SlideShare a Scribd company logo
Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com 
ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 
www.ijera.com 4 | P a g e 
Design Analysis and Optimization of Internal Combustion Engine Piston using CAE tool ANSYS Aditya Kumar Gupta 1 , Vinay Kumar Tripathi 2 1Scholar of Master of Technology , Mechanical Engineering Department ,UCER , Allahabad 2Asst. Professor , Mechanical Engineering Department, UCER, Allahabad Abstract In the internal combustion engine there are many reciprocating parts which are responsible for giving the motion to the engine. from them the piston is very important part of the internal combustion engine.. The working condition of the piston is so worst in comparison of other parts of the internal combustion engine. There is very high probability to failure of the piston due to high wear and tear. So there is necessary to inspection the working condition of piston. In before there is no availability of software packages. So there is difficult to check out the failure of the piston, it is also very time taken process. In now days the software packages are used to consume less time and give quality assurance. In this study work there are two steps of analysis of the piston they are Designing and Analysis. Firstly design the model of the piston in giving design specification on the modelling software like INVENTOR . Then giving it the constraints which are act on the working condition of the piston after import the model of the piston into the analysis software ANSYS in IGES format. Then the analysis become completed on the different parameters(temperature, stress, deformation) and easily analysis the result. In this work the piston become optimized after the reducing the material of the piston. the mass and volume of the piston become reduced. The deformation also increased after the optimization which is responsible for the stress distribution on the piston head or piston crown. Keywords: Piston , INVENTOR, ANSYS 
I. Introduction 
Piston is a most important component of an internal combustion engine. Its working condition is so worst. It is very important to calculate the piston temperature distribution in order to control the thermal stresses and deformation. In the working condition piston produce the stress and deformation due to periodic load effect which produce from high gas pressure, high speed reciprocating motion of the inertia force and lateral pressure. By the chemical reaction of burning the gas the high temperature generates which make the piston expand which creates thermal stress and thermal deformation. The thermal deformation and mechanical deformation causes piston cracks, tortuosity etc. Therefore it is very essential to check out or analyze the stress distribution, temperature distribution, heat transfer, thermal load, mechanical load in order to minimize the stress, minimize the thermal stress and different loads on working condition of the piston. Most of the internal combustion engine piston is made of Al alloy which have thermal coefficient is 80% higher than the cylinder bore material made of cast iron. This creates difference between the running and design clearances. Therefore it is very necessary to examine the crucial thermal behaviour of the piston. In this study firstly make the virtual piston on real working environment by the modelling software INVENTOR and finally analysis the piston giving boundary constraints by ANSYS. The present work has been based on the following objectives- 
1. To design an IC engine piston using INVENTOR. 
2. To perform the structural and thermal analysis of piston using ANSYS 13.0. 
II. Piston 
Piston is considered as a very important part of a reciprocating engine in which it helps to convert the chemical energy after the burning of fuel into mechanical energy. The purpose of the piston is to help in conveying the gasses to crankshaft via connecting rod without loss of gas. The piston ring is used to provide seal between the cylinder and piston. It must able to work with low friction, high explosive forces and high temperature around 2000℃ to 2800℃.The piston is to be strong but its weight should be less to prevent inertia forces due to reciprocating motion. 
RESEARCH ARTICLE OPEN ACCESS
Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com 
ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 
www.ijera.com 5 | P a g e 
III. Functions of Piston 
 To receive the thrust force generated by the 
chemical reaction of fuel in the cylinder and 
transmits to connecting rod. 
 To reciprocate in the cylinder provide seal in 
suction, compression, expansion and exhaust 
stroke. 
IV. Piston Materials 
Generally pistons are made of Al alloy and cast 
iron. But the Al alloy is more preferable in 
comparison of cast iron because of its light weight 
which suitable for the reciprocating part. There are 
some drawbacks of Al alloys in comparison to cast 
iron that are the Al alloys are less in strength and in 
wearing qualities. The heat conductivity of Al is 
about of thrice of the cast iron. Al pistons are made 
thicker which is necessary for strength in order to 
give proper cooling. 
V. Design consideration for a Piston 
In designing a piston, the following points should be 
taken into consideration: 
1. It should have enormous strength to 
withstand the high gas pressure and inertia 
forces. 
2. It should have minimum mass to minimise 
the inertia forces. 
3. It should form an effective gas and oil 
sealing of the cylinder. 
4. It should provide sufficient bearing area to 
prevent undue wear. 
5. It should disperse the heat of combustion 
quickly to the cylinder walls. 
6. It should have high speed reciprocation 
without noise. 
7. It should be of sufficient rigid construction 
to withstand thermal and mechanical 
distortion. 
8. It should have sufficient support for the 
piston pin. 
Procedure for design of Piston 
The procedures of the piston design are 
1. The thickness of the piston head (tH) 
2. Heat flow through the piston head(H) 
3. Radial thickness of the ring(t1) 
4. Axial thickness of the ring(t2) 
5. Width of the top land(b1) 
6. Width of the other land(b2) 
The explanations of the above steps are 
Thickness of the Piston (tH) 
tH = 
2 3 
16 t 
pD 
 
Where p= maximum gas pressure(2MPa) 
D= Bore diameter (mm) 
σt= Permissible stress(90MPa) 
Heat flow through the piston head (H) 
H= 12.56×tH×K×(Tc-Te) 
Where K=thermal conductivity 
Tc=Temperature at the centre of the piston 
head in℃ 
Te=Temperature at edges of piston in℃ 
Radial thickness of Ring (t1) 
t1=D 
3 w 
t 
p 
 
Where pw= Pressure of fuel on cylinder 
wall(0.025N/mm2-0.042N/mm2) 
Axial thickness of Ring (t2) 
t2 = 0.7t1 to t1 
or 
t2= 
10 r 
D 
 n 
Where nr= number of rings 
Width of the top land (b1) 
b1= tH to 1.2 tH 
Width of the other land (b2) 
b2= 0.7t2 to t2 
Maximum thickness of barrel (t3) 
t3=0.03×D+t1+4.9 
Designing specification for Piston: 
S. No. Parameters Values 
1 
Length (L) 
158mm 
2 
Bore Diameter(D) 
120mm 
3 
Pressure(p) 
2MPa 
4 
Permissible stress(휎푡 ) 
90MPa 
5 
Gas pressure(pw) 
0.25MPa
Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com 
ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 
www.ijera.com 6 | P a g e 
Material properties of Piston 
Material of Piston 
Young's Modulus (M Pa) 
Poission's Ratio 
Bulk Modulus (M Pa) 
Shear Modulus (M Pa) 
Density (Kgmm-3) 
Coefficient of thermal expansion (℃-1) 
Al alloy 
71000 
0.33 
69608 
26692 
2.77×10-6 
2.3×10-5 
Designing of Piston The piston is designed by giving the dimensions into the modelling software INVENTOR. The geometry of the piston is designed in INVENTOR is imported to the analysis software in the IGES format. The figure of the designed piston is below- 
Fig.1. Design of Piston Analysis of Piston The piston is analyzed by giving the constraints they are 1. Pressure 2. Select the material properties, 3. Fine meshing, 4. Initial Temperature 5. Convection Temperature
Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com 
ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 
www.ijera.com 7 | P a g e 
Fig.2. Applied Pressure Fig.3. Fixed supports 5. Fixed the piston pin, 6. Film coefficient:-9.56×10-3W/mm2K After giving the constraints the analysis become goes on into the mechanical APDL in ANSYS software. 
VI. Result and Discussion 
1.Before optimization When the constraints are given to the design of the piston and analysis is done then the result are come out by which we analysis the piston working condition. The some results are given below 1.1 Temperature distribution The temperature distribution of piston is very important to check the effect of temperature is maximum on which part of piston. After the analysis of temperature distribution the result comes out that the maximum temperature is on the piston head and the minimum temperature is on the piston skirt. The temperature distribution of the piston is given below. 
Fig.4. Temperature distribution
Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com 
ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 
www.ijera.com 8 | P a g e 
1.2 Total Deflection 
The deformation of the piston is essential to know the resistance of the piston material on working condition. 
The deformation occurred into piston is 0.25483mm.The deformation in the piston is given below 
Fig.5. Total Deformation 
1.3 Equivalent stress (Von- Mises) 
Von mises stress is important to calculate the factor of safety by which we decide that design is safe. The 
maximum Von-mises stress is 81.636MPa. The Von-Mises stress is become less than the permissible stress. In 
this permissible stress is 90MPa for the Al alloy. By this the design is safe because factor of safety is greater 
than 1. It is very important to calculate to design the piston that the design is safe or not. 
Fig.6. Von -Mises stress 
Optimization 
Optimization is technique to improve the design specifications. There are some constraints which are consider 
for optimization of piston they are 
1. Maximum Von mises stress<Allowable stress
Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com 
ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 
www.ijera.com 9 | P a g e 
2. Factor of safety>1 
3. Deflection 
2. After Optimization The changes after optimization are discussed by the following results 2.1 Deflection after optimization After the optimization the deflection becomes 0.2687mm from 0.25483mm.By this the resistance from pressure applied to piston become increase. The chances of failure decrease by the optimization process. 
Fig.7.Deflection after optimization 2.2 Von-Mises stress after optimization The Von-mises stress becomes 87.875MPa from 81.636MPa after optimization. 
Fig.8.Von-Mises stress after optimization Design values after optimization Parameter after the analysis of piston after optimization on working environment the results are 
S. No. 
Parameter 
Before Optimization 
After Optimization 
Design Consideration 
1 
Volume 
904370mm3 
863980mm3 
863980mm3 
2 
Mass 
2.5051 kg 
2.3932 kg 
2.3932 kg 
3 
Length 
158mm 
158mm 
158mm 
4 
Bore Diameter 
120mm 
120mm 
120mm 
5 
Deflection 
0.25483mm 
0.2687mm 
0.2687mm 
6 
Von-Mises Stress 
81.636MPa 
87.875MPa 
87.875MPa 
7 
Factor of Safety 
1.102 
1.02 
1.02
Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com 
ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 
www.ijera.com 10 | P a g e 
VII. Conclusion 
Concluded from above study and analysis by using INVENTOR and ANSYS software the deflection due to pressure applied to the piston become increased after optimization. This is taken for the design consideration for the design of piston. The stress induced in the piston is mainly formed due to the deformation of piston. Therefore the stress reduction is very important factor which is responsible for the designing of pistol crown or piston head. In this work the main consideration is to optimize the piston with reduction of piston weight. The material of the piston becomes reduced. Then the optimized result of the piston obtained. The design become consider as safe when Von-Mises stress is less than the permissible stress. The factor of safety becomes greater than one then the design become safe. The factor of safety after optimization is 1.02 obtained. The permissible stress induced in the piston is about 81.636Mpa to 87.875MPa. References 
[1.] Ekeren Buyukkaya, Muhammet Cerit, Thermal analysis of a ceramic coating diesel using 3-D finite method, Surface & coating Technology 202 (2007) 398-402. 
[2.] Ekeren Buyukkaya, Thermal analysis of functionally graded coating AlSi alloy and steel pistons, Surface & Coatings Technology 202 (2008) 3856–3865. 
[3.] Al-Beiruti, Dr.Basim M. Al Quraishi & Isam Ezzulddinyousif, Thermal effects on Diesel Engine Piston and Piston Compression Rings, Eng. & Tech .Journal Vol. 27, 2009 
[4.] Shuoguo Zhao, Design the piston of Internal Combustion Engine by PROENGEER,EMEIT-2012, 
[5.] A.R. Bhagat, Y.M. Jibhakate, Thermal Analysis and Optimization of I.C. Engine Piston Using Finite Element Method, IJMER,Vol.2, July 2012, 2919-2921 
[6.] Ch. Venkata Rajan ,P.V.K. Murthy, M.V.S. Muraly Krishna, G.M. Prasada Rao, Design Analysis and Optimization Of Piston using CATIA and ANSYS, International Journal of Innovative Research in Engineering & Science Vol.1 , January 2013 
[7.] Swati S Chougule, Vinayak H Khatawate, Piston Strength Analysis Using FEM, IJERA,Vol.3, March 2013 
[8.] CH Venkata Rajan, P.V.K. Murthy ,M.V.S. Muraly Krishna, Linear Static Structural Analysis of Optimized Piston For Bio-Fuel Using ANSYS, IJMPERD, Vol.3, June 2013 
[9.] Kesarapu Sandeep Reddy, K.R. Senthil Kumar, P R Jeyakrishnam , Study on 
Stability of Honeycomb Structured Piston, IJERA,Vol.3, Sep.2013 
[10.] Isam Jasim Jaber and Ajeet Kumar Rai, Design and Analysis of IC Engine Piston and Piston-Ring Using CATIA and ANSYS Software, IJMET, Vol.5, 2014

More Related Content

What's hot

Engine Block/ Cylinder Block
Engine Block/ Cylinder BlockEngine Block/ Cylinder Block
Engine Block/ Cylinder BlockAbu Sufyan Malik
 
FAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEA
FAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEAFAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEA
FAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEAIjripublishers Ijri
 
Automotive engine valve recession (engineering research series)
Automotive engine valve recession (engineering research series)Automotive engine valve recession (engineering research series)
Automotive engine valve recession (engineering research series)Arul Gnana John
 
THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...
THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...
THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...Ijripublishers Ijri
 
IRJET- Analysis of Drum Brake Review Article
IRJET- Analysis of Drum Brake Review ArticleIRJET- Analysis of Drum Brake Review Article
IRJET- Analysis of Drum Brake Review ArticleIRJET Journal
 
Thermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel Engine
Thermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel EngineThermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel Engine
Thermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel EngineDr. Amarjeet Singh
 
THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...
THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...
THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...Ijripublishers Ijri
 
FAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSIS
FAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSISFAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSIS
FAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSISIAEME Publication
 
fatigue failure analysis of steam turbine shaft using fem technique
 fatigue failure analysis of steam turbine shaft using fem technique fatigue failure analysis of steam turbine shaft using fem technique
fatigue failure analysis of steam turbine shaft using fem techniqueIjripublishers Ijri
 
MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)
MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)
MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)Vision Solutions
 
structural and modal analysis of an engine block by varying materials
 structural and modal analysis of an engine block by varying materials structural and modal analysis of an engine block by varying materials
structural and modal analysis of an engine block by varying materialsIjripublishers Ijri
 
Design, Thermal Analysis and Optimization of a Piston using Ansys
Design, Thermal Analysis and Optimization of a Piston using AnsysDesign, Thermal Analysis and Optimization of a Piston using Ansys
Design, Thermal Analysis and Optimization of a Piston using AnsysIRJET Journal
 
IRJET- Analysis of Engine Fin Body by Varying Geometry & Materials
IRJET-  	  Analysis of Engine Fin Body by Varying Geometry & MaterialsIRJET-  	  Analysis of Engine Fin Body by Varying Geometry & Materials
IRJET- Analysis of Engine Fin Body by Varying Geometry & MaterialsIRJET Journal
 
Effect of air swirl with dimpled cylinder
Effect of air swirl with dimpled cylinderEffect of air swirl with dimpled cylinder
Effect of air swirl with dimpled cylinderprj_publication
 

What's hot (20)

Engine Block/ Cylinder Block
Engine Block/ Cylinder BlockEngine Block/ Cylinder Block
Engine Block/ Cylinder Block
 
Piston design
Piston designPiston design
Piston design
 
FAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEA
FAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEAFAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEA
FAILURE ANALYSIS OF IC ENGINE VALVES BY USING FEA
 
Piston Design
Piston DesignPiston Design
Piston Design
 
R4805114117
R4805114117R4805114117
R4805114117
 
Automotive engine valve recession (engineering research series)
Automotive engine valve recession (engineering research series)Automotive engine valve recession (engineering research series)
Automotive engine valve recession (engineering research series)
 
THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...
THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...
THERMAL ANALYSIS OF INTERNAL COMBUSTION DIESEL ENGINE EXHAUST VALVE FOR THE E...
 
IRJET- Analysis of Drum Brake Review Article
IRJET- Analysis of Drum Brake Review ArticleIRJET- Analysis of Drum Brake Review Article
IRJET- Analysis of Drum Brake Review Article
 
Thermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel Engine
Thermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel EngineThermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel Engine
Thermo Structural Analysis on Cylinder Head of 4 Stroke VCR Diesel Engine
 
THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...
THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...
THERMAL INVESTIGATION (PRESSURE DISTRIBUTION) ON BOX TYPE CYLINDER HEAD OF A ...
 
FAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSIS
FAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSISFAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSIS
FAILURE ANALYSIS OF GAS TURBINE BLADE USING FINITE ELEMENT ANALYSIS
 
30120140503010
3012014050301030120140503010
30120140503010
 
fatigue failure analysis of steam turbine shaft using fem technique
 fatigue failure analysis of steam turbine shaft using fem technique fatigue failure analysis of steam turbine shaft using fem technique
fatigue failure analysis of steam turbine shaft using fem technique
 
[IJET V2I3-1P3] Authors:G.Siva Prasad K.Dinesh Achari E.Dileep Kumar Goud M.N...
[IJET V2I3-1P3] Authors:G.Siva Prasad K.Dinesh Achari E.Dileep Kumar Goud M.N...[IJET V2I3-1P3] Authors:G.Siva Prasad K.Dinesh Achari E.Dileep Kumar Goud M.N...
[IJET V2I3-1P3] Authors:G.Siva Prasad K.Dinesh Achari E.Dileep Kumar Goud M.N...
 
MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)
MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)
MECHANICAL PROJECT LIST (UNIGRAPHICS & HEPERMESH & CATIA)
 
structural and modal analysis of an engine block by varying materials
 structural and modal analysis of an engine block by varying materials structural and modal analysis of an engine block by varying materials
structural and modal analysis of an engine block by varying materials
 
Design, Thermal Analysis and Optimization of a Piston using Ansys
Design, Thermal Analysis and Optimization of a Piston using AnsysDesign, Thermal Analysis and Optimization of a Piston using Ansys
Design, Thermal Analysis and Optimization of a Piston using Ansys
 
IRJET- Analysis of Engine Fin Body by Varying Geometry & Materials
IRJET-  	  Analysis of Engine Fin Body by Varying Geometry & MaterialsIRJET-  	  Analysis of Engine Fin Body by Varying Geometry & Materials
IRJET- Analysis of Engine Fin Body by Varying Geometry & Materials
 
Effect of air swirl with dimpled cylinder
Effect of air swirl with dimpled cylinderEffect of air swirl with dimpled cylinder
Effect of air swirl with dimpled cylinder
 
30120140507014
3012014050701430120140507014
30120140507014
 

Similar to Design Analysis and Optimization of Internal Combustion Engine Piston using CAE tool ANSYS

IRJET- Static and Thermal Analysis of Piston with Different Thermal Coatings
IRJET- Static and Thermal Analysis of Piston with Different Thermal CoatingsIRJET- Static and Thermal Analysis of Piston with Different Thermal Coatings
IRJET- Static and Thermal Analysis of Piston with Different Thermal CoatingsIRJET Journal
 
Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...
Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...
Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...IRJET Journal
 
Transient state thermal analysis of a 4 stroke CI engine Piston
Transient state thermal analysis of a 4 stroke CI engine PistonTransient state thermal analysis of a 4 stroke CI engine Piston
Transient state thermal analysis of a 4 stroke CI engine PistonIRJET Journal
 
IRJET- A Review on I. C. Engine Head Fins Design
IRJET- A Review on I. C. Engine Head Fins DesignIRJET- A Review on I. C. Engine Head Fins Design
IRJET- A Review on I. C. Engine Head Fins DesignIRJET Journal
 
Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYS
	Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYS	Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYS
Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYSinventionjournals
 
Modeling and Analysis of Gas Turbine Rotor Blade
Modeling and Analysis of Gas Turbine Rotor BladeModeling and Analysis of Gas Turbine Rotor Blade
Modeling and Analysis of Gas Turbine Rotor BladeIRJET Journal
 
IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...
IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...
IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...IRJET Journal
 
Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...
Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...
Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...IJSRD
 
MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...
MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...
MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...Ijripublishers Ijri
 
IRJET - Design and Analysis of Connecting Rod using Different Materials
IRJET - Design and Analysis of Connecting Rod using Different MaterialsIRJET - Design and Analysis of Connecting Rod using Different Materials
IRJET - Design and Analysis of Connecting Rod using Different MaterialsIRJET Journal
 
Investigation of Heat Transfer Through Fins Using Fem
Investigation of Heat Transfer Through Fins Using FemInvestigation of Heat Transfer Through Fins Using Fem
Investigation of Heat Transfer Through Fins Using FemIJERA Editor
 
IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...
IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...
IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...IRJET Journal
 
DESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALS
DESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALSDESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALS
DESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALSIRJET Journal
 
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine VaneIRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine VaneIRJET Journal
 
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET-  	  Design and Analysis of Ceramic(Sic) Gas Turbine VaneIRJET-  	  Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine VaneIRJET Journal
 
Paper id 21201487
Paper id 21201487Paper id 21201487
Paper id 21201487IJRAT
 
Modeling and Stress Analysis of Gas Turbine Rotor
Modeling and Stress Analysis of Gas Turbine RotorModeling and Stress Analysis of Gas Turbine Rotor
Modeling and Stress Analysis of Gas Turbine RotorIRJET Journal
 

Similar to Design Analysis and Optimization of Internal Combustion Engine Piston using CAE tool ANSYS (20)

IRJET- Static and Thermal Analysis of Piston with Different Thermal Coatings
IRJET- Static and Thermal Analysis of Piston with Different Thermal CoatingsIRJET- Static and Thermal Analysis of Piston with Different Thermal Coatings
IRJET- Static and Thermal Analysis of Piston with Different Thermal Coatings
 
Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...
Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...
Thermal Barrier Coating on IC Engine Piston to Enhance Better Utilization of ...
 
Transient state thermal analysis of a 4 stroke CI engine Piston
Transient state thermal analysis of a 4 stroke CI engine PistonTransient state thermal analysis of a 4 stroke CI engine Piston
Transient state thermal analysis of a 4 stroke CI engine Piston
 
IRJET- A Review on I. C. Engine Head Fins Design
IRJET- A Review on I. C. Engine Head Fins DesignIRJET- A Review on I. C. Engine Head Fins Design
IRJET- A Review on I. C. Engine Head Fins Design
 
Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYS
	Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYS	Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYS
Theoretical Analysis of Stress and Design of Piston Head using CATIA & ANSYS
 
P410394102
P410394102P410394102
P410394102
 
Modeling and Analysis of Gas Turbine Rotor Blade
Modeling and Analysis of Gas Turbine Rotor BladeModeling and Analysis of Gas Turbine Rotor Blade
Modeling and Analysis of Gas Turbine Rotor Blade
 
IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...
IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...
IRJET- Single Stop Transient Thermal Coupled with Structural Analysis and Rep...
 
D1302032028
D1302032028D1302032028
D1302032028
 
Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...
Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...
Thermal and Structural Analysis Using Fea on Pillar Vains Type Ventilated Dis...
 
MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...
MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...
MULTI CAVITY DIE PREPARATION, ANALYSIS AND MANUFACTURING PROCESS OF DIESEL EN...
 
IRJET - Design and Analysis of Connecting Rod using Different Materials
IRJET - Design and Analysis of Connecting Rod using Different MaterialsIRJET - Design and Analysis of Connecting Rod using Different Materials
IRJET - Design and Analysis of Connecting Rod using Different Materials
 
Investigation of Heat Transfer Through Fins Using Fem
Investigation of Heat Transfer Through Fins Using FemInvestigation of Heat Transfer Through Fins Using Fem
Investigation of Heat Transfer Through Fins Using Fem
 
IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...
IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...
IRJET-Design and Fatigue Life Estimation of Diesel Engine Piston using Ansys ...
 
DESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALS
DESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALSDESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALS
DESIGN AND ANALYSIS OF PISTON USING VARIOUS MATERIALS
 
30120140502008
3012014050200830120140502008
30120140502008
 
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine VaneIRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
 
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET-  	  Design and Analysis of Ceramic(Sic) Gas Turbine VaneIRJET-  	  Design and Analysis of Ceramic(Sic) Gas Turbine Vane
IRJET- Design and Analysis of Ceramic(Sic) Gas Turbine Vane
 
Paper id 21201487
Paper id 21201487Paper id 21201487
Paper id 21201487
 
Modeling and Stress Analysis of Gas Turbine Rotor
Modeling and Stress Analysis of Gas Turbine RotorModeling and Stress Analysis of Gas Turbine Rotor
Modeling and Stress Analysis of Gas Turbine Rotor
 

Recently uploaded

Scaling in conventional MOSFET for constant electric field and constant voltage
Scaling in conventional MOSFET for constant electric field and constant voltageScaling in conventional MOSFET for constant electric field and constant voltage
Scaling in conventional MOSFET for constant electric field and constant voltageRCC Institute of Information Technology
 
Antenna efficency lecture course chapter 3.pdf
Antenna  efficency lecture course chapter 3.pdfAntenna  efficency lecture course chapter 3.pdf
Antenna efficency lecture course chapter 3.pdfAbrahamGadissa
 
Toll tax management system project report..pdf
Toll tax management system project report..pdfToll tax management system project report..pdf
Toll tax management system project report..pdfKamal Acharya
 
Laundry management system project report.pdf
Laundry management system project report.pdfLaundry management system project report.pdf
Laundry management system project report.pdfKamal Acharya
 
Cloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptx
Cloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptxCloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptx
Cloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptxMd. Shahidul Islam Prodhan
 
Architectural Portfolio Sean Lockwood
Architectural Portfolio Sean LockwoodArchitectural Portfolio Sean Lockwood
Architectural Portfolio Sean Lockwoodseandesed
 
Quality defects in TMT Bars, Possible causes and Potential Solutions.
Quality defects in TMT Bars, Possible causes and Potential Solutions.Quality defects in TMT Bars, Possible causes and Potential Solutions.
Quality defects in TMT Bars, Possible causes and Potential Solutions.PrashantGoswami42
 
Digital Signal Processing Lecture notes n.pdf
Digital Signal Processing Lecture notes n.pdfDigital Signal Processing Lecture notes n.pdf
Digital Signal Processing Lecture notes n.pdfAbrahamGadissa
 
ASME IX(9) 2007 Full Version .pdf
ASME IX(9)  2007 Full Version       .pdfASME IX(9)  2007 Full Version       .pdf
ASME IX(9) 2007 Full Version .pdfAhmedHussein950959
 
WATER CRISIS and its solutions-pptx 1234
WATER CRISIS and its solutions-pptx 1234WATER CRISIS and its solutions-pptx 1234
WATER CRISIS and its solutions-pptx 1234AafreenAbuthahir2
 
ENERGY STORAGE DEVICES INTRODUCTION UNIT-I
ENERGY STORAGE DEVICES  INTRODUCTION UNIT-IENERGY STORAGE DEVICES  INTRODUCTION UNIT-I
ENERGY STORAGE DEVICES INTRODUCTION UNIT-IVigneshvaranMech
 
CME397 Surface Engineering- Professional Elective
CME397 Surface Engineering- Professional ElectiveCME397 Surface Engineering- Professional Elective
CME397 Surface Engineering- Professional Electivekarthi keyan
 
shape functions of 1D and 2 D rectangular elements.pptx
shape functions of 1D and 2 D rectangular elements.pptxshape functions of 1D and 2 D rectangular elements.pptx
shape functions of 1D and 2 D rectangular elements.pptxVishalDeshpande27
 
İTÜ CAD and Reverse Engineering Workshop
İTÜ CAD and Reverse Engineering WorkshopİTÜ CAD and Reverse Engineering Workshop
İTÜ CAD and Reverse Engineering WorkshopEmre Günaydın
 
Hall booking system project report .pdf
Hall booking system project report  .pdfHall booking system project report  .pdf
Hall booking system project report .pdfKamal Acharya
 
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Dr.Costas Sachpazis
 
Event Management System Vb Net Project Report.pdf
Event Management System Vb Net  Project Report.pdfEvent Management System Vb Net  Project Report.pdf
Event Management System Vb Net Project Report.pdfKamal Acharya
 
Danfoss NeoCharge Technology -A Revolution in 2024.pdf
Danfoss NeoCharge Technology -A Revolution in 2024.pdfDanfoss NeoCharge Technology -A Revolution in 2024.pdf
Danfoss NeoCharge Technology -A Revolution in 2024.pdfNurvisNavarroSanchez
 

Recently uploaded (20)

Scaling in conventional MOSFET for constant electric field and constant voltage
Scaling in conventional MOSFET for constant electric field and constant voltageScaling in conventional MOSFET for constant electric field and constant voltage
Scaling in conventional MOSFET for constant electric field and constant voltage
 
Antenna efficency lecture course chapter 3.pdf
Antenna  efficency lecture course chapter 3.pdfAntenna  efficency lecture course chapter 3.pdf
Antenna efficency lecture course chapter 3.pdf
 
Toll tax management system project report..pdf
Toll tax management system project report..pdfToll tax management system project report..pdf
Toll tax management system project report..pdf
 
Laundry management system project report.pdf
Laundry management system project report.pdfLaundry management system project report.pdf
Laundry management system project report.pdf
 
Cloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptx
Cloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptxCloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptx
Cloud-Computing_CSE311_Computer-Networking CSE GUB BD - Shahidul.pptx
 
Architectural Portfolio Sean Lockwood
Architectural Portfolio Sean LockwoodArchitectural Portfolio Sean Lockwood
Architectural Portfolio Sean Lockwood
 
Standard Reomte Control Interface - Neometrix
Standard Reomte Control Interface - NeometrixStandard Reomte Control Interface - Neometrix
Standard Reomte Control Interface - Neometrix
 
Quality defects in TMT Bars, Possible causes and Potential Solutions.
Quality defects in TMT Bars, Possible causes and Potential Solutions.Quality defects in TMT Bars, Possible causes and Potential Solutions.
Quality defects in TMT Bars, Possible causes and Potential Solutions.
 
Digital Signal Processing Lecture notes n.pdf
Digital Signal Processing Lecture notes n.pdfDigital Signal Processing Lecture notes n.pdf
Digital Signal Processing Lecture notes n.pdf
 
ASME IX(9) 2007 Full Version .pdf
ASME IX(9)  2007 Full Version       .pdfASME IX(9)  2007 Full Version       .pdf
ASME IX(9) 2007 Full Version .pdf
 
WATER CRISIS and its solutions-pptx 1234
WATER CRISIS and its solutions-pptx 1234WATER CRISIS and its solutions-pptx 1234
WATER CRISIS and its solutions-pptx 1234
 
ENERGY STORAGE DEVICES INTRODUCTION UNIT-I
ENERGY STORAGE DEVICES  INTRODUCTION UNIT-IENERGY STORAGE DEVICES  INTRODUCTION UNIT-I
ENERGY STORAGE DEVICES INTRODUCTION UNIT-I
 
CME397 Surface Engineering- Professional Elective
CME397 Surface Engineering- Professional ElectiveCME397 Surface Engineering- Professional Elective
CME397 Surface Engineering- Professional Elective
 
shape functions of 1D and 2 D rectangular elements.pptx
shape functions of 1D and 2 D rectangular elements.pptxshape functions of 1D and 2 D rectangular elements.pptx
shape functions of 1D and 2 D rectangular elements.pptx
 
İTÜ CAD and Reverse Engineering Workshop
İTÜ CAD and Reverse Engineering WorkshopİTÜ CAD and Reverse Engineering Workshop
İTÜ CAD and Reverse Engineering Workshop
 
Hall booking system project report .pdf
Hall booking system project report  .pdfHall booking system project report  .pdf
Hall booking system project report .pdf
 
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...
Sachpazis:Terzaghi Bearing Capacity Estimation in simple terms with Calculati...
 
Water Industry Process Automation and Control Monthly - May 2024.pdf
Water Industry Process Automation and Control Monthly - May 2024.pdfWater Industry Process Automation and Control Monthly - May 2024.pdf
Water Industry Process Automation and Control Monthly - May 2024.pdf
 
Event Management System Vb Net Project Report.pdf
Event Management System Vb Net  Project Report.pdfEvent Management System Vb Net  Project Report.pdf
Event Management System Vb Net Project Report.pdf
 
Danfoss NeoCharge Technology -A Revolution in 2024.pdf
Danfoss NeoCharge Technology -A Revolution in 2024.pdfDanfoss NeoCharge Technology -A Revolution in 2024.pdf
Danfoss NeoCharge Technology -A Revolution in 2024.pdf
 

Design Analysis and Optimization of Internal Combustion Engine Piston using CAE tool ANSYS

  • 1. Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 www.ijera.com 4 | P a g e Design Analysis and Optimization of Internal Combustion Engine Piston using CAE tool ANSYS Aditya Kumar Gupta 1 , Vinay Kumar Tripathi 2 1Scholar of Master of Technology , Mechanical Engineering Department ,UCER , Allahabad 2Asst. Professor , Mechanical Engineering Department, UCER, Allahabad Abstract In the internal combustion engine there are many reciprocating parts which are responsible for giving the motion to the engine. from them the piston is very important part of the internal combustion engine.. The working condition of the piston is so worst in comparison of other parts of the internal combustion engine. There is very high probability to failure of the piston due to high wear and tear. So there is necessary to inspection the working condition of piston. In before there is no availability of software packages. So there is difficult to check out the failure of the piston, it is also very time taken process. In now days the software packages are used to consume less time and give quality assurance. In this study work there are two steps of analysis of the piston they are Designing and Analysis. Firstly design the model of the piston in giving design specification on the modelling software like INVENTOR . Then giving it the constraints which are act on the working condition of the piston after import the model of the piston into the analysis software ANSYS in IGES format. Then the analysis become completed on the different parameters(temperature, stress, deformation) and easily analysis the result. In this work the piston become optimized after the reducing the material of the piston. the mass and volume of the piston become reduced. The deformation also increased after the optimization which is responsible for the stress distribution on the piston head or piston crown. Keywords: Piston , INVENTOR, ANSYS I. Introduction Piston is a most important component of an internal combustion engine. Its working condition is so worst. It is very important to calculate the piston temperature distribution in order to control the thermal stresses and deformation. In the working condition piston produce the stress and deformation due to periodic load effect which produce from high gas pressure, high speed reciprocating motion of the inertia force and lateral pressure. By the chemical reaction of burning the gas the high temperature generates which make the piston expand which creates thermal stress and thermal deformation. The thermal deformation and mechanical deformation causes piston cracks, tortuosity etc. Therefore it is very essential to check out or analyze the stress distribution, temperature distribution, heat transfer, thermal load, mechanical load in order to minimize the stress, minimize the thermal stress and different loads on working condition of the piston. Most of the internal combustion engine piston is made of Al alloy which have thermal coefficient is 80% higher than the cylinder bore material made of cast iron. This creates difference between the running and design clearances. Therefore it is very necessary to examine the crucial thermal behaviour of the piston. In this study firstly make the virtual piston on real working environment by the modelling software INVENTOR and finally analysis the piston giving boundary constraints by ANSYS. The present work has been based on the following objectives- 1. To design an IC engine piston using INVENTOR. 2. To perform the structural and thermal analysis of piston using ANSYS 13.0. II. Piston Piston is considered as a very important part of a reciprocating engine in which it helps to convert the chemical energy after the burning of fuel into mechanical energy. The purpose of the piston is to help in conveying the gasses to crankshaft via connecting rod without loss of gas. The piston ring is used to provide seal between the cylinder and piston. It must able to work with low friction, high explosive forces and high temperature around 2000℃ to 2800℃.The piston is to be strong but its weight should be less to prevent inertia forces due to reciprocating motion. RESEARCH ARTICLE OPEN ACCESS
  • 2. Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 www.ijera.com 5 | P a g e III. Functions of Piston  To receive the thrust force generated by the chemical reaction of fuel in the cylinder and transmits to connecting rod.  To reciprocate in the cylinder provide seal in suction, compression, expansion and exhaust stroke. IV. Piston Materials Generally pistons are made of Al alloy and cast iron. But the Al alloy is more preferable in comparison of cast iron because of its light weight which suitable for the reciprocating part. There are some drawbacks of Al alloys in comparison to cast iron that are the Al alloys are less in strength and in wearing qualities. The heat conductivity of Al is about of thrice of the cast iron. Al pistons are made thicker which is necessary for strength in order to give proper cooling. V. Design consideration for a Piston In designing a piston, the following points should be taken into consideration: 1. It should have enormous strength to withstand the high gas pressure and inertia forces. 2. It should have minimum mass to minimise the inertia forces. 3. It should form an effective gas and oil sealing of the cylinder. 4. It should provide sufficient bearing area to prevent undue wear. 5. It should disperse the heat of combustion quickly to the cylinder walls. 6. It should have high speed reciprocation without noise. 7. It should be of sufficient rigid construction to withstand thermal and mechanical distortion. 8. It should have sufficient support for the piston pin. Procedure for design of Piston The procedures of the piston design are 1. The thickness of the piston head (tH) 2. Heat flow through the piston head(H) 3. Radial thickness of the ring(t1) 4. Axial thickness of the ring(t2) 5. Width of the top land(b1) 6. Width of the other land(b2) The explanations of the above steps are Thickness of the Piston (tH) tH = 2 3 16 t pD  Where p= maximum gas pressure(2MPa) D= Bore diameter (mm) σt= Permissible stress(90MPa) Heat flow through the piston head (H) H= 12.56×tH×K×(Tc-Te) Where K=thermal conductivity Tc=Temperature at the centre of the piston head in℃ Te=Temperature at edges of piston in℃ Radial thickness of Ring (t1) t1=D 3 w t p  Where pw= Pressure of fuel on cylinder wall(0.025N/mm2-0.042N/mm2) Axial thickness of Ring (t2) t2 = 0.7t1 to t1 or t2= 10 r D  n Where nr= number of rings Width of the top land (b1) b1= tH to 1.2 tH Width of the other land (b2) b2= 0.7t2 to t2 Maximum thickness of barrel (t3) t3=0.03×D+t1+4.9 Designing specification for Piston: S. No. Parameters Values 1 Length (L) 158mm 2 Bore Diameter(D) 120mm 3 Pressure(p) 2MPa 4 Permissible stress(휎푡 ) 90MPa 5 Gas pressure(pw) 0.25MPa
  • 3. Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 www.ijera.com 6 | P a g e Material properties of Piston Material of Piston Young's Modulus (M Pa) Poission's Ratio Bulk Modulus (M Pa) Shear Modulus (M Pa) Density (Kgmm-3) Coefficient of thermal expansion (℃-1) Al alloy 71000 0.33 69608 26692 2.77×10-6 2.3×10-5 Designing of Piston The piston is designed by giving the dimensions into the modelling software INVENTOR. The geometry of the piston is designed in INVENTOR is imported to the analysis software in the IGES format. The figure of the designed piston is below- Fig.1. Design of Piston Analysis of Piston The piston is analyzed by giving the constraints they are 1. Pressure 2. Select the material properties, 3. Fine meshing, 4. Initial Temperature 5. Convection Temperature
  • 4. Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 www.ijera.com 7 | P a g e Fig.2. Applied Pressure Fig.3. Fixed supports 5. Fixed the piston pin, 6. Film coefficient:-9.56×10-3W/mm2K After giving the constraints the analysis become goes on into the mechanical APDL in ANSYS software. VI. Result and Discussion 1.Before optimization When the constraints are given to the design of the piston and analysis is done then the result are come out by which we analysis the piston working condition. The some results are given below 1.1 Temperature distribution The temperature distribution of piston is very important to check the effect of temperature is maximum on which part of piston. After the analysis of temperature distribution the result comes out that the maximum temperature is on the piston head and the minimum temperature is on the piston skirt. The temperature distribution of the piston is given below. Fig.4. Temperature distribution
  • 5. Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 www.ijera.com 8 | P a g e 1.2 Total Deflection The deformation of the piston is essential to know the resistance of the piston material on working condition. The deformation occurred into piston is 0.25483mm.The deformation in the piston is given below Fig.5. Total Deformation 1.3 Equivalent stress (Von- Mises) Von mises stress is important to calculate the factor of safety by which we decide that design is safe. The maximum Von-mises stress is 81.636MPa. The Von-Mises stress is become less than the permissible stress. In this permissible stress is 90MPa for the Al alloy. By this the design is safe because factor of safety is greater than 1. It is very important to calculate to design the piston that the design is safe or not. Fig.6. Von -Mises stress Optimization Optimization is technique to improve the design specifications. There are some constraints which are consider for optimization of piston they are 1. Maximum Von mises stress<Allowable stress
  • 6. Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 www.ijera.com 9 | P a g e 2. Factor of safety>1 3. Deflection 2. After Optimization The changes after optimization are discussed by the following results 2.1 Deflection after optimization After the optimization the deflection becomes 0.2687mm from 0.25483mm.By this the resistance from pressure applied to piston become increase. The chances of failure decrease by the optimization process. Fig.7.Deflection after optimization 2.2 Von-Mises stress after optimization The Von-mises stress becomes 87.875MPa from 81.636MPa after optimization. Fig.8.Von-Mises stress after optimization Design values after optimization Parameter after the analysis of piston after optimization on working environment the results are S. No. Parameter Before Optimization After Optimization Design Consideration 1 Volume 904370mm3 863980mm3 863980mm3 2 Mass 2.5051 kg 2.3932 kg 2.3932 kg 3 Length 158mm 158mm 158mm 4 Bore Diameter 120mm 120mm 120mm 5 Deflection 0.25483mm 0.2687mm 0.2687mm 6 Von-Mises Stress 81.636MPa 87.875MPa 87.875MPa 7 Factor of Safety 1.102 1.02 1.02
  • 7. Aditya Kumar Gupta Int. Journal of Engineering Research and Applications www.ijera.com ISSN : 2248-9622, Vol. 4, Issue 11(Version - 5), November 2014, pp.04-10 www.ijera.com 10 | P a g e VII. Conclusion Concluded from above study and analysis by using INVENTOR and ANSYS software the deflection due to pressure applied to the piston become increased after optimization. This is taken for the design consideration for the design of piston. The stress induced in the piston is mainly formed due to the deformation of piston. Therefore the stress reduction is very important factor which is responsible for the designing of pistol crown or piston head. In this work the main consideration is to optimize the piston with reduction of piston weight. The material of the piston becomes reduced. Then the optimized result of the piston obtained. The design become consider as safe when Von-Mises stress is less than the permissible stress. The factor of safety becomes greater than one then the design become safe. The factor of safety after optimization is 1.02 obtained. The permissible stress induced in the piston is about 81.636Mpa to 87.875MPa. References [1.] Ekeren Buyukkaya, Muhammet Cerit, Thermal analysis of a ceramic coating diesel using 3-D finite method, Surface & coating Technology 202 (2007) 398-402. [2.] Ekeren Buyukkaya, Thermal analysis of functionally graded coating AlSi alloy and steel pistons, Surface & Coatings Technology 202 (2008) 3856–3865. [3.] Al-Beiruti, Dr.Basim M. Al Quraishi & Isam Ezzulddinyousif, Thermal effects on Diesel Engine Piston and Piston Compression Rings, Eng. & Tech .Journal Vol. 27, 2009 [4.] Shuoguo Zhao, Design the piston of Internal Combustion Engine by PROENGEER,EMEIT-2012, [5.] A.R. Bhagat, Y.M. Jibhakate, Thermal Analysis and Optimization of I.C. Engine Piston Using Finite Element Method, IJMER,Vol.2, July 2012, 2919-2921 [6.] Ch. Venkata Rajan ,P.V.K. Murthy, M.V.S. Muraly Krishna, G.M. Prasada Rao, Design Analysis and Optimization Of Piston using CATIA and ANSYS, International Journal of Innovative Research in Engineering & Science Vol.1 , January 2013 [7.] Swati S Chougule, Vinayak H Khatawate, Piston Strength Analysis Using FEM, IJERA,Vol.3, March 2013 [8.] CH Venkata Rajan, P.V.K. Murthy ,M.V.S. Muraly Krishna, Linear Static Structural Analysis of Optimized Piston For Bio-Fuel Using ANSYS, IJMPERD, Vol.3, June 2013 [9.] Kesarapu Sandeep Reddy, K.R. Senthil Kumar, P R Jeyakrishnam , Study on Stability of Honeycomb Structured Piston, IJERA,Vol.3, Sep.2013 [10.] Isam Jasim Jaber and Ajeet Kumar Rai, Design and Analysis of IC Engine Piston and Piston-Ring Using CATIA and ANSYS Software, IJMET, Vol.5, 2014