design and fea based vibration characteristic analysis of ... · considered rocker bogie mechanism....
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Design and FEA Based Vibration Characteristic Analysis of Rocker
Bogie Mechanism
Vishvajeet
B.Tech student, Department of Mechanical Engineering,
Dev Bhoomi Institute of Technology,
Dehradun, Uttrakhand, India.
Faraz Ahmad
Assistant professor, Department of Mechanical Engineering,
Dev Bhoomi Institute of Technology,
Dehradun, Uttrakhand, India.
Pankaj Singh
B.Tech student, Department of Mechanical Engineering,
Dev Bhoomi Institute of Technology,
Dehradun, Uttrakhand, India.
Ravindra singh
B.Tech student, Department of Mechanical Engineering,
Dev Bhoomi Institute of Technology,
Dehradun, Uttrakhand, India.
ABSTRACT A rocker bogie mechanism is a vehicle in which the
mechanisms balance the Bogie at different ground
conditions. Rockers bogie mechanism is generally
used by space research companies for space
exploration. Now days it has application in various
fields like; military, spy vision at hilly areas etc. This
type of moving vehicle was subjected to vibration. So
the present study deals with the modeling of the
rocker bogie mechanism, which was design by Catia
software and analyzed by Ansys 14.0. The failure
frequency range was determined by changing the
boundary condition of the considered rocker bogie
mechanism. First six failure frequencies were
calculated by modal analysis. Furthermore the model
was analyzed for static lording condition. The
simulation result was under safety limit and can
sustain the failure criteria.
Keyword: Rocker mechanism, vibration, CAD
model, failure range.
Introduction
In Rocker Bogie Mechanism, The term Rocker
denotes the links of the mechanism. There was six
links at both side of the mechanism and balanced the
Bogie in the moving condition. To maintain the
center of gravity of the vehicle, one link or rocker of
the rocker bogie mechanism moves upward and the
other rockers goes downward. One side of the rocker
was connected to the drive wheel the other end
connected to the bogie and the relative movement
provides the required motion and degree of freedom
to the rocker bogie mechanism. Many researchers
work on the dynamic modeling and control of the
rocker mechanism like:
Rockers bogie mechanism becomes the NASA’s
most favorite design of wheel robot, the main
problem with this mechanism is its low average
operating speed, places where the large flat surface is
needed to cover in short time interval this mechanism
becomes not suitable mechanism, mainly due to its
stability problems [1-4].
Nitin Yadav et. al. have studied about the places,
where the gravitational coefficient remains lower
than the earth, at this place available suspension
system not gives the required results as the shock
absorbing or among the changes. To oppose this anti
gravity effect, Jet Propulsion Laboratory and NASA
introduced a mechanism called the rocker bogie
mechanism. It is generally a suspension system
basically used in mechanical robotics vehicles for the
space explorations .This suspension based mars rover
International Journal of Applied Engineering Research ISSN 0973-4562 Volume 14, Number 9, 2019 (Special Issue) © Research India Publications. http://www.ripublication.com
Page 209 of 214
mechanism is firstly introduced for the Mars Path
finder, Mars Exploration and for Mars Science
Laboratory mission. The motive this research is to
understand the mechanical design [5].
Brian D. el. al. has designed the rocker bogie
mechanism for slow speed. It is able to climb the
obstacles that are of the size of a wheel. When
obstacle comes, the vehicles motion effectively stops
and the front wheels climbs the obstacles at a low
speed [6].
Material properties and Finite Element
Analysis
In present study the CAD model was designed by
Catia and the model was tested by PVC material. this
material was good in strength for light weight
application like; photography. PVC material has 1,45
g/cm3 of density, 580 Mpa modulus of elasticity and
0.4 Poisson’s ratio. Figure 1 and 2 shows the 3-D
model and mesh model of the rocker bogie
mechanism respectively.
Figure 1: Rocker Bogie CAD model
Figure 2: Rocker Bogie Mesh model
Figure 3: Base fixed boundary condition
Figure 4: Axel fixed boundary condition
The main objective of this study was to find out the
resonance frequency of the considered bogie
mechanism. The modal analysis was carried out for
first six mode shape and the corresponding
deformation was calculated. By analyzing the model
with different fixed boundary condition the modal
analysis give the range for failure.
International Journal of Applied Engineering Research ISSN 0973-4562 Volume 14, Number 9, 2019 (Special Issue) © Research India Publications. http://www.ripublication.com
Page 210 of 214
Simulation Result
Base fixed boundary condition result
Figure 5: Mode shape for based fixed boundary condition
International Journal of Applied Engineering Research ISSN 0973-4562 Volume 14, Number 9, 2019 (Special Issue) © Research India Publications. http://www.ripublication.com
Page 211 of 214
Axel fixed boundary condition result
Figure 6: Mode shape for Axel fixed boundary condition
International Journal of Applied Engineering Research ISSN 0973-4562 Volume 14, Number 9, 2019 (Special Issue) © Research India Publications. http://www.ripublication.com
Page 212 of 214
Figure 7: first six mode frequency comparison
Figure 8: First six mode Total Deformation
comparison
Static structural analysis
The CAD model of the rocker bogie mechanism was
fixed at wheel axel as shown in figure 4. Furthermore
a static loading of 50 N was applied as shown in
figure 9, to check the static behavior.
Figure 9: Applied loading condition
The result of total deformation, stress and strain due
to 50 N loading was demonstrated in figure 10 to 12,
respectively.
Figure 10: Total deformation
Figure 11: Equivalent Stress
Figure 12: Equivalent Strain
Conclusion
The solid structure of the rocker bogie mechanism
was designed for analysis. The two different
boundary conditions were selected for the analysis to
determine the failure range. From the 7 we can see
that the failure frequency in fixed axel was less as
0
200
400
600
800
1000
1 2 3 4 5 6
Modeshape
Based fixedcondition
Axel fixedcondition
NaturalFrequency
0
100
200
300
400
500
600
700
800
900
1 2 3 4 5 6
Modeshape
Based fixedcondition
Axel fixedcondition
Total Deformation
International Journal of Applied Engineering Research ISSN 0973-4562 Volume 14, Number 9, 2019 (Special Issue) © Research India Publications. http://www.ripublication.com
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compare to the base fixed condition frequency. That
way 203.9Hz was the fundamental frequency of the
considered Rocker bogie mechanism. Furthermore
the result of the deformation, stress and strain was
under satisfactory condition. We can say that the
design is safe under light loading (50 N) condition.
References
[1] Hong-an Yang at al., Dynamic Rocker-Bogie: A
Stability Enhancement for High-Speed Traversal
International Journal of Robotics and Automation
(IJRA) Vol. 3, No. 3, September 2014, pp.
212~220 ISSN: 2089-4856
[2] A. Bhole, S. H. Turlapati, Raja shekhar V. S, J.
Dixit, S. V. Shah, Madhava Krishna K, “Design
of a Robust Stair Climbing Compliant Modular
Robot to Tackle Overhang on Stairs”
arXiv:1607.03077v1 [cs.RO], 11 Jul 2016.
[3] Dongkyu Choi at al., „Analysis method of
climbing stairs with the rocker-bogie
mechanism‟ , „Journal of Mechanical Science
and Technology‟ vol.27,issue 9 ,pp 2783-
2788,2016
[4] Brian D. Harrington and Chris Voorhees, The
Challenges of Designing the Rocker-Bogie
Suspension for the Mars Exploration Rover,
Proceedings of the 37th Aerospace Mechanisms
Symposium, Johnson Space Center, May 1921,
2004.
[5] Yadav, N., Bhardwaj, B., & Bhardwaj, S. (2015).
Design analysis of Rocker Bogie Suspension
System and Access the possibility to implement
in Front Loading Vehicles. IOSR Journal of
Mechanical and Civil Engineering (IOSR-JMCE),
12(3), 64-67.
[6] Brian D. Harrington and Chris Voorhees, The
Challenges of Designing the Rocker-Bogie
Suspension for the Mars Exploration Rover,
Proceedings of the 37th Aerospace Mechanisms
Symposium, Johnson Space Center, May 1921,
2004.
International Journal of Applied Engineering Research ISSN 0973-4562 Volume 14, Number 9, 2019 (Special Issue) © Research India Publications. http://www.ripublication.com
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