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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 350
Explicit dynamic analysis of gear tooth of a synchromesh manual
transmission gear box
SHREEKANTH R D 1, H S MANJUNATH2, BYRE GOWDA K C3, AMITH KUMAR S N4
1M.Tech Scholar, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru
2Assistant Professor, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru
3Assistant Professor, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru
4Assistant Professor, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract - New ideas and developed solution are the best
compliments for the desired solution in order to avoid failure
in gears and improve the service life using new technologies
makes accomplishmentofobjectives. Materialpropertiesplays
a very important role during the process we need to compare
it with different other material properties .using simulation
software all the desired functions can be checked analytically
and mathematical ways .since the basis of experiments were
on trial and error methods upon that we need to design some
model using CAD software. Later we import through ABAQUS
software, so simulation is done further. Since by using the
software it makes work faster and accurate results can be
achieved without any loss of data. It helps in realizing the
stress levels in the desired manner.
Key Words: PET bottle; Structural Optimization; Light
weight Design.
1. INTRODUCTION
Gears are one of the primitive sector of human inventions
surprisingly machines as that uses gearing asoneofthekind
of gear design considered for a specific importance place a
very important role for the industrial point of view gear is
considered as a important aspect of vibration analysis in
order to realize the behavior of the gears when they are
meshed quiet importantly it would perform through system
monitoring and control of the gear transmission system
basic understanding of gear mesh needs to be confirmed.
Stress are produced when gears are meshed together some
kind of activities that takes place such as tooth bending and
shearing this characteristic was finely noted at a nonlinear
problem by applying codes and different elements and
algorithms. Due to complicated condition solution converge
results those are obtained are challenging some solution
angular displacement gear pitch circle rolls on each other
without slipping at constant torque load contact region
similarly change can accomplish from singletoothcontact to
double contact region due to mesh cycle tool at line of action
normal contact force of tooth mesh stiffness tend to act and
gear transmission can be easily found out. Coupling among
transverse motion and torsion of the system where linear
mesh stiffness gives the feasible approach to learn coupling.
Gear modelling and analysis was not only the important
objective linear tooth mesh stiffness and finite element
analysis we used to compare among those experiments
conducted a aim is to validate gear box diagnostic
methodologies we need to identify the vibration frequency
associated with gear and bearing.
Fig -1: A typical multi-mesh gear system
2. METHODOLOGY
The main basic steps is create a geometric model of gear
structure will be modeled using solid edge modeling tool.
Once the model is created as per specification then it is
imported into ABAQUS for meshing. Extract mid surfaceand
mesh the model using shell elements. Then the performance
linear analysis for bending loads using the ABAQUS solver
and finally comparing the strength required for standards.
2.1 Dynamic analysis
Dynamic analysis carried out at different loading condition
to get the stress level of the component
2.2 Material Properties
Material property for AISI 8630 steel
Table -1: Material Property
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 351
2.3 Geometric modeling
Fig -2: A typical multi-mesh gear system
The above figure 2 gives the representation of geometric
modeling structure and The modeling has been done using
the modeling software, SOLID EDGE. Solid works is a
modeler which utilizes a parametric feature-basedapproach
to create model and assemblies. Constraints are referred as
parameters whose values determine the shape or geometry
of the model or assembly. Parameters can be either numeric
or geometric, numerical such as circle diameter or line
lengths and geometric, such as parallel, concentric, tangent
etc.
Model is built in solid works by 2D sketch. Then todefine the
size and location, dimensions are added to the sketch.
Relations are used to define attributes such as
perpendicularity, parallelism and tangency. Later drawings
are created from parts.
Based on this drawing views are generated automatically
and to this tolerance and dimensions are added.
After creation of model then this model will be imported to
abaqus where meshing is done. During meshing elements
are selected based on the requirements and the meshing of
the model is done as shown below following the procedure.
Fig -3: FE Meshed model
The meshed model shown n the above figure is the finite
element model of gear structure which is discredited using
hexahedral element of type C3D8R. These elements are
selected because of their ability to capture the geometry of
any complex model. Since the model is of various size and
shapes, hence hexahedral element is used. The meshed gear
total number of node is 239278 and total number of the
element is 209485.
2.4 Loads and Boundary conditions
Fig -4: loads and boundary condition
The boundary condition is the one of the major important
factors to govern the output result of FEA and loading
condition or loads are forces, acceleration or deformations
applied to a structure or its components. Load cause
deformations, displacement and stress in structures.
Applying the loads and boundary condition plays a
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 352
significant role boundary applied whenever needed or
required since that closely matched motion as loads acts at
the system depending on the mannerism of the abaqus
boundary condition are applied condition varies if explicit
procedure had been chosen degree of freedom restricts for
both pinion and gear except the rotational motion therefore
it is free rotate the gear is axially and radially constrained
then analytically rigid surface used to simulate shaftmethod
is used and applied at 125 rad per sec of angular velocity .
3. RESULTS
3.1 Explicit Dynamic Analysis, Displacement
Fig -5: Explicit Displacement of Gears
The two gears are contact with each other and one
gear rotation in clock wise direction and other is
rotated in the antilock wise direction. The load is
increases and corresponding to the stress is also
increases. The displacement of the above model is
6mm with respect to the step time 2.400e-3
3.2 Stages of displacement
Fig -6: First stages of displacement of the gears
Fig -7: Second stages of displacement of the gears
The stages displaced are find out by using Abqus solver in
Fig 6 shows the magnitude of the model is 0.1mm with
respect to the step time 0 and Fig 7 shows second stage of
the displacement is 0.3mm with respect to the step time
1.0001e-04 in the figure 3.2 you can see the gear and the
pinion at the rest position the displaced activity is absolute
zero and there is no variation in the movement of the gears
hence there is no transient vibration .since the explicit
methods is not applied here in the case of any vibration that
is caused during the vibration in the figure 3.3itundergoesa
displacement so explicit methods are imbibed here since
there should be some amount of accuracy is high and fast
that can be easily realized. It is significant to understand the
displacement where the exact location of gear approached
and what position the gears are revoked the abaqus plays a
important role in realizing the movements of the gear due to
actual load condition.
3.2 Explicit dynamic stress analysis
Fig -8: Explicit Dynamic Stress Analysis
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 353
Abaqus in the case of linear and nonlinear dynamic analysis
work will be carried out at abaqus addition to it such as
inertial affect and dynamic nonlinear system responseto the
torque input of the driving gear was successfully examined.
In the case of nonlinear analysis there can be a choice
between modes and direct integration methods. So as the
performance of the program changes we can roll on to
slightly nonlinear system where modal method can be
performed using Eigen modes as a platform for calculating
the response. Then commuting the problem becomes less
expensive and simple to use the direct integrationapplied to
all the degree of freedom. Maximum stress goes up to
1269.8Mpa.
3.3 Stages of Stress Development
Fig -9: First Stages of Stress Development
Fig -10: Second Stages of stress development
Fig -11: Third Stages of stress development
3.4 Contact pressure
Fig -10: Contact Pressure
The contact stress created when surface of two bodies are
bodies are pressed together by external loads are significant
stress. The FEA results for the contact pressure distribution
at different position along the contact path of gear teeth as
shown above the figure. The variation ofcontactpressure on
the gear tooth. Which shows similar trend to its loadsharing
pattern. The contact pressure developed two surface of gear
contact with each other the maximum pressuredevelopedis
1725.3Mpa using ABAQUAS software. Along the z direction
the stress value is found to be zero, mean stress is found to
be about 1006.4 Mpa .The increment values 64845 at the
step 1 and inhibited step time would be 7.0001E0.4.
Pressure depends upon the path of engagement and dis
engagement of the gears and the line of contact of the stress
is concentrated to one values. Since the pressure angle
between the common tangent and common normal goes on
decreasing due to the variation of the loads one of the stress
components becomes zero in the z direction
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072
© 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 354
4. CONCLUSION
The synchromesh gear system is analyzed for the
strength and dynamic simulation of the gear
movements is captured. Explicit dynamic analysis
proves to be a great tool to study the time dependent
behavior of the gears where the sequence of events is
calculated for a very small time period of impact
conditions. The high speed gear contact isfoundtobein
accordance with the expected behavior. The contact
stress developed is slightly higher at 1270 Mpa, owing
to the nature of dynamic impact stress of up to two
times the normal static stress which can be acceptable.
The rotation sequence shows constant engagementand
disengagement of the gears and subsequent stress
transfer can be seen from the sequence of event. The
contact pressure plotshowsthenormal contactwhichis
desired is obtained. The stress values those are
calculated during the engagement and dis engagement
is said to be convinced with the desired values.
Displacement during the action of the loads is said tobe
limited hence leads to the smooth operation of gears.
The main objective is to obtain the stress value below
2000 MPA hence it is achieved
REFERENCES
1. S.Sai Anusha, P.Satish Reddy, P.Bhaskar, MManoj
“Contact Stress Analysis of Helical Gear by Using
AGMA and ANSYS” Vol 2, Issue 12, 2014.
2. Mrs.Shinde S.P, Mr. Nikam A.A , Mr. Mulla T.S.
“Static Analysis of Spur Gear Using FiniteElement
Analysis” ISSN: 2278-1684, PP: 26-31.
3. Ivana Atanasovska, Vera Nikolic-Stanojlovic,
Dejan Dimitrijevic, Dejan
4. Momcilovic “Finite Element Model for Stress
Analysis and Nonlinear Contact Analysis of Helical
Gears” Vol.LVIX,No.1,2009.
5. Mohammad Asaduzzaman Chowdhury, Dewan
Muhammad Nuruzzaman, Biplov
6. Kumar Roy “Experimental Investigation of Friction
Coefficient and Wear Rate of
7. Stainless Steel 304 Sliding against Smooth and
Rough Mild Steel Counter faces” 2013.

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Explicit dynamic analysis of gear tooth stress in manual transmission

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 350 Explicit dynamic analysis of gear tooth of a synchromesh manual transmission gear box SHREEKANTH R D 1, H S MANJUNATH2, BYRE GOWDA K C3, AMITH KUMAR S N4 1M.Tech Scholar, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru 2Assistant Professor, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru 3Assistant Professor, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru 4Assistant Professor, Mechanical Engineering, Dr. Ambedkar Institute of Technology, Bengaluru ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract - New ideas and developed solution are the best compliments for the desired solution in order to avoid failure in gears and improve the service life using new technologies makes accomplishmentofobjectives. Materialpropertiesplays a very important role during the process we need to compare it with different other material properties .using simulation software all the desired functions can be checked analytically and mathematical ways .since the basis of experiments were on trial and error methods upon that we need to design some model using CAD software. Later we import through ABAQUS software, so simulation is done further. Since by using the software it makes work faster and accurate results can be achieved without any loss of data. It helps in realizing the stress levels in the desired manner. Key Words: PET bottle; Structural Optimization; Light weight Design. 1. INTRODUCTION Gears are one of the primitive sector of human inventions surprisingly machines as that uses gearing asoneofthekind of gear design considered for a specific importance place a very important role for the industrial point of view gear is considered as a important aspect of vibration analysis in order to realize the behavior of the gears when they are meshed quiet importantly it would perform through system monitoring and control of the gear transmission system basic understanding of gear mesh needs to be confirmed. Stress are produced when gears are meshed together some kind of activities that takes place such as tooth bending and shearing this characteristic was finely noted at a nonlinear problem by applying codes and different elements and algorithms. Due to complicated condition solution converge results those are obtained are challenging some solution angular displacement gear pitch circle rolls on each other without slipping at constant torque load contact region similarly change can accomplish from singletoothcontact to double contact region due to mesh cycle tool at line of action normal contact force of tooth mesh stiffness tend to act and gear transmission can be easily found out. Coupling among transverse motion and torsion of the system where linear mesh stiffness gives the feasible approach to learn coupling. Gear modelling and analysis was not only the important objective linear tooth mesh stiffness and finite element analysis we used to compare among those experiments conducted a aim is to validate gear box diagnostic methodologies we need to identify the vibration frequency associated with gear and bearing. Fig -1: A typical multi-mesh gear system 2. METHODOLOGY The main basic steps is create a geometric model of gear structure will be modeled using solid edge modeling tool. Once the model is created as per specification then it is imported into ABAQUS for meshing. Extract mid surfaceand mesh the model using shell elements. Then the performance linear analysis for bending loads using the ABAQUS solver and finally comparing the strength required for standards. 2.1 Dynamic analysis Dynamic analysis carried out at different loading condition to get the stress level of the component 2.2 Material Properties Material property for AISI 8630 steel Table -1: Material Property
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 351 2.3 Geometric modeling Fig -2: A typical multi-mesh gear system The above figure 2 gives the representation of geometric modeling structure and The modeling has been done using the modeling software, SOLID EDGE. Solid works is a modeler which utilizes a parametric feature-basedapproach to create model and assemblies. Constraints are referred as parameters whose values determine the shape or geometry of the model or assembly. Parameters can be either numeric or geometric, numerical such as circle diameter or line lengths and geometric, such as parallel, concentric, tangent etc. Model is built in solid works by 2D sketch. Then todefine the size and location, dimensions are added to the sketch. Relations are used to define attributes such as perpendicularity, parallelism and tangency. Later drawings are created from parts. Based on this drawing views are generated automatically and to this tolerance and dimensions are added. After creation of model then this model will be imported to abaqus where meshing is done. During meshing elements are selected based on the requirements and the meshing of the model is done as shown below following the procedure. Fig -3: FE Meshed model The meshed model shown n the above figure is the finite element model of gear structure which is discredited using hexahedral element of type C3D8R. These elements are selected because of their ability to capture the geometry of any complex model. Since the model is of various size and shapes, hence hexahedral element is used. The meshed gear total number of node is 239278 and total number of the element is 209485. 2.4 Loads and Boundary conditions Fig -4: loads and boundary condition The boundary condition is the one of the major important factors to govern the output result of FEA and loading condition or loads are forces, acceleration or deformations applied to a structure or its components. Load cause deformations, displacement and stress in structures. Applying the loads and boundary condition plays a
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 352 significant role boundary applied whenever needed or required since that closely matched motion as loads acts at the system depending on the mannerism of the abaqus boundary condition are applied condition varies if explicit procedure had been chosen degree of freedom restricts for both pinion and gear except the rotational motion therefore it is free rotate the gear is axially and radially constrained then analytically rigid surface used to simulate shaftmethod is used and applied at 125 rad per sec of angular velocity . 3. RESULTS 3.1 Explicit Dynamic Analysis, Displacement Fig -5: Explicit Displacement of Gears The two gears are contact with each other and one gear rotation in clock wise direction and other is rotated in the antilock wise direction. The load is increases and corresponding to the stress is also increases. The displacement of the above model is 6mm with respect to the step time 2.400e-3 3.2 Stages of displacement Fig -6: First stages of displacement of the gears Fig -7: Second stages of displacement of the gears The stages displaced are find out by using Abqus solver in Fig 6 shows the magnitude of the model is 0.1mm with respect to the step time 0 and Fig 7 shows second stage of the displacement is 0.3mm with respect to the step time 1.0001e-04 in the figure 3.2 you can see the gear and the pinion at the rest position the displaced activity is absolute zero and there is no variation in the movement of the gears hence there is no transient vibration .since the explicit methods is not applied here in the case of any vibration that is caused during the vibration in the figure 3.3itundergoesa displacement so explicit methods are imbibed here since there should be some amount of accuracy is high and fast that can be easily realized. It is significant to understand the displacement where the exact location of gear approached and what position the gears are revoked the abaqus plays a important role in realizing the movements of the gear due to actual load condition. 3.2 Explicit dynamic stress analysis Fig -8: Explicit Dynamic Stress Analysis
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 353 Abaqus in the case of linear and nonlinear dynamic analysis work will be carried out at abaqus addition to it such as inertial affect and dynamic nonlinear system responseto the torque input of the driving gear was successfully examined. In the case of nonlinear analysis there can be a choice between modes and direct integration methods. So as the performance of the program changes we can roll on to slightly nonlinear system where modal method can be performed using Eigen modes as a platform for calculating the response. Then commuting the problem becomes less expensive and simple to use the direct integrationapplied to all the degree of freedom. Maximum stress goes up to 1269.8Mpa. 3.3 Stages of Stress Development Fig -9: First Stages of Stress Development Fig -10: Second Stages of stress development Fig -11: Third Stages of stress development 3.4 Contact pressure Fig -10: Contact Pressure The contact stress created when surface of two bodies are bodies are pressed together by external loads are significant stress. The FEA results for the contact pressure distribution at different position along the contact path of gear teeth as shown above the figure. The variation ofcontactpressure on the gear tooth. Which shows similar trend to its loadsharing pattern. The contact pressure developed two surface of gear contact with each other the maximum pressuredevelopedis 1725.3Mpa using ABAQUAS software. Along the z direction the stress value is found to be zero, mean stress is found to be about 1006.4 Mpa .The increment values 64845 at the step 1 and inhibited step time would be 7.0001E0.4. Pressure depends upon the path of engagement and dis engagement of the gears and the line of contact of the stress is concentrated to one values. Since the pressure angle between the common tangent and common normal goes on decreasing due to the variation of the loads one of the stress components becomes zero in the z direction
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 05 Issue: 11 | N ov 2018 www.irjet.net p-ISSN: 2395-0072 © 2018, IRJET | Impact Factor value: 7.211 | ISO 9001:2008 Certified Journal | Page 354 4. CONCLUSION The synchromesh gear system is analyzed for the strength and dynamic simulation of the gear movements is captured. Explicit dynamic analysis proves to be a great tool to study the time dependent behavior of the gears where the sequence of events is calculated for a very small time period of impact conditions. The high speed gear contact isfoundtobein accordance with the expected behavior. The contact stress developed is slightly higher at 1270 Mpa, owing to the nature of dynamic impact stress of up to two times the normal static stress which can be acceptable. The rotation sequence shows constant engagementand disengagement of the gears and subsequent stress transfer can be seen from the sequence of event. The contact pressure plotshowsthenormal contactwhichis desired is obtained. The stress values those are calculated during the engagement and dis engagement is said to be convinced with the desired values. Displacement during the action of the loads is said tobe limited hence leads to the smooth operation of gears. The main objective is to obtain the stress value below 2000 MPA hence it is achieved REFERENCES 1. S.Sai Anusha, P.Satish Reddy, P.Bhaskar, MManoj “Contact Stress Analysis of Helical Gear by Using AGMA and ANSYS” Vol 2, Issue 12, 2014. 2. Mrs.Shinde S.P, Mr. Nikam A.A , Mr. Mulla T.S. “Static Analysis of Spur Gear Using FiniteElement Analysis” ISSN: 2278-1684, PP: 26-31. 3. Ivana Atanasovska, Vera Nikolic-Stanojlovic, Dejan Dimitrijevic, Dejan 4. Momcilovic “Finite Element Model for Stress Analysis and Nonlinear Contact Analysis of Helical Gears” Vol.LVIX,No.1,2009. 5. Mohammad Asaduzzaman Chowdhury, Dewan Muhammad Nuruzzaman, Biplov 6. Kumar Roy “Experimental Investigation of Friction Coefficient and Wear Rate of 7. Stainless Steel 304 Sliding against Smooth and Rough Mild Steel Counter faces” 2013.