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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 58
Design and Validation of Efficient Flywheel Cup of Magneto to Improve
the Thermal Behaviour
Rakesh Narsayya Gundu1, Amol B. Gaikwad2, Atul Jain3, Kharad B.N.4
1Scholar, Dept. of Mechanical Engg, Vishwabharti Academy’s College of Engineering, Ahmednagar, Maharashtra, India
2Asst. Prof. Dept. of Mechanical Engg, Dr. D.Y. Patil School of Engineering, Pune, Maharashtra, India
3General Manager (R&D), Varroc Engineering Limited, Pune, Maharashtra, India
4Asst. Prof. Dept. of Mechanical Engg, Vishwabharti Academy’s College of Engineering, Ahmednagar, Maharashtra, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract – A flywheel magneto is an electromechanical
device for generating AC electric power which is used to drive
electrical loads in vehicles. The flywheel magneto is also
responsible for generating signals for the ignition system of
the vehicle. Flywheel magneto produces heat which makes
thermal behaviour management complicated and very
difficult. All losses from the flywheel magneto are converted
into heat. The most of heat generated in magneto assembly
due to winding copper losses & these losses increase the
winding temperature.
This paper demonstrates the design and validationof
efficient flywheel cupof magnetotoimprovethermalbehavior.
The cup is designed with cooling holes in such a manner that
those holes assist the cooling of the winding. To study the
thermal performance (heat loss dissipation) duetoperipheral
holes, the thermal analysis is performedusingAnsys software.
The CFD analysis is performed for different scenarios, no flow
(no holes on cup), maximum flow through axial holes and
maximum flow through lateral holes aiming on the winding.
CFD results are compared with physical testing results. The
maximum air flow rate with lateral cooling holes condition
indicates lower temperature generation compared to no flow
with no cooling holes and maximum flow with axial holes of
flywheel cup. The lower temperature achieved in copper
winding ensures the winding insulation is not affected due to
excess heat.
Key Words: flywheel magneto, electromechanical, thermal
behaviour, flywheel cup, copper losses, efficiency, Ansys
software, etc.
1. INTRODUCTION
A magneto is an AC power generator used for
generating AC electrical power in automobiles (two, three
wheelers). Magneto is working as per faraday’s law of
electromagnetic induction, which states that when a
conductor is placed in a rotating (changing) magnetic field,
e.m.f. is induced in it. Magneto is used in vehicles for
electrical power generation to drive electrical loads such as:
lighting loads, horn & electrical circuits (Ignition Circuit,
Speedometer Circuits etc.) Apart from electrical power
generation, magneto also generates signals which are used
by the ignition circuit for the spark timing, duration etc. The
signals are also used by the speedometer for engine RPM
display. The magneto is the source of energy generation in
the magneto ignition system. Magneto generates AC
electrical power which will be used to drive electrical loads
in vehicles. The AC power from magneto will be going to the
signal conditioning part which is more popularly known as
regulator. Based on the loads the power is getting processed
in this signal conditioning & power is converted into
Regulated DC, Regulated AC etc. The magneto is also
responsible for generating signals for the ignition circuit.
Magneto has a pulser coil which acts as a magnetic sensor &
senses the position of the rotor with the help of pulser pip
present on the rotor. As this function of the magneto of
signal generation is directly related to the ignition of the
vehicle, the same is very important. The components of
magneto causing the signal generation are tobetreatedvery
much carefully as any defect in these components will make
the engine to stop & the vehicle will not start at all. A
magneto consists of a rotor assembly & a stator assembly as
shown in fig. 1.1. A rotor assy. is a part which will be rotating
with magnets fixed on it which will produce rotating
magnetic field. Stator assy. will be a stationary part with
conductor coils fixed on it. Because of rotating (changing)
magnetic field, e.m.f. is induced in the conductor placed on
the stator.
Fig -1: Flywheel magneto assembly
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 59
1.1 Flywheel Cup
The flywheel cup is a primary component of rotor assy.
which will be used to cover the stator assembly with
magnets as it will be responsible for holding the magnets.
The overall construction can be understood from the figure
shown aside. Along with holding the magnets it also has
pulser pip projected on it which will be responsible for the
signal generation from magneto.
Fig -1.1: Flywheel cup
The cup is going to be application dependent and can have a
different construction; normally the pulser pip can have a
different construction. Even in some cases the pulser pip is
not available on flywheel cup, in such applicationthesame is
present on any other component of the rotor depending
upon the design of the Magneto.
2. PROBLEM DEFINITION
A magneto is an electrical generator that uses
permanent magnets to produce alternating current.
Magnetos that are adapted to produce pulses of high voltage
electricity are used in the ignition systems of some gasoline-
powered internal combustion engines to provide energy to
the spark plugs. However existing flywheel magneto
produces substantial heat especially at high operating
speeds and makes the thermal behaviour management of
these machines difficult and complicated. The temperature
rise in the flywheel magneto leads to damaged insulation,
demagnetization and reduced power output and efficiency.
Power losses could cause an increase in the temperature of
the windings and permanent magnets which reduces the
efficiency of the flywheel magneto. To improve the thermal
behaviour of magneto planned to design new coolingpathof
flywheel cup.
2.1 Objectives of the Project
The current project work aims to achieve the following
objectives:
 Design and optimization of new cooling path.
 To Analyse the thermal behaviour of existing and
proposed design in CFD
 To analyse the temperature difference of existing
and proposed design with experimental
 To compare CFD result with experimental result.
3. DESIGN CALCULATIONS
In flywheel cup design following material selection and
mechanical parameters are considered.
3.1 Material Selection:
Steel sheet/strip hot rolled; pickled & skin passed. Grade.
EDD as per IS: 1079-1994.
3.2 Mechanical Parameters
 Selection of material sheet thickness is 3.2 mm.
 Electrically minimum thicknessis=or>3.2mm.Itis
minimum thickness for flux of flow. (Considering
magnetic flux, material chemical composition-low
carbon percentage, eddy current losses.) Thickness
does not show change in outer diameter (Ø139.4)
under rotation movement at high speed.
 Flywheel cup OD related dimensions not crossing
the limits set by the customer based on the fit &
function of magneto i.e. (Ø70 & 37.5). While
selecting Ø70, bush mating diameter to be
considered.
 Cooling Holes PCD as per customer requirement.
 The direction of piercing always from surface
mating with boss to inner surface of cup.
 Pip position by punching method, projection is not
more than 1/3 of the sheet thickness used for
flywheel cup.
 Pip radius as per customer requirement.
 Selection of size of rivet, rivet PCD & no. of rivets
depends on customer requirement of shear
strength.
 Position of rivet always equal spaced.
 The minimum gap between two holes is 1.5 times
sheet thickness or min sheet thickness.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 60
 Position of magnet and location of spacer ring as
per layout of rotor pole & stator pole alignment at
T.D.C condition.
3.3 Velocity Calculations
Speed – 3000 rpm
Radius of Cup = 0.0697 m
Angular Velocity (ω) = 2 X 3.14 X 3000/60
ω = 314.159 rad/s2
Coolant Velocity (Vc) = ω X Outer radius of cup (r)
Vc = 21.896 m/s
3.4 Proposed Flywheel Cup Design
Fig –3.4: Proposed flywheel cup design
In proposed design lateral cooling holes provided with
combining two different angles as shown in figure3.4.These
holes provided on peripheral side offlywheel cup. Pattern of
holes direction shown in anticlockwise from front view of
cup.
4. FINITE ELEMENT ANALYSIS
In automobile applications on various areas of
interest commonly encountered in engineering include
structural analysis, optical analysis, heat transfer, fluid flow,
mass transport, and electromagnetic potential. Addressed
the problems typically involves solving the geometry
boundary value problems are associated with the partial
differential equations. By formulating theproblems byusing
the finite element method, a system of sum algebraic
equations is obtained as the solution.
4.1 FEA Results
4.1.1 Boundary Conditions
Fig -4.1.1 Boundary Conditions.
4.1.2 Baseline Design
In baseline design no cooling holes providedon flywheel cup
bottom face.
4.1.2.1 Baseline flywheel magneto assy. with no
holes
Fig -4.1.2.1: Thermal behavior of the baseline flywheel
magneto assy. (No Holes) at 3000 RPM, at No flow
Fig - 4.1.2.2: Velocity distribution in baseline magneto
assy. with No cooling holes, at 3000 RPM
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 61
The thermal behavior and velocity distribution in baseline
flywheel magneto assy. (No Holes) at 3000 RPM shown in
figure 4.1.2.1 and 4.1.2.2 In this case maximum temperature
found 170°C & maximum velocity 23.2 m/s observed in
rotation movement because no cooling path provided on
flywheel cup.
4.1.3 Flywheel magneto assy. with Ø12 mm axial
cooling holes
Fig -4.13.1: Thermal behavior of the flywheel magneto
assy. with Ø12 mm cooling holes at 3000 RPM
Fig -4.1.3.2: Velocity distribution in flywheel magneto
assy. with Ø12 mm cooling holes at 3000 RPM
In this case axial holes are provided on bottom face of
flywheel cup. The thermal behavior and velocity distribution
in flywheel magnetoassy.withØ12mmcoolingholesat3000
RPM shown in figure 4.1.3.1and4.1.3.2Inthiscasemaximum
temperature found 140°C and maximum velocity 23.2 m/s
observed because rotating speed is constant & amount of
flow increased as compared to baseline flywheel magneto
assembly without holes.
4.1.4 Proposed Design
In this proposal lateral holes provided on peripheral sides of
flywheel cup.
4.1.4.1 Flywheel magneto assy. with Ø8 mm lateral
cooling holes
Fig -4.1.4.1: Thermal behavior of the flywheel magneto
assy. with Ø8 mm lateral cooling holes at 3000 RPM
Fig 4.1.4.2: Velocity distribution in flywheel magneto
assy. with Ø8 mm lateral cooling holes at 3000 RPM
The minimum temperatureobserved in the proposed design
is 131.68 °C and coolant velocity observed constant is 23.2
m/s max. The air flow circulation improved as compared to
baseline design and trails Ø12 mm axial holes proposal
results.
5. EXPERIMENTAL VALIDATION
For experimental validation proposed flywheel cup with Ø8
mm lateral holes proto sample is manufacturedasperdesign
dimensions and this cup assembled in rotorassembly. Stator
assembly used existing for experimental testing.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 62
5.1 Experimental Procedure for Testing
The experiments are performed using a performance testing
machinemfg. By MEA, where a temperaturetestisconducted
at 3000 RPM. The Performance testing machine provides
results that are compared with the analysis results obtained
from Finite Element Analysis (FEA).
Figure 5.1 displays a picture of the complete experimental
setup and temperature values displayed on the digital
ammeter.
Fig -5.1 Experimental set-up
5.2 Experimental Result Summery
Table 5.2 Experimental result summery
Experimental Sample
Description
Maximum
Temperature at
Winding °C
Baseline flywheel
magneto assy. with no
holes
175
Flywheel magneto assy.
with Ø12 mm axial
cooling holes
140.5
Flywheel magneto assy.
with Ø8 mm lateral
cooling holes
131
Experimental test result shown in table 5.2, in this table
clearly mentioned the maximum temperature shown at
winding.
5.3 Graph of Temperature Variation
5.3 Graph of temperature variation
6. RESULT AND DISCUSSION
The finite element analysis result table shown a
comparison between the baseline, modified design and
proposed design of flywheelmagneto assy. Foranalysing the
results, the following observations can be made:
Table 6.1 FEA And Experimental Result Summery
Description FEA Temp. °C
Experimental
Temp. °C
Baseline flywheel
magneto assy. with
no holes
170 175
Flywheel magneto
assy. with Ø12
mm axial cooling
holes
140 140.5
Flywheel magneto
assy. with Ø8 mm
lateral cooling
holes
131.68 31
The summery table of the finite element analysis (FEA)
results shows that the minimum temperature 131.68 °C
observed in the proposed flywheel magneto assy. with Ø8
mm lateral cooling holes. The Experimental results also
shows that the minimum temperature131°C observedinthe
proposed flywheel magnetoassy. with Ø8 mmlateralcooling
holes.
Both result shows proposed flywheel magneto assy. with Ø8
mm lateral cooling holes are meets the results and found
minimum temperature in copper winding.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072
© 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 63
7. CONCLUSION
The cup is designed with cooling holes in such a manner
that those holes assist the cooling of the winding. To study
the thermal performance (heat loss dissipation) due to
peripheral holes, the thermal analysis is performed using
Ansys software. The CFD analysis is performed for the
different scenarios, no flow (no holesoncup),maximumflow
through axial holes and maximum flow through lateral holes
aiming on the winding. CFD results are compared with
physical testing results. The maximum air flow rate with
lateral cooling holes condition indicates lower temperature
generation compared to no flow with no cooling holes and
maximum flow with axial cooling hole of flywheel cup. The
lower temperature achieved in copper winding ensures the
winding insulation is not affected due to excess heat.
REFERENCES
[1] Wei. Tong, Mechanical Design of Electric Motors, 1st
Edition, CRC Press, Boca Raton, London, 2017.
[2] General Electric, Evaluation and ApplicationofEnergy
Efficient Motors, e- GEA-M1019, Book: GE Industrial
Systems, Fort Wayne, Indiana, 2002.
[3] M. Benhaddadi, G. Olivier, R. Ibtiouen, J. Yelle, J.
Tremblay, Premium Efficiency Motors, Abook chapter
in book: Electric Machines and Drives, Miroslav
Chomat, Intech Open, DOI: 10.5772/14893, 2011.
[4] M. Murugesan, R. Balasubramanian, TheEffectofMass
flow Rate on the Enhanced Heat Transfer
Characteristics in A Corrugated Plate Type Heat
Exchanger,Res. J. Engineering sci., Vol. 1(6), pp 22-26,
2016.
[5] Z. Rehman, K. Seong, Three-D Numerical Thermal
Analysis of Electric Motor with Cooling Jacket,
Energies, 11(1) 92, 2018.
[6] S. Li, Y. Li, W. Choi, and B. Sarlioglu, High-Speed
Electric Machines: Challenges and Design
Considerations, in IEEE Transactions on
Transportation Electrification, 2(1)2-13, March 2016.
[7] J. Schultz, Examining How Cooling Impacts the Torque
and Power of PMAC Motors, Parker Hannifin
Corporation, Electromechanical and Drives Division.
[8] Aswin Inbaraj Jaison A and Karuppasamy K, Design
and Optimization of Flywheel for Automobile
Applications, International Journal of Mechanical
Engineering and Research,ISSN 0973-4562Vol.5No.1
(2015).
[9] Colin Richmond, Ramesh Kuppuswamy, Azeem Khan,
The Effect of Coolant Velocity for Enhancing the High-
Speed Permanent Magnet Generator Efficiency,
Procedia CIRP 91 (2020) 21-26.
[10] Samarth Jain, Kedar Kanase and Phaneesh K,
Improving Electrical Energy Consumption by
Application of Integrated Starter Generator for Single
Cylinder Engine Applications, IJERT,ISSN:2278-0181,
Vol. 9 Issue 03, March-2020.
[11] J. Nithinkumar, D. Gopi Chand and N. Chandra Shekar,
Finite Element Analysis of Sheet Metal WorksforDeep
Drawing in Manufacturing of Fly Wheel Cup, IJERT,
ISSN 2278-0181, Vol. 3 Issue 9, September 2014.
[12] Jan Szczypior and Rafal Jakubowski, Thermal
Calculations and Testing of External Rotor Permanent
Magnet Machine, Technical Transactions, Electrical
Engineering, DOI 10.4467/235337XCT.15.058.3858,
2015.

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Design and Validation of Efficient Flywheel Cup of Magneto to Improve the Thermal Behaviour

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 58 Design and Validation of Efficient Flywheel Cup of Magneto to Improve the Thermal Behaviour Rakesh Narsayya Gundu1, Amol B. Gaikwad2, Atul Jain3, Kharad B.N.4 1Scholar, Dept. of Mechanical Engg, Vishwabharti Academy’s College of Engineering, Ahmednagar, Maharashtra, India 2Asst. Prof. Dept. of Mechanical Engg, Dr. D.Y. Patil School of Engineering, Pune, Maharashtra, India 3General Manager (R&D), Varroc Engineering Limited, Pune, Maharashtra, India 4Asst. Prof. Dept. of Mechanical Engg, Vishwabharti Academy’s College of Engineering, Ahmednagar, Maharashtra, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract – A flywheel magneto is an electromechanical device for generating AC electric power which is used to drive electrical loads in vehicles. The flywheel magneto is also responsible for generating signals for the ignition system of the vehicle. Flywheel magneto produces heat which makes thermal behaviour management complicated and very difficult. All losses from the flywheel magneto are converted into heat. The most of heat generated in magneto assembly due to winding copper losses & these losses increase the winding temperature. This paper demonstrates the design and validationof efficient flywheel cupof magnetotoimprovethermalbehavior. The cup is designed with cooling holes in such a manner that those holes assist the cooling of the winding. To study the thermal performance (heat loss dissipation) duetoperipheral holes, the thermal analysis is performedusingAnsys software. The CFD analysis is performed for different scenarios, no flow (no holes on cup), maximum flow through axial holes and maximum flow through lateral holes aiming on the winding. CFD results are compared with physical testing results. The maximum air flow rate with lateral cooling holes condition indicates lower temperature generation compared to no flow with no cooling holes and maximum flow with axial holes of flywheel cup. The lower temperature achieved in copper winding ensures the winding insulation is not affected due to excess heat. Key Words: flywheel magneto, electromechanical, thermal behaviour, flywheel cup, copper losses, efficiency, Ansys software, etc. 1. INTRODUCTION A magneto is an AC power generator used for generating AC electrical power in automobiles (two, three wheelers). Magneto is working as per faraday’s law of electromagnetic induction, which states that when a conductor is placed in a rotating (changing) magnetic field, e.m.f. is induced in it. Magneto is used in vehicles for electrical power generation to drive electrical loads such as: lighting loads, horn & electrical circuits (Ignition Circuit, Speedometer Circuits etc.) Apart from electrical power generation, magneto also generates signals which are used by the ignition circuit for the spark timing, duration etc. The signals are also used by the speedometer for engine RPM display. The magneto is the source of energy generation in the magneto ignition system. Magneto generates AC electrical power which will be used to drive electrical loads in vehicles. The AC power from magneto will be going to the signal conditioning part which is more popularly known as regulator. Based on the loads the power is getting processed in this signal conditioning & power is converted into Regulated DC, Regulated AC etc. The magneto is also responsible for generating signals for the ignition circuit. Magneto has a pulser coil which acts as a magnetic sensor & senses the position of the rotor with the help of pulser pip present on the rotor. As this function of the magneto of signal generation is directly related to the ignition of the vehicle, the same is very important. The components of magneto causing the signal generation are tobetreatedvery much carefully as any defect in these components will make the engine to stop & the vehicle will not start at all. A magneto consists of a rotor assembly & a stator assembly as shown in fig. 1.1. A rotor assy. is a part which will be rotating with magnets fixed on it which will produce rotating magnetic field. Stator assy. will be a stationary part with conductor coils fixed on it. Because of rotating (changing) magnetic field, e.m.f. is induced in the conductor placed on the stator. Fig -1: Flywheel magneto assembly
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 59 1.1 Flywheel Cup The flywheel cup is a primary component of rotor assy. which will be used to cover the stator assembly with magnets as it will be responsible for holding the magnets. The overall construction can be understood from the figure shown aside. Along with holding the magnets it also has pulser pip projected on it which will be responsible for the signal generation from magneto. Fig -1.1: Flywheel cup The cup is going to be application dependent and can have a different construction; normally the pulser pip can have a different construction. Even in some cases the pulser pip is not available on flywheel cup, in such applicationthesame is present on any other component of the rotor depending upon the design of the Magneto. 2. PROBLEM DEFINITION A magneto is an electrical generator that uses permanent magnets to produce alternating current. Magnetos that are adapted to produce pulses of high voltage electricity are used in the ignition systems of some gasoline- powered internal combustion engines to provide energy to the spark plugs. However existing flywheel magneto produces substantial heat especially at high operating speeds and makes the thermal behaviour management of these machines difficult and complicated. The temperature rise in the flywheel magneto leads to damaged insulation, demagnetization and reduced power output and efficiency. Power losses could cause an increase in the temperature of the windings and permanent magnets which reduces the efficiency of the flywheel magneto. To improve the thermal behaviour of magneto planned to design new coolingpathof flywheel cup. 2.1 Objectives of the Project The current project work aims to achieve the following objectives:  Design and optimization of new cooling path.  To Analyse the thermal behaviour of existing and proposed design in CFD  To analyse the temperature difference of existing and proposed design with experimental  To compare CFD result with experimental result. 3. DESIGN CALCULATIONS In flywheel cup design following material selection and mechanical parameters are considered. 3.1 Material Selection: Steel sheet/strip hot rolled; pickled & skin passed. Grade. EDD as per IS: 1079-1994. 3.2 Mechanical Parameters  Selection of material sheet thickness is 3.2 mm.  Electrically minimum thicknessis=or>3.2mm.Itis minimum thickness for flux of flow. (Considering magnetic flux, material chemical composition-low carbon percentage, eddy current losses.) Thickness does not show change in outer diameter (Ø139.4) under rotation movement at high speed.  Flywheel cup OD related dimensions not crossing the limits set by the customer based on the fit & function of magneto i.e. (Ø70 & 37.5). While selecting Ø70, bush mating diameter to be considered.  Cooling Holes PCD as per customer requirement.  The direction of piercing always from surface mating with boss to inner surface of cup.  Pip position by punching method, projection is not more than 1/3 of the sheet thickness used for flywheel cup.  Pip radius as per customer requirement.  Selection of size of rivet, rivet PCD & no. of rivets depends on customer requirement of shear strength.  Position of rivet always equal spaced.  The minimum gap between two holes is 1.5 times sheet thickness or min sheet thickness.
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 60  Position of magnet and location of spacer ring as per layout of rotor pole & stator pole alignment at T.D.C condition. 3.3 Velocity Calculations Speed – 3000 rpm Radius of Cup = 0.0697 m Angular Velocity (ω) = 2 X 3.14 X 3000/60 ω = 314.159 rad/s2 Coolant Velocity (Vc) = ω X Outer radius of cup (r) Vc = 21.896 m/s 3.4 Proposed Flywheel Cup Design Fig –3.4: Proposed flywheel cup design In proposed design lateral cooling holes provided with combining two different angles as shown in figure3.4.These holes provided on peripheral side offlywheel cup. Pattern of holes direction shown in anticlockwise from front view of cup. 4. FINITE ELEMENT ANALYSIS In automobile applications on various areas of interest commonly encountered in engineering include structural analysis, optical analysis, heat transfer, fluid flow, mass transport, and electromagnetic potential. Addressed the problems typically involves solving the geometry boundary value problems are associated with the partial differential equations. By formulating theproblems byusing the finite element method, a system of sum algebraic equations is obtained as the solution. 4.1 FEA Results 4.1.1 Boundary Conditions Fig -4.1.1 Boundary Conditions. 4.1.2 Baseline Design In baseline design no cooling holes providedon flywheel cup bottom face. 4.1.2.1 Baseline flywheel magneto assy. with no holes Fig -4.1.2.1: Thermal behavior of the baseline flywheel magneto assy. (No Holes) at 3000 RPM, at No flow Fig - 4.1.2.2: Velocity distribution in baseline magneto assy. with No cooling holes, at 3000 RPM
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 61 The thermal behavior and velocity distribution in baseline flywheel magneto assy. (No Holes) at 3000 RPM shown in figure 4.1.2.1 and 4.1.2.2 In this case maximum temperature found 170°C & maximum velocity 23.2 m/s observed in rotation movement because no cooling path provided on flywheel cup. 4.1.3 Flywheel magneto assy. with Ø12 mm axial cooling holes Fig -4.13.1: Thermal behavior of the flywheel magneto assy. with Ø12 mm cooling holes at 3000 RPM Fig -4.1.3.2: Velocity distribution in flywheel magneto assy. with Ø12 mm cooling holes at 3000 RPM In this case axial holes are provided on bottom face of flywheel cup. The thermal behavior and velocity distribution in flywheel magnetoassy.withØ12mmcoolingholesat3000 RPM shown in figure 4.1.3.1and4.1.3.2Inthiscasemaximum temperature found 140°C and maximum velocity 23.2 m/s observed because rotating speed is constant & amount of flow increased as compared to baseline flywheel magneto assembly without holes. 4.1.4 Proposed Design In this proposal lateral holes provided on peripheral sides of flywheel cup. 4.1.4.1 Flywheel magneto assy. with Ø8 mm lateral cooling holes Fig -4.1.4.1: Thermal behavior of the flywheel magneto assy. with Ø8 mm lateral cooling holes at 3000 RPM Fig 4.1.4.2: Velocity distribution in flywheel magneto assy. with Ø8 mm lateral cooling holes at 3000 RPM The minimum temperatureobserved in the proposed design is 131.68 °C and coolant velocity observed constant is 23.2 m/s max. The air flow circulation improved as compared to baseline design and trails Ø12 mm axial holes proposal results. 5. EXPERIMENTAL VALIDATION For experimental validation proposed flywheel cup with Ø8 mm lateral holes proto sample is manufacturedasperdesign dimensions and this cup assembled in rotorassembly. Stator assembly used existing for experimental testing.
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 62 5.1 Experimental Procedure for Testing The experiments are performed using a performance testing machinemfg. By MEA, where a temperaturetestisconducted at 3000 RPM. The Performance testing machine provides results that are compared with the analysis results obtained from Finite Element Analysis (FEA). Figure 5.1 displays a picture of the complete experimental setup and temperature values displayed on the digital ammeter. Fig -5.1 Experimental set-up 5.2 Experimental Result Summery Table 5.2 Experimental result summery Experimental Sample Description Maximum Temperature at Winding °C Baseline flywheel magneto assy. with no holes 175 Flywheel magneto assy. with Ø12 mm axial cooling holes 140.5 Flywheel magneto assy. with Ø8 mm lateral cooling holes 131 Experimental test result shown in table 5.2, in this table clearly mentioned the maximum temperature shown at winding. 5.3 Graph of Temperature Variation 5.3 Graph of temperature variation 6. RESULT AND DISCUSSION The finite element analysis result table shown a comparison between the baseline, modified design and proposed design of flywheelmagneto assy. Foranalysing the results, the following observations can be made: Table 6.1 FEA And Experimental Result Summery Description FEA Temp. °C Experimental Temp. °C Baseline flywheel magneto assy. with no holes 170 175 Flywheel magneto assy. with Ø12 mm axial cooling holes 140 140.5 Flywheel magneto assy. with Ø8 mm lateral cooling holes 131.68 31 The summery table of the finite element analysis (FEA) results shows that the minimum temperature 131.68 °C observed in the proposed flywheel magneto assy. with Ø8 mm lateral cooling holes. The Experimental results also shows that the minimum temperature131°C observedinthe proposed flywheel magnetoassy. with Ø8 mmlateralcooling holes. Both result shows proposed flywheel magneto assy. with Ø8 mm lateral cooling holes are meets the results and found minimum temperature in copper winding.
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 10 Issue: 06 | Jun 2023 www.irjet.net p-ISSN: 2395-0072 © 2023, IRJET | Impact Factor value: 8.226 | ISO 9001:2008 Certified Journal | Page 63 7. CONCLUSION The cup is designed with cooling holes in such a manner that those holes assist the cooling of the winding. To study the thermal performance (heat loss dissipation) due to peripheral holes, the thermal analysis is performed using Ansys software. The CFD analysis is performed for the different scenarios, no flow (no holesoncup),maximumflow through axial holes and maximum flow through lateral holes aiming on the winding. CFD results are compared with physical testing results. The maximum air flow rate with lateral cooling holes condition indicates lower temperature generation compared to no flow with no cooling holes and maximum flow with axial cooling hole of flywheel cup. The lower temperature achieved in copper winding ensures the winding insulation is not affected due to excess heat. REFERENCES [1] Wei. Tong, Mechanical Design of Electric Motors, 1st Edition, CRC Press, Boca Raton, London, 2017. [2] General Electric, Evaluation and ApplicationofEnergy Efficient Motors, e- GEA-M1019, Book: GE Industrial Systems, Fort Wayne, Indiana, 2002. [3] M. Benhaddadi, G. Olivier, R. Ibtiouen, J. Yelle, J. Tremblay, Premium Efficiency Motors, Abook chapter in book: Electric Machines and Drives, Miroslav Chomat, Intech Open, DOI: 10.5772/14893, 2011. [4] M. Murugesan, R. Balasubramanian, TheEffectofMass flow Rate on the Enhanced Heat Transfer Characteristics in A Corrugated Plate Type Heat Exchanger,Res. J. Engineering sci., Vol. 1(6), pp 22-26, 2016. [5] Z. Rehman, K. Seong, Three-D Numerical Thermal Analysis of Electric Motor with Cooling Jacket, Energies, 11(1) 92, 2018. [6] S. Li, Y. Li, W. Choi, and B. Sarlioglu, High-Speed Electric Machines: Challenges and Design Considerations, in IEEE Transactions on Transportation Electrification, 2(1)2-13, March 2016. [7] J. Schultz, Examining How Cooling Impacts the Torque and Power of PMAC Motors, Parker Hannifin Corporation, Electromechanical and Drives Division. [8] Aswin Inbaraj Jaison A and Karuppasamy K, Design and Optimization of Flywheel for Automobile Applications, International Journal of Mechanical Engineering and Research,ISSN 0973-4562Vol.5No.1 (2015). [9] Colin Richmond, Ramesh Kuppuswamy, Azeem Khan, The Effect of Coolant Velocity for Enhancing the High- Speed Permanent Magnet Generator Efficiency, Procedia CIRP 91 (2020) 21-26. [10] Samarth Jain, Kedar Kanase and Phaneesh K, Improving Electrical Energy Consumption by Application of Integrated Starter Generator for Single Cylinder Engine Applications, IJERT,ISSN:2278-0181, Vol. 9 Issue 03, March-2020. [11] J. Nithinkumar, D. Gopi Chand and N. Chandra Shekar, Finite Element Analysis of Sheet Metal WorksforDeep Drawing in Manufacturing of Fly Wheel Cup, IJERT, ISSN 2278-0181, Vol. 3 Issue 9, September 2014. [12] Jan Szczypior and Rafal Jakubowski, Thermal Calculations and Testing of External Rotor Permanent Magnet Machine, Technical Transactions, Electrical Engineering, DOI 10.4467/235337XCT.15.058.3858, 2015.