mechanical Strain Strain Chart -2: Thermal mechanical coupling strain on the piston 7.3 Heat Flux on the piston According to the thermal analysisresults,thedistribution of the heat flow rate intensity is maximum in Eutectic Alloy. Fig -11: Heat Flux on the piston for Eutectic material Fig -12: Heat Flux on the piston for Special Eutectic material Fig -13: Heat Flux on the piston for Hyper Eutectic material Eutectic Hyper Eutectic Special Eutectic Heat Flux 5.3 4.79 4.9 5.3 4.79 4.9 4.4 4.6 4.8 5 5.2 5.4 Heatflux(w/mm2) Heat Flux on the Piston Heat Flux Chart -3: Heat flux on the piston
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 12 | Dec-2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 6.171 | ISO 9001:2008 Certified Journal | Page 1317 8. CONCLUSION The thermal stress field only caused by the uneven temperature distribution was obtained in this study. To simulate the stress field, the steady-state temperature field was calculated. In thermal stress analysis, the overall constraint of the piston is achieved by fixing piston pin, which is consistent with the actual working condition of the piston. After all the works that have been done before, the simulation results of thermal stress are obtained properly. This thesis tries to put forward a thermal mechanical decoupling method, which is used to simulate the thermal stress field only caused by the uneven temperature distribution when piston works. The basic conclusions are presented below:  The temperature distributiononthepistoncrownis relatively complex; the highest temperature appears in combustion chamber bottom, while temperature at the edge of combustion chamber is quite high too, but no more than the material allowable range. The temperature on piston ring is not high, since the external heatdissipatingcapacity is small leading to small heating load. The overall temperature of the piston skirt is low and the thermal load is low as well.  In this thesis, a new constraint method is proposed in piston thermal stress analysis. The overall constraint of the piston is achieved by fixing piston pin with frictionless support, since the pin can indirectly constraints the piston by the contact between them, which is consistent with the actual working condition of the piston.  It can be seen that the distribution of the thermal mechanical coupling stress is minimum in Hyper Eutectic Alloy. But for Special Eutectic Alloy (AISi18 CuMgNi) the maximum stress is medium (94.07 MPa) as compared to other two alloys. However, this is not likely to cause structural damage or plastic deformation, since the stress is far less than the yield limit (280 MPa) of piston material.  According to the thermal mechanical coupling analysis results, the distribution of the thermal mechanical coupling strain is minimum in Special Eutectic Alloy.  The distribution of the heat flow rate intensity is maximum in Eutectic Alloy. For hyper eutectic alloy it is 4.9 W/mm2 which is also near to eutectic alloy.  Comparing all above points (Point-4 to 6) It is observed that the Special Eutectic alloy (AISi18 CuMgNi) is best suitable material for the piston. 9. REFRENCES [1] Dipayan Sinha, Susenjit Sarkar and Samar Chandra Mandal “Thermo Mechanical Analysis of a Piston with Different Thermal Barrier Coating Configuration” International Journal of EngineeringTrendsandTechnology (IJETT) – Volume 48 Number 6 June 2017 [2] Yaohui Lu, Xing Zhang, Penglin Xiang, Dawei Dong “Analysis of Thermal TemperatureFieldsandThermal Stress under Steady Temperature field of Diesel Engine Piston” Applied Thermal Engineering (2016) [3] Vaishali R. Nimbarte, Prof. S.D. Khamankar “Stress Analysis Of Piston Using Pressure Load And Thermal Load” IPASJ International Journal of Mechanical Engineering (IIJME) Volume 3, Issue 8, August 2015 [4] Muhammet Cerit*, Mehmet Coban “Temperature and thermal stress analyses of a ceramic-coated aluminum alloy piston used in a diesel engine” International Journal of Thermal Sciences 77 (2014) 11-18 [5] R. Bhagat, Y. M. Jibhakate “Thermal Analysis And Optimization Of I.C. Engine Piston Using finite Element Method” International Journal of Modern Engineering Research (IJMER) Vol.2, Issue.4, July-Aug 2012 pp-2919- 2921