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International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056
Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 109
Crash analysis of torque box beam column of an automobile vehicle
Sagar H N1 , Dr.B.Ravindra2
1 Department Of Mechanical Engineering Dr. Ambedkar Institute Of Technology Bangalore, India
2 Professor and HOD Department of Mechanical Engineering Dr. Ambedkar Institute of Technology
Bangalore, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract-Crash boxes otherthinwalledstructure whichis
mounted between automotive chassis and the bumper.
Geometric model of torque box beam column is done using
solid edge ST8 modelling tool. Once the geometry is created
as per specification and it is imported to ABAQUS for
meshing. This finite element model is imported to ABAQUS
explicitly to evaluate the explicit dynamic analysis
.segmented torque box beam columns are placed between
two rigid bodies at the top and bottom. But bottom rigid
bodies fixed completely it doesn’t have any motion in any
direction. The boundary condition for the top rigid body is
free to move in Y direction only and apply the velocity of 55
km per hour on column and evaluate the result.
Keywords— torque box beam column; crash
analysis;solid edge ST8; ABAQUS explicitly.
1. INTRODUCTION
Crash box is one of the passive safety components, because
of collision it undergoes deformation and it observes the
effect energy by the crash field itself. Crash containers are a
thin walled structures mounted among car chassis and
bumper (fig-1) which can be used as power absorption all
through crash event. Those factors play an essential role has
crash worthy machine and used to reduces the numerous
accidents due to frontal crash and additionally play a
function to soak up the impact strength of the frontal crash
by way of present process plastic deformation to shield the
occupants.
Figure- 1: Crash boxes positions mounted between
automotive chassis and bumper.
Because of friction, fraction, metal slicing, torsion, crushing,
cyclic plastic deformation, shear, Extension and fluid float
which thanks to friction, to power soak up were designed to
deplete electricity. a few of the entire above element the
number one energy absorbing mechanism are cyclic plastic
deformation, extension and friction.
Have a look at on two segments crash field remains
restricted, wherein this layout can possible to growth the
allowable crucial load and exceptional materials in every
phase may be used. The crash box designs the use of hybrid
cloth of aluminum and metallic had been developedasa way
to reduce crash container weight up to 17.5%.
.
Figure -2: Two segments crash box model.
1.1 Material
Mild metallic is used for the layout of torque container beam
column. It’s far an Iron-carbon alloy containing less than
0.25 percentage carbon which makes it more ductile and
much less hard as a result rendering it flawed for structural
work.
1.2 Problem Definition
The aim of this project is to study the impact of rigid body on
energy observing bumper column and optimize.
Therefore a crash simulation is performed and validated
using analytical method.
International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056
Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 110
And optimize the geometry of torque box bumper
column.Above configuration is optimized using TOSCA by
using the parameters given below
1. Connection angle between segments (θ) will be of the
range 0-90 degree of the interval of10 degree each.
2. Connection length between segments (p) will be varied
from 10-20mm of the interval 2mm.
3. Outside diameter (do) will be varied from 50-100mm of
the interval 10mm each.
4. Segment Height and thickness ratio will be constant
40/60mm and 2/3mm respectively.
2 Methodology
The primary step is to create a geometrical versionoftorque
container beam Column is performed the use of strong
aspect ST8 modeling tool. Rigid mass is modeled and
implemented with a pace equivalent to most speed
specification. That is impacted at the torque container beam
column. Once the geometryiscreatedasaccordingtospecsit
is imported into ABAQUS for messing.Thefinitedetail model
is ready by meshing it with suitable elements like linear
hexahedral, contact factors and constraining the version via
making use of cloth homes and boundary conditions. This
finite element model is imported to ABAQUS explicit to
evaluating the expressdynamic evaluationandsubsequently
results are analyzed and the effect damage is studied. The
response forces are located.
Following are the steps involved in Methodology:
Step1: The 3D model of the torque box beam Column is
done using Solid Edge ST8, created meshingandanalysishas
been done using ABAQUS/CAE.
Step 2: Rigid mass is modeled and applied with a velocity
equivalent to maximum speedspecification.Thisisimpacted
on the torque box beam column.
Step 3: Explicit dynamic analysis is performed using
ABAQUS/EXPLICIT.
Step 4: Results are analyzed and the impact damage is
studied. The reaction forces are observed.
2.1 Geometric Modeling
Figure 3 shows the geometric model of a section of the
torque box beam Column. The modelinghasbeendoneusing
SOLID EDGE ST8 modeling software. The dimensions of
torque box beam Column are considers from the literature
survey. It consists of two segment crash box which has the
Connection angle between segments (θ)of45degree.Design
parameters in two segments crash box is as shown in figure
3.
Figure -3: Design parameters in two segments crash box.
Figure- 4: Geometric models of two segments of crash box
2.2 Meshing
fig 5 suggests the Finite detail version generated for the
geometric model of the 2 segments of crash fieldusinglinear
hexahedral factors of kind C3D8R. those factors are selected
due to the fact the quadratic end result interpolation at the
combination point.
International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056
Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 111
Figure- 5: Mesh models of two segments of crash box
2.3 Loads and Boundary Conditions
Figure- 6: Application of loads and boundary condition
The segmented crash column is places between the 2
inflexible bodies at the top and backside. The lowest
inflexible frame is constant completely which would not
have any motion in any route. The Boundary condition for
the top inflexible body could be free to transport in Y axis
and constrained to X and Z axis.
The speed boundary conditionisgiventopinnaclerigidbody
in poor Y course with the importance of 15m/s. The top
inflexible body acts because the impact loads so that it will
be of an item moving at 55km/h on the column. The analysis
has been achieved in ABAQUS /CAE.
3 RESULTS & DISCUSSION
The FE model of torque box beam column with loads and
boundary conditions was run for analysis in ABAQUS. The
following figures give the results of both stress contour and
displacement contours.
3.1 Stress Contour
The figure 7 shows the stress in the segment box column
after the load is applied
Figure -7: stress in the segment box column
The above figures show the amount of strain inside the
section box column. As the pressure carried out from the
pinnacle rigid body the first phase tends to deform.
Maximum pressure of 522Mpa is inside the first phase and
the minimal stress attention is of for 43.5.5Mpa within the
second section. The evaluation shows the stress inside the
first section would not intrude pressurewithinthe2dphase.
3.2 Displacement Contour
Figure -8: total displacement in the segment box column
The above figures indicate the total displacement within the
phase whilst the burden is applied. The whole displacement
is the suggest of the preliminary role to final function of the
section. The maximum displacement inside the bad Y pathis
of 14.84mm which is red in shade. The yellow colorsuggests
the displacement in the variety of nine.891mm to 11.13mm.
all of the displacement is in the first section. Inside the
International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056
Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 112
second section there's very small displacement which is of
the range0-1.23mm displacement.
4 OPTIMISATION USING TOSCA
The Tosca optimisation suite built into ABAQUS/CAE
platform takes full advantage of any improvement potential
while leveraging advanced simulation capabilities.Itcreates
optimised design concepts to achieve the highest
performance and quality in shortest development time.
4.1 Optimization Results
Fig -9: Starin Graph
Graph suggests the tracking of goal feature and constraint
thru the optimisation steps. It shows convergence to the
satisfactory possible answer. With up to 60% of the weight
reduction within the first segment. pressure power is inside
perfect limits.
4.2 Stress Counter
Fig-10: Stress In Segment
The above figures display the quantity of strain within the
section containercolumn.Astheforceimplementedfrom the
top inflexible frame the primary section tends to deform.
Maximum pressure of 382.7Mpa is withinthefirstphaseand
the minimal pressure attention is of 31.1Mpa within the 2d
phase. The analysis indicates the pressure within the first
section doesn't intervenepressurewithinthe2dsection.The
pressure cost is decreased after optimization.
4.3 Displacement Counter
Fig-11:Totale Displacement
The above figures shows the total displacement in the
segment when the load is applied.
Final Maximum displacement is 0.1 mm.
4.4 Topology of the Final Configuration of the
First Segment
Fig-12: Topology of the Final Configuration
5 CONCLUSION
 The maximum stress in the segment is found to
be 522 Mpa which exceeded the ultimate
strength of the material to failure. After the
optimisation, the stress reduced to ~345 Mpa.
International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056
Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 113
 The optimised stress is within ultimate limit
which will justundergoplastic deformationand
avoid permanent failure.
 Displacements are found to followtheexpected
buckling pattern in explicit dynamic analysis.
 Total Energy is absorbed by the first segment
crash box by affecting the rollup of the segment
and doesn’t intrude inside the second segment.
 Total 60 % of first segment weight is reduced
by this topology optimisation process.
SCOPE OF FUTURE WORK
Connection angle between the segment change to 300,
variation of diametrical ratio,thicknessvariation,change the
material like aluminum because too much malleable, use
metal -metal composite. And go forotheranalysislikedesign
response from exist, static analysis, strain energy design
response etc.
REFERENCE
[1] A survey paper on factors controlling the energy
absorption of crash box” by Ashutosh S. Kalshetti,
Sanjaysingh Vijaysingh Patil, Associate professor,
Department of Mechanical EngineeringRMDSinhgadSchool
of Engineering.
[2] “Application of analytical hierarchy processinthedesign
concept selection of automotive composite bumper beam
during the conceptual design stage”, by A. Hambali1, S. M.
Sapuan1, N. Ismail1 and Y. Nukman2, Malaysia.
[3] “Simulation of Automobile Side Member Collapse For
Crash Energy Management”
[4] “Experimental InvestigationswithCrushBoxSimulations
for Different Segment Cars using LS-DYNA”by A.Siva Kumar
Ȧ*, G.Himabindu Ȧ, M.Sankar Raman Ȧ and K.Vijaya Kumar
Reddy Ḃ . India Accepted 10 January 2014, Available online
01 February 2014, Special Issue-2, (February 2014).
[5] “Simulation Of Automobile Side Member Collapse For
Crash Energy Management” By Ichiro Hagiwara,Masaaki
Tsuda,Vashihirosato And Yuichi Kitegawa, Nissan Moter Co
Pvt Ltd.
[6] “Lumped Parameter Model for Design of Crash Energy
Absorption Tubes” By Piyush Dube, M. L. J. Suman, Facultyof
Engineering and Technology, M. S. Ramaiah University of
Applied Sciences, Bangalore 560 054.
[7] “Design and Analysis of an Automotive Front Bumper
Beam for Low-Speed Impact” By MaheshkumarV.Dange, Dr.
Rajesh. B. Buktar, Dr. Nilesh. R. Raykar, Department of
Mechanical Engineering, Sardar Patel College of
Engineering/ Mumbai University, India.

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Crash Analysis of Torque Box Beam Column of an Automobile Vehicle

  • 1. International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056 Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 109 Crash analysis of torque box beam column of an automobile vehicle Sagar H N1 , Dr.B.Ravindra2 1 Department Of Mechanical Engineering Dr. Ambedkar Institute Of Technology Bangalore, India 2 Professor and HOD Department of Mechanical Engineering Dr. Ambedkar Institute of Technology Bangalore, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract-Crash boxes otherthinwalledstructure whichis mounted between automotive chassis and the bumper. Geometric model of torque box beam column is done using solid edge ST8 modelling tool. Once the geometry is created as per specification and it is imported to ABAQUS for meshing. This finite element model is imported to ABAQUS explicitly to evaluate the explicit dynamic analysis .segmented torque box beam columns are placed between two rigid bodies at the top and bottom. But bottom rigid bodies fixed completely it doesn’t have any motion in any direction. The boundary condition for the top rigid body is free to move in Y direction only and apply the velocity of 55 km per hour on column and evaluate the result. Keywords— torque box beam column; crash analysis;solid edge ST8; ABAQUS explicitly. 1. INTRODUCTION Crash box is one of the passive safety components, because of collision it undergoes deformation and it observes the effect energy by the crash field itself. Crash containers are a thin walled structures mounted among car chassis and bumper (fig-1) which can be used as power absorption all through crash event. Those factors play an essential role has crash worthy machine and used to reduces the numerous accidents due to frontal crash and additionally play a function to soak up the impact strength of the frontal crash by way of present process plastic deformation to shield the occupants. Figure- 1: Crash boxes positions mounted between automotive chassis and bumper. Because of friction, fraction, metal slicing, torsion, crushing, cyclic plastic deformation, shear, Extension and fluid float which thanks to friction, to power soak up were designed to deplete electricity. a few of the entire above element the number one energy absorbing mechanism are cyclic plastic deformation, extension and friction. Have a look at on two segments crash field remains restricted, wherein this layout can possible to growth the allowable crucial load and exceptional materials in every phase may be used. The crash box designs the use of hybrid cloth of aluminum and metallic had been developedasa way to reduce crash container weight up to 17.5%. . Figure -2: Two segments crash box model. 1.1 Material Mild metallic is used for the layout of torque container beam column. It’s far an Iron-carbon alloy containing less than 0.25 percentage carbon which makes it more ductile and much less hard as a result rendering it flawed for structural work. 1.2 Problem Definition The aim of this project is to study the impact of rigid body on energy observing bumper column and optimize. Therefore a crash simulation is performed and validated using analytical method.
  • 2. International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056 Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 110 And optimize the geometry of torque box bumper column.Above configuration is optimized using TOSCA by using the parameters given below 1. Connection angle between segments (θ) will be of the range 0-90 degree of the interval of10 degree each. 2. Connection length between segments (p) will be varied from 10-20mm of the interval 2mm. 3. Outside diameter (do) will be varied from 50-100mm of the interval 10mm each. 4. Segment Height and thickness ratio will be constant 40/60mm and 2/3mm respectively. 2 Methodology The primary step is to create a geometrical versionoftorque container beam Column is performed the use of strong aspect ST8 modeling tool. Rigid mass is modeled and implemented with a pace equivalent to most speed specification. That is impacted at the torque container beam column. Once the geometryiscreatedasaccordingtospecsit is imported into ABAQUS for messing.Thefinitedetail model is ready by meshing it with suitable elements like linear hexahedral, contact factors and constraining the version via making use of cloth homes and boundary conditions. This finite element model is imported to ABAQUS explicit to evaluating the expressdynamic evaluationandsubsequently results are analyzed and the effect damage is studied. The response forces are located. Following are the steps involved in Methodology: Step1: The 3D model of the torque box beam Column is done using Solid Edge ST8, created meshingandanalysishas been done using ABAQUS/CAE. Step 2: Rigid mass is modeled and applied with a velocity equivalent to maximum speedspecification.Thisisimpacted on the torque box beam column. Step 3: Explicit dynamic analysis is performed using ABAQUS/EXPLICIT. Step 4: Results are analyzed and the impact damage is studied. The reaction forces are observed. 2.1 Geometric Modeling Figure 3 shows the geometric model of a section of the torque box beam Column. The modelinghasbeendoneusing SOLID EDGE ST8 modeling software. The dimensions of torque box beam Column are considers from the literature survey. It consists of two segment crash box which has the Connection angle between segments (θ)of45degree.Design parameters in two segments crash box is as shown in figure 3. Figure -3: Design parameters in two segments crash box. Figure- 4: Geometric models of two segments of crash box 2.2 Meshing fig 5 suggests the Finite detail version generated for the geometric model of the 2 segments of crash fieldusinglinear hexahedral factors of kind C3D8R. those factors are selected due to the fact the quadratic end result interpolation at the combination point.
  • 3. International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056 Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 111 Figure- 5: Mesh models of two segments of crash box 2.3 Loads and Boundary Conditions Figure- 6: Application of loads and boundary condition The segmented crash column is places between the 2 inflexible bodies at the top and backside. The lowest inflexible frame is constant completely which would not have any motion in any route. The Boundary condition for the top inflexible body could be free to transport in Y axis and constrained to X and Z axis. The speed boundary conditionisgiventopinnaclerigidbody in poor Y course with the importance of 15m/s. The top inflexible body acts because the impact loads so that it will be of an item moving at 55km/h on the column. The analysis has been achieved in ABAQUS /CAE. 3 RESULTS & DISCUSSION The FE model of torque box beam column with loads and boundary conditions was run for analysis in ABAQUS. The following figures give the results of both stress contour and displacement contours. 3.1 Stress Contour The figure 7 shows the stress in the segment box column after the load is applied Figure -7: stress in the segment box column The above figures show the amount of strain inside the section box column. As the pressure carried out from the pinnacle rigid body the first phase tends to deform. Maximum pressure of 522Mpa is inside the first phase and the minimal stress attention is of for 43.5.5Mpa within the second section. The evaluation shows the stress inside the first section would not intrude pressurewithinthe2dphase. 3.2 Displacement Contour Figure -8: total displacement in the segment box column The above figures indicate the total displacement within the phase whilst the burden is applied. The whole displacement is the suggest of the preliminary role to final function of the section. The maximum displacement inside the bad Y pathis of 14.84mm which is red in shade. The yellow colorsuggests the displacement in the variety of nine.891mm to 11.13mm. all of the displacement is in the first section. Inside the
  • 4. International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056 Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 112 second section there's very small displacement which is of the range0-1.23mm displacement. 4 OPTIMISATION USING TOSCA The Tosca optimisation suite built into ABAQUS/CAE platform takes full advantage of any improvement potential while leveraging advanced simulation capabilities.Itcreates optimised design concepts to achieve the highest performance and quality in shortest development time. 4.1 Optimization Results Fig -9: Starin Graph Graph suggests the tracking of goal feature and constraint thru the optimisation steps. It shows convergence to the satisfactory possible answer. With up to 60% of the weight reduction within the first segment. pressure power is inside perfect limits. 4.2 Stress Counter Fig-10: Stress In Segment The above figures display the quantity of strain within the section containercolumn.Astheforceimplementedfrom the top inflexible frame the primary section tends to deform. Maximum pressure of 382.7Mpa is withinthefirstphaseand the minimal pressure attention is of 31.1Mpa within the 2d phase. The analysis indicates the pressure within the first section doesn't intervenepressurewithinthe2dsection.The pressure cost is decreased after optimization. 4.3 Displacement Counter Fig-11:Totale Displacement The above figures shows the total displacement in the segment when the load is applied. Final Maximum displacement is 0.1 mm. 4.4 Topology of the Final Configuration of the First Segment Fig-12: Topology of the Final Configuration 5 CONCLUSION  The maximum stress in the segment is found to be 522 Mpa which exceeded the ultimate strength of the material to failure. After the optimisation, the stress reduced to ~345 Mpa.
  • 5. International Research Journal of Engineering and Technology (IRJET) e- ISSN: 2395- 0056 Volume: 04 Issue: 08 | Aug -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 113  The optimised stress is within ultimate limit which will justundergoplastic deformationand avoid permanent failure.  Displacements are found to followtheexpected buckling pattern in explicit dynamic analysis.  Total Energy is absorbed by the first segment crash box by affecting the rollup of the segment and doesn’t intrude inside the second segment.  Total 60 % of first segment weight is reduced by this topology optimisation process. SCOPE OF FUTURE WORK Connection angle between the segment change to 300, variation of diametrical ratio,thicknessvariation,change the material like aluminum because too much malleable, use metal -metal composite. And go forotheranalysislikedesign response from exist, static analysis, strain energy design response etc. REFERENCE [1] A survey paper on factors controlling the energy absorption of crash box” by Ashutosh S. Kalshetti, Sanjaysingh Vijaysingh Patil, Associate professor, Department of Mechanical EngineeringRMDSinhgadSchool of Engineering. [2] “Application of analytical hierarchy processinthedesign concept selection of automotive composite bumper beam during the conceptual design stage”, by A. Hambali1, S. M. Sapuan1, N. Ismail1 and Y. Nukman2, Malaysia. [3] “Simulation of Automobile Side Member Collapse For Crash Energy Management” [4] “Experimental InvestigationswithCrushBoxSimulations for Different Segment Cars using LS-DYNA”by A.Siva Kumar Ȧ*, G.Himabindu Ȧ, M.Sankar Raman Ȧ and K.Vijaya Kumar Reddy Ḃ . India Accepted 10 January 2014, Available online 01 February 2014, Special Issue-2, (February 2014). [5] “Simulation Of Automobile Side Member Collapse For Crash Energy Management” By Ichiro Hagiwara,Masaaki Tsuda,Vashihirosato And Yuichi Kitegawa, Nissan Moter Co Pvt Ltd. [6] “Lumped Parameter Model for Design of Crash Energy Absorption Tubes” By Piyush Dube, M. L. J. Suman, Facultyof Engineering and Technology, M. S. Ramaiah University of Applied Sciences, Bangalore 560 054. [7] “Design and Analysis of an Automotive Front Bumper Beam for Low-Speed Impact” By MaheshkumarV.Dange, Dr. Rajesh. B. Buktar, Dr. Nilesh. R. Raykar, Department of Mechanical Engineering, Sardar Patel College of Engineering/ Mumbai University, India.