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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 331
“Design and development of better alternatives to shrink fit achieved
by induction heating in rotor shaft assembly of the hermetically sealed
reciprocating compressor”
Nandini Chavan1, Dr .M. S. Kale 2
Student, Mechanical Engineering Department, Government College Of Engineering, Karad, Maharashtra India.
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - In rotorshaft assembly of hermetically sealed reciprocating compressor, there is interferencefitbetweenrotorand
shaft. To obtain this interference fit various methods are used. Without the use of extra mechanical fastening systems,
interference-fitted joints are an efficient and cost-effective way to assemble components. An interface pressure is established
during assembly by press-fitting or a shrink-fitting assembly process as a result of a dimensional misfit between the two parts,
which is frequently in a shaft and rotor. Because of frictional resistance, the joint is able to withstand axial forces and torques.
The traditional method for achievinga shrink fit between the rotorand shaft is induction heating. Thisprocessrequiresheating
equipment and higher energy consumption,thiswillincreasethemanufacturingcostofthecompressor.Duetothelimitationsof
induction heating process, there is a need to identify and design an alternative options for achieving shrink fit in rotor shaft
assembly in cost effective manner yet ensuring the desired quality. This paper presents the study of current and proposed
assembly procedureused to get rotor-shaft assembly in hermeticallysealedreciprocatingcompressor.Inthisstudy,factorsthat
affect an interference-fitted joints' abilitytofunctionproperlyaregroupedunderafewgeneralheadings,including:coefficientof
friction, coefficient of thermal expansion, surfaces, the geometry,frictionalforce,torque,tangentialforce,materials,loading,and
lastly the assembly method utilized to create the joint between the rotor and shaft.
Keywords: Interference fit, , rotorshaftassembly,shrinkfitting,inductionheating,radialorinterfacepressure,torque,
frictional force, tangential force.
1. INTRODUCTION:
In rotorshaft assembly of thehermetically sealed reciprocatingcompressor,toachieveaninterferencefitbetweenrotorand
shaft, shrink fitting techniques are generally used. Shrink fitting typically refers to techniques that utilize the phenomena of
thermal contraction and expansion to produce an interference fit. The most common method for doing this is to heat the outer
component, causing it to expand thermally. Then two parts fit together easily. An incredibly tight joint forms around the inner
part when the outer part cools to room temperature and contracts back to its original size. Typically, metals will expand in
response to heating. So induction heating is generally used to obtain shrink fit in rotor shaft assembly. In existing induction
heating process rotoris heated from outsidesurface and then heat istransferredfromoutsidetoinsidesurfaceofrotortoobtain
thermal expansion of rotor bore. After expansion, rotor is shrink fitted into the shaft. But this process requires higher power
consumption and hence increases the manufacturing costof the compressor.Soheatingfromtheinsidesurfaceoftherotorbore
is the alternative option to achieve shrink fit in rotor shaft assembly.
2. Rotor Shaft Assembly:
Figure 1.Dimensions of rotor and shaft interference fit prior to assembling
dA = Outside diameter of shaft
dM = Inside diameter of rotor
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 332
d = Diametric interference
Figure shows the dimensions of rotor and shaft interference fit prior to assembling.Interferencefitisalsoknownaspress fitor
friction fit, is a fastening method where two parts, typically circular cross section shape, are pushed together (one into the
other) and kept in place due to the pressure between them. Typically, theinnerpartwill havea nominal outerdiameterslightly
greater than the nominal inner diameter of the outer part, and when pushed or forced together thecontactfrictionforceskeep
the parts from moving relative to each other. Thelevel ofinterferencedependsonthe negativedifferenceinnominal diameters.
Shrink Fit Process
Obtaining shrink fit by heating from the inside surface of the rotor bore:
The only viable way to heat the rotor is using an inductioncoil from the insidesurfaceoftheoftherotorbore,thisheatallowsfor
better energy delivery to the assembly. In this method heating will beonlylocalheating.Aninductioncoilcanbeusedtoheatthe
rotor bore. The coil is inserted into the rotor bore and power is applied for certain time to reach the required temperature for
heating the rotor bore and tried to expand the rotor bore and placed onto the shaft. This process consumes less power as
compared to heating from the outside surface of rotor.
Theoretical modelling of Thermal expansion:
Table 1: Dimensions and material properties of aluminium rotor
Diameter increase of rotor bore when being heated or Thermal expansion of rotor bore is calculated as:
Δd = doαΔT
Where,
Δd = change in diameter of rotor bore or thermal expansion (mm)
do = inside diameter of rotor at initial temperature (mm)
α = coefficient of thermal expansion of aluminum, 23.1 10-6 (mm/mm0C)
ΔT = change in temperature (0C )
Room temperature =27 0C
Table 2: Theoretical modelling of Thermal expansion
Part Material Outside diameter
(mm)
Inside
Diameter(mm)
Stack
Height(mm)
Coefficient of Thermal
expansion(mm/mm0c)
Rotor Aluminium 60.3 19.5 63.5 23.1
Original diameter of
rotor bore (mm)
Temperature
(0C)
Thermal expansion of
rotor bore (mm)
Increased diameter of
rotor bore (mm)
19.5 50 0.01 19.51
19.5 80 0.023 19.523
19.5 100 0.032 19.53
19.5 150 0.05 19.55
19.5 200 0.07 19.57
19.5 225 0.089 19.58
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 333
Experimental method for obtaining required thermal expansion of rotor bore by heating from inside surface of rotor
bore:
Rotor Material Rotor outside diameter (mm) Rotor inside diameter (mm)
Aluminium 60.3 19.5
Table 3: Dimensions of aluminium rotor bore
Process: A 2 KW cartridge heater rod is used to heat the rotor bore. The rod is inserted intotherotorboreandpower isapplied
for time to reach the required temperature at which thermal expansionofrotor boreisobtained.Inthisprocesstriedtoexpand
the rotor bore at various temperature. Temperature is measured by thermocouple. Thermal expansion is measured by digital
vernier caliper having least count of 0.01mm.
Figure 2. Cartridge Heater Rod Figure 3. Aluminum Rotor
Figure 4. Experimental Setup Figure 5. Thermal Expansion of aluminium
rotor bore
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 334
Experimental Result:
Table 4: Experimental results of thermal expansion
Comparison of Theoretical and Experimental result
Figure 6. A comparison between theoretical and experimental measured results
Original Diameter of
rotor bore(mm)
Temperature(ºC) Thermal
expansion(mm)
Change in diameter of
rotor bore(mm)
19.5 50 0.03 19.53
19.5 80 0.06 19.56
19.5 100 0.08 19.58
19.5 150 0.18 19.68
Temperature(⁰C)
Thermal Expansion
Theoretical (mm) Experimental(mm)
50 0.01 0.03
80 0.023 0.06
100 0.032 0.08
150 0.05 0.18
200 0.07 0.25
225 0.08 0.33
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 335
Reasons for getting difference between theoretical and experimental results:
 From figure, it is observed that there is difference between theoreticalandexperimentalexpansionvalues,itisbecause
of role of heating time in getting expansion.
 In experimental method, expansion obtained is more because of heating time is getting more for every time.
 More heat energy is transferred to material, so expansion is more.
Mathematical Modelling of Friction Force:
Friction or frictional force is defined as the force that resists an object’s motion ona surface.Theobjectcaneither be stationary
or in motion relative to the surface. Friction occurs where the object is in contactwiththesurface.Inotherwords,it takesplace
between two surfaces, and hence, is a contact force.
Figure 7. Schematic of Shrink fit assembly
The “coulomb friction” model is used for modelling tangential forces between contact surfaces. If tangential forces are lower
than friction forces µN, they will be proportional to the relative displacement between the contact surfaces. If they are larger,
the contact surfaces start to slip and the tangential forces will equal the friction forces. This condition is called as “macro-slip"
model. So to avoid this phenomenon in case of rotor shaft shrink fit assembly, frictional force should be greater than the
tangential force. Then there will be relative displacement between rotor and shaft.
 The contact pressure between rotor and shaft involved in interference fit is given by the Lame´s equation:
























i
i
i
i
o
o
o
o R
R
R
R
E
R
R
R
R
R
E
R
p



2
2
2
2
2
2
2
2
Where,
p = contact pressure between rotor and shaft during assembly (Pa)
δ = Radial interference (m)
R = Outside radius of shaft (m)
Ro = Outside radius of rotor (m)
Ri = Inside radius of shaft = zero (solid shaft)
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 336
Eo = Modulus of elasticity of rotor (Pa)
Ei = Modulus of elasticity of shaft Pa)
γ0 = Poisson’s Ratio for rotor
γi = Poisson’s Ratio for shaft
 Maximum frictional force developed due to contact pressure:
FF = p × 2π × R × L × µ
Where,
p = contact pressure (Pa)
R = Radius of shaft (m)
µ = Coefficient of friction between rotor and shaft
L = Length of contact (m)
 Tangential force given by motor :
Torque = Tangential force × radius of shaft
T = FT × R
Where,
T = Motor starting torque (Nm)
FT = Tangential Force (N)
R = Radius of shaft (m)
If frictional force is greater than tangential force then shaft can transmit the specified power of motor and interference fit is
suitable for rotor shaft assembly.
Conclusion:
 Heating from inside of the rotor bore can be a better option for heating rotor to get quicker expansion of rotor bore.
 In case of heating rotor bore, heating will be only local heating. Only required part is heated and expanded.
 This method gives possibility of avoiding cooling of assembly, so it could remove cooling operation all together.
Future Scope:
Some opportunities for future work on present dissertation work are outlined as follows:
 Heating from bore diameter can be achieved by suitably designed induction coil that fits into bore.
 Study the effect of varying the size and shape of the induction heating coil in case of external heating of the rotor.
 Add a sleeve of highly conductive material to the inner surface of the rotor so that it expands easily.
References:
1. Fiji Toma, Optimization of rotor shaft shrink-fit method for motor using ‘‘Robust design,’’ Journal of Industrial
Engineering International (2018),pp. 705–717
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072
© 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 337
2. Mitesh. S. Agrawal, Ankit. M. Rathi, Prof. Prashant. B. Shiwalkar, ‘Algorithm in Automated Press Fit for Rotor Shaft
Assembly of an Induction Motor’, IJIRSET, Vol. 5, Issue 11, November 2016, pp. 20143-20149.
3. Nazım Arda Eyyuboğlu, ‘Investigation of the Parameters Affecting Crankshaft and Rotor Interference Fit’, school of
mechanical engineering, 2014, pp.1-10.
4. Somnath Kolgiri, “Static and Dynamic Analysis for Rotor Shaft of Electric Motor”, (2009), pp.1-17.
5. J.D. Booker and C.E. Truman, MEASURING THE COEFFICIENT OF FRICTION FOR USE IN SHRINK-FIT CALCULATIONS,
Department of Mechanical Engineering, University of Bristol, UK, November 2009,pp.7-13.
6. Truman, C.E., and Booker, J.D., ‘‘Analysis of a Shrink-fit Failure on a Gear Hub/Shaft Assembly,’’ Engineering Failure
Analysis 14(4):557–572 (2007).

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“Design and development of better alternatives to shrink fit achieved by induction heating in rotor shaft assembly of the hermetically sealed reciprocating compressor”

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 331 “Design and development of better alternatives to shrink fit achieved by induction heating in rotor shaft assembly of the hermetically sealed reciprocating compressor” Nandini Chavan1, Dr .M. S. Kale 2 Student, Mechanical Engineering Department, Government College Of Engineering, Karad, Maharashtra India. ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - In rotorshaft assembly of hermetically sealed reciprocating compressor, there is interferencefitbetweenrotorand shaft. To obtain this interference fit various methods are used. Without the use of extra mechanical fastening systems, interference-fitted joints are an efficient and cost-effective way to assemble components. An interface pressure is established during assembly by press-fitting or a shrink-fitting assembly process as a result of a dimensional misfit between the two parts, which is frequently in a shaft and rotor. Because of frictional resistance, the joint is able to withstand axial forces and torques. The traditional method for achievinga shrink fit between the rotorand shaft is induction heating. Thisprocessrequiresheating equipment and higher energy consumption,thiswillincreasethemanufacturingcostofthecompressor.Duetothelimitationsof induction heating process, there is a need to identify and design an alternative options for achieving shrink fit in rotor shaft assembly in cost effective manner yet ensuring the desired quality. This paper presents the study of current and proposed assembly procedureused to get rotor-shaft assembly in hermeticallysealedreciprocatingcompressor.Inthisstudy,factorsthat affect an interference-fitted joints' abilitytofunctionproperlyaregroupedunderafewgeneralheadings,including:coefficientof friction, coefficient of thermal expansion, surfaces, the geometry,frictionalforce,torque,tangentialforce,materials,loading,and lastly the assembly method utilized to create the joint between the rotor and shaft. Keywords: Interference fit, , rotorshaftassembly,shrinkfitting,inductionheating,radialorinterfacepressure,torque, frictional force, tangential force. 1. INTRODUCTION: In rotorshaft assembly of thehermetically sealed reciprocatingcompressor,toachieveaninterferencefitbetweenrotorand shaft, shrink fitting techniques are generally used. Shrink fitting typically refers to techniques that utilize the phenomena of thermal contraction and expansion to produce an interference fit. The most common method for doing this is to heat the outer component, causing it to expand thermally. Then two parts fit together easily. An incredibly tight joint forms around the inner part when the outer part cools to room temperature and contracts back to its original size. Typically, metals will expand in response to heating. So induction heating is generally used to obtain shrink fit in rotor shaft assembly. In existing induction heating process rotoris heated from outsidesurface and then heat istransferredfromoutsidetoinsidesurfaceofrotortoobtain thermal expansion of rotor bore. After expansion, rotor is shrink fitted into the shaft. But this process requires higher power consumption and hence increases the manufacturing costof the compressor.Soheatingfromtheinsidesurfaceoftherotorbore is the alternative option to achieve shrink fit in rotor shaft assembly. 2. Rotor Shaft Assembly: Figure 1.Dimensions of rotor and shaft interference fit prior to assembling dA = Outside diameter of shaft dM = Inside diameter of rotor
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 332 d = Diametric interference Figure shows the dimensions of rotor and shaft interference fit prior to assembling.Interferencefitisalsoknownaspress fitor friction fit, is a fastening method where two parts, typically circular cross section shape, are pushed together (one into the other) and kept in place due to the pressure between them. Typically, theinnerpartwill havea nominal outerdiameterslightly greater than the nominal inner diameter of the outer part, and when pushed or forced together thecontactfrictionforceskeep the parts from moving relative to each other. Thelevel ofinterferencedependsonthe negativedifferenceinnominal diameters. Shrink Fit Process Obtaining shrink fit by heating from the inside surface of the rotor bore: The only viable way to heat the rotor is using an inductioncoil from the insidesurfaceoftheoftherotorbore,thisheatallowsfor better energy delivery to the assembly. In this method heating will beonlylocalheating.Aninductioncoilcanbeusedtoheatthe rotor bore. The coil is inserted into the rotor bore and power is applied for certain time to reach the required temperature for heating the rotor bore and tried to expand the rotor bore and placed onto the shaft. This process consumes less power as compared to heating from the outside surface of rotor. Theoretical modelling of Thermal expansion: Table 1: Dimensions and material properties of aluminium rotor Diameter increase of rotor bore when being heated or Thermal expansion of rotor bore is calculated as: Δd = doαΔT Where, Δd = change in diameter of rotor bore or thermal expansion (mm) do = inside diameter of rotor at initial temperature (mm) α = coefficient of thermal expansion of aluminum, 23.1 10-6 (mm/mm0C) ΔT = change in temperature (0C ) Room temperature =27 0C Table 2: Theoretical modelling of Thermal expansion Part Material Outside diameter (mm) Inside Diameter(mm) Stack Height(mm) Coefficient of Thermal expansion(mm/mm0c) Rotor Aluminium 60.3 19.5 63.5 23.1 Original diameter of rotor bore (mm) Temperature (0C) Thermal expansion of rotor bore (mm) Increased diameter of rotor bore (mm) 19.5 50 0.01 19.51 19.5 80 0.023 19.523 19.5 100 0.032 19.53 19.5 150 0.05 19.55 19.5 200 0.07 19.57 19.5 225 0.089 19.58
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 333 Experimental method for obtaining required thermal expansion of rotor bore by heating from inside surface of rotor bore: Rotor Material Rotor outside diameter (mm) Rotor inside diameter (mm) Aluminium 60.3 19.5 Table 3: Dimensions of aluminium rotor bore Process: A 2 KW cartridge heater rod is used to heat the rotor bore. The rod is inserted intotherotorboreandpower isapplied for time to reach the required temperature at which thermal expansionofrotor boreisobtained.Inthisprocesstriedtoexpand the rotor bore at various temperature. Temperature is measured by thermocouple. Thermal expansion is measured by digital vernier caliper having least count of 0.01mm. Figure 2. Cartridge Heater Rod Figure 3. Aluminum Rotor Figure 4. Experimental Setup Figure 5. Thermal Expansion of aluminium rotor bore
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 334 Experimental Result: Table 4: Experimental results of thermal expansion Comparison of Theoretical and Experimental result Figure 6. A comparison between theoretical and experimental measured results Original Diameter of rotor bore(mm) Temperature(ºC) Thermal expansion(mm) Change in diameter of rotor bore(mm) 19.5 50 0.03 19.53 19.5 80 0.06 19.56 19.5 100 0.08 19.58 19.5 150 0.18 19.68 Temperature(⁰C) Thermal Expansion Theoretical (mm) Experimental(mm) 50 0.01 0.03 80 0.023 0.06 100 0.032 0.08 150 0.05 0.18 200 0.07 0.25 225 0.08 0.33
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 335 Reasons for getting difference between theoretical and experimental results:  From figure, it is observed that there is difference between theoreticalandexperimentalexpansionvalues,itisbecause of role of heating time in getting expansion.  In experimental method, expansion obtained is more because of heating time is getting more for every time.  More heat energy is transferred to material, so expansion is more. Mathematical Modelling of Friction Force: Friction or frictional force is defined as the force that resists an object’s motion ona surface.Theobjectcaneither be stationary or in motion relative to the surface. Friction occurs where the object is in contactwiththesurface.Inotherwords,it takesplace between two surfaces, and hence, is a contact force. Figure 7. Schematic of Shrink fit assembly The “coulomb friction” model is used for modelling tangential forces between contact surfaces. If tangential forces are lower than friction forces µN, they will be proportional to the relative displacement between the contact surfaces. If they are larger, the contact surfaces start to slip and the tangential forces will equal the friction forces. This condition is called as “macro-slip" model. So to avoid this phenomenon in case of rotor shaft shrink fit assembly, frictional force should be greater than the tangential force. Then there will be relative displacement between rotor and shaft.  The contact pressure between rotor and shaft involved in interference fit is given by the Lame´s equation:                         i i i i o o o o R R R R E R R R R R E R p    2 2 2 2 2 2 2 2 Where, p = contact pressure between rotor and shaft during assembly (Pa) δ = Radial interference (m) R = Outside radius of shaft (m) Ro = Outside radius of rotor (m) Ri = Inside radius of shaft = zero (solid shaft)
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 336 Eo = Modulus of elasticity of rotor (Pa) Ei = Modulus of elasticity of shaft Pa) γ0 = Poisson’s Ratio for rotor γi = Poisson’s Ratio for shaft  Maximum frictional force developed due to contact pressure: FF = p × 2π × R × L × µ Where, p = contact pressure (Pa) R = Radius of shaft (m) µ = Coefficient of friction between rotor and shaft L = Length of contact (m)  Tangential force given by motor : Torque = Tangential force × radius of shaft T = FT × R Where, T = Motor starting torque (Nm) FT = Tangential Force (N) R = Radius of shaft (m) If frictional force is greater than tangential force then shaft can transmit the specified power of motor and interference fit is suitable for rotor shaft assembly. Conclusion:  Heating from inside of the rotor bore can be a better option for heating rotor to get quicker expansion of rotor bore.  In case of heating rotor bore, heating will be only local heating. Only required part is heated and expanded.  This method gives possibility of avoiding cooling of assembly, so it could remove cooling operation all together. Future Scope: Some opportunities for future work on present dissertation work are outlined as follows:  Heating from bore diameter can be achieved by suitably designed induction coil that fits into bore.  Study the effect of varying the size and shape of the induction heating coil in case of external heating of the rotor.  Add a sleeve of highly conductive material to the inner surface of the rotor so that it expands easily. References: 1. Fiji Toma, Optimization of rotor shaft shrink-fit method for motor using ‘‘Robust design,’’ Journal of Industrial Engineering International (2018),pp. 705–717
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 09 Issue: 09 | Sep 2022 www.irjet.net p-ISSN: 2395-0072 © 2022, IRJET | Impact Factor value: 7.529 | ISO 9001:2008 Certified Journal | Page 337 2. Mitesh. S. Agrawal, Ankit. M. Rathi, Prof. Prashant. B. Shiwalkar, ‘Algorithm in Automated Press Fit for Rotor Shaft Assembly of an Induction Motor’, IJIRSET, Vol. 5, Issue 11, November 2016, pp. 20143-20149. 3. Nazım Arda Eyyuboğlu, ‘Investigation of the Parameters Affecting Crankshaft and Rotor Interference Fit’, school of mechanical engineering, 2014, pp.1-10. 4. Somnath Kolgiri, “Static and Dynamic Analysis for Rotor Shaft of Electric Motor”, (2009), pp.1-17. 5. J.D. Booker and C.E. Truman, MEASURING THE COEFFICIENT OF FRICTION FOR USE IN SHRINK-FIT CALCULATIONS, Department of Mechanical Engineering, University of Bristol, UK, November 2009,pp.7-13. 6. Truman, C.E., and Booker, J.D., ‘‘Analysis of a Shrink-fit Failure on a Gear Hub/Shaft Assembly,’’ Engineering Failure Analysis 14(4):557–572 (2007).