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International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 786
ANALYSIS OF ENERGY ABSORPTION TUBES (CRUSH CAN)
Upkar mane1, Prof. S.S. Mashyal2
1Post Graduate Student, Department of Mechanical Engineering, MMEC Belgaum, Karnataka, India
2Professor, Department of Mechanical Engineering, MMEC Belgaum, Karnataka, India
---------------------------------------------------------------------***---------------------------------------------------------------------
Abstract- Thin-walled Energy Absorption tube are
extensively used as energy absorbers in numerous automotive
and aerospace applications as a result of their higher energy
absorption capacity. Energy Absorption tube are connecting
between Front bumper and Dash Toe pan. They are one of the
structural members which will absorb high energiesin frontal
impact, so that impact energy won’t transmit to
driver/passengers.
Consider the energy absorption through dynamic impact,
Speed of impact & momentum ofimpactareinfluentialfactors.
The analysis has done quasi-staticanalysiswhereassomehave
gone for dynamic analysis. EnergyAbsorptiontubelength, and
tube cross-sectional aspect ratio, along with friction and
impacting mass on crashworthiness parameters such as
specific energy absorption contact time, peak force and crush
distance. The impact velocity is assumed to be constant at 15
m/s. The various section aluminum tubes analysiswascarried
out by using finite element analysis. After providing the
necessary interactions and performing meshing, the whole
model is run for dynamic explicit code using LS DYNA.
Key Words- CAD, FEA, Crash Analysis
1.INTRODUCTION
Safety of the occupants of vehicles has continuously been a
priority in automobile design. Earlier efforts during this
direction were focussedondevelopingsystemsand parts for
preventing accidents. Future stage of development was to
make a safer close for restrained occupants. Post1960, with
legislated safety rules, crashworthiness of automobile
structure became focus of attention. Saving of vehicles
additionalattention. Saving of vehicles additional necessitate
d development of novel structural designs to
boost occupier safety. One of the
structural designs used conspicuously for controlling slowin
g and energy absorption consists of tubes destined within
the longitudinal direction. Withinthe eventofa frontal crash,
these tubes, subjected to compressive axial loading, fail
through through crippling of the walls and corners. Energy
dissipated during this processhelpsreduce kinetic energy of
the vehicle, and ultimately brings it to a stop. Post-crippling
kinematics of the tube and resisting load generated by it
depends on geometric dimensionsofthe cross-sectional and
yield strength of the material. A typical tube deformation
pattern and corresponding load-time characteristics for a
crush underdynamicloading. Slowing ofthevehicledepends
on this force. Since potential of injuries to occupants,
either due to restraint force or impact with the inside, is
directly proportional to vehicle slowing, limiting magnitude
of this force may be a key goal in design. Design of
those tubes involves correct proportioning of 2 sides of
rectangular cross-sectional, wall thicknesses and
corner geometry and non-linear properties of the material.
With no easy analytical answer out there for this
complicated drawback, in earlier years, designersdepended
heavily on testing tocomeback upwith neededtube designs.
This was a protracted, tedious andcostlyprocessprototypes
testing.
The crash of a car is nowadays of great important. Strict
standards have to be compelled to be adhered to within
the trade, above all to guard human life. The aim to improve
better performance, the design variables of vehicles
and higher protection capabilities for driver and
passengers.
So on decrease design time, Reduce Prototype and
Improve design standards of crashandcrush ofvehicles, and
components, tests are generally performed in numerical
simulations. The crash and crush analysisortests results are
used for entire improvement of a replacement design. The
FEA simulation results whereas not manufacturing any
physical model, and should be performed quickly. This
enables Design optimisation of the vehicle
components before an physical model of the
vehicle must be built. The foremost necessary
development is to absorb the kinetic energy during a crash
situation . Crash tubes are designed for absorb max. kinetic
energy and convert max kinetic energy into plastic strain
energy under different loading conditions. During the axial
crashing and crushing behaviour of tubes or structure.
1.1 FEA Analysis
This paper presents the FEA of the Energy absorption
tubes of a passenger car. Front rails connect between Dash
Toe pan and Front bumper. It is a structural memberswhich
will absorb high kinetic energy during front impact, so that
impact energy won’t transmit to driver/passengers. The
material is used for rails Steel. The whole meshing, deck
preparation and the solution is run in dynamic explicit code
using ABAQUS 6.11 PR3. The resultsofKineticEnergy,Strain
Energy, Total Energy andInternal Energyarecomparedwith
that of standard square tube. It was found that Kinetic
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 787
Energy decreased with time, Internal Energy increasedwith
time, and Total Energy of the system remained the same.
The SEA is calculated for two different velocities i.e. at 20
and 30 mph and different material aluminium and steel.
2. OBJECTIVE AND SCOPE OF THE WORK
2.1 Objective of Project
 The objective of this projectis tofind the effectof
impact on different types of Energy Absorption
tubes.
 Ability of vehicle structure and Subsystems to
guard the occupants in survivable Crashes
with affordable slowing pulse.
 Restrain system give extra protection to
reduce injury to occupier.
 To investigate effect axial crush behavior of

 various structures energy absorption aluminium
tubes through finite element analysis and
experimen
2.2 Scope of Project:
•Study of Energy Absorption tubes
•Design of Energy Absorption tubes
•Finite element Meshing, loading, boundary conditions etc.
• Finite element Analysis
2.3 FE Model-
The CAD geometry of crush can as shown in fig 4.2 is
imported as an input in <.stp> form into Hypermesh for the
preparation of meshing. The sensitive region has been
remeshed by manually considering shape and size of part.
3D model is prepared by using Pro-W Creo2.0. The CAD
Model of Crash tube specification is Length-200mm, Width-
38.1mm, Height- 63.5mm and thickness 1.6mm.
Fig -1: Schematic of a CAD model
2.2.1 Meshing Details
The 3d cad geometry prepare in ProE creo2.0 and export
in .stp and then import in hypermesh and prepare for
meshing. Parabolic quaditateral element is used for
analysis.
Fig-2: meshing model
CAD model in .igs file format is imported in HyperMesh.
2D Quad meshing is carried out on surfacesofthe geometry.
The element size chosen is 4mm.
no. of element- 2466
no. of nodes-2552
2.4Quality Criteria
Quality Parameter Allowable Quad Meshing
1. maximum aspect ratio < 5
2. maximum Warpage Angle < 10
3. Minimum Quads < 45
4. Maximum Quads < 135
5. Minimum Tria < 15
6. Maximum Tria < 120
Warpage
Aspect Ratio
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 788
Skew
Jocobian
2.5 Material Properties
Material is one of the important properties that define the
behaviour of geometry. An aluminium material was wont
to describe the material behaviour of Tubes in dynamic
analysis.
Material properties used are described below
For Tubes – aluminium Al6063
Young’s modulus = E= 6.9×10e4MPa,
Poisson ratio = μ =0.33,
Density of steel = ρ = 2.8×10e-9 tons/mm3
Yield strength= 210MPa
Ultimate strength= 234MPa
% of elongation= 12.8
2.6 Boundary Conditions:
The boundary condition that's used here includes totally
different kind of loads,i.e.Constraints,supportsorboundary
field specification. The Aluminiumtubeone endisconstraint
in all rotational and translational dof of all nodes on tube
edge (rigid body). The another end of aluminium
tube can constraint in five degree of freedom which
can move axially towards the fixed plate or
except the direction of the moving impact. At the fixed end
reactions is calculated and other end on (moving plate)
impactor.
Fig-3: Loading
The Impactor was modelled only linear displacement is
allowable can move axially towards the fixed plate. Other
linear and rotational dof are constraint. The energy
absorbing structure is capable to absorbing max crash
energy can be absorbed bytwoaluminiumtubesismuchless
than 50 %.
Chart-1: Prescribed displacement of 150mm Given to
movable platen in the direction of Tube axis.
3. RESULTS
3.1 Square Section
Dynamic explicit analysis on the passenger car
aluminium crush can at velocities15m/s. when theaccident
or front impact of energy absorption tubes at the
displacement determined was a hundred and
fifty millimetre.
Axial deflection structural behaviour of the crash can
subjected to the initial speed of 15 m/s. The deflection
obtained from FEA solutions are shown in Figure and
validate with the experimental testing. within
the explicit solution, the collapse at the highest has been
predicted but the deformations close to the centre of the
tube. Energy absorb by axial loading is higher than oblique
loading because axial loading subjected to bending and
compressive nature.
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 789
Chart-2: Energy Graph
Chart-3: Force vs. Time
Fig-4: Displacement Contour plot
Fig-5: Von-mises stress contour plot
Results:-
Peak Initial crush force=73.8kN
3.2 Circular Section
Fig-6: Meshing model
Chart-4:EnergyGraph
Chart-5-: Force vs. Time
Fig-7 : Displacement Contour plot
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 790
Fig-8: Von-mises stress contour plot
Results:-
Peak Initial crush force=205kN
3.3 Rectangular Section
Fig-9: Meshing model
Chart-6: Energy Graph
Chart-7: Force vs. Time
Fig-10 : Displacement Contour plot
Fig-11: Vonmises stress contour plot
Results:-
Peak Initial crush force=138kN
3.4 Square with holes Section
Fig-11: Meshing model
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 791
Chart-8: Energy Graph
Chart-9: Force vs. Time
Fig-12: Displacement Contour plot
Fig-13: Vonmises stress contour plot
Results:-
Peak Initial crush force=190Kn
4. Experiment
4.1 Experimental Testing
There are two failure criteria descrbed for crush
can crash test standards.
The first criteria is that fracture or buckling occurs and
second criteria is progressive crush.Requirement: Crushing
behaviour during impact. Failure will be defined as any
permanent deformation, fracture, breakage, loosening or
other inability to mechanical function.
Fig-14:Schematic of Impact Test Machine
4.2 Experimental setup:
A UTM (universal testing machine) is used for
standard tensile and compressive strength of material. The
crush can is mounted on machine fixture and extensometer
is placed to record displacement or changeinlengthofcrush
can during experimentation. Once the crush can is fix the
impact load is applied on crush can by UTM and data
acquisition system give the output of load, tensile or
compression of crush can.
Fig-15:Test Setup
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 792
Fig-16:Test Sample
As shown in above Fig. UTM and Aluminium Test sample.
Energy absorption tube is fixed in a fixture. A Impact force
is applied in the axial direction.
Fig-17:Deformation Modes of Energy Absorbers
Table -1 Result
Results
Original Guage
length(mm) 50
Final guage
length(mm) 56.4
Pre Load(%) 0.2
Machine Capacity
(KN) 600
Specimen Type Flat
Thickness (mm) 3mm
5. CONCLUSION:-
From the analytical and experimental investigation on
Energy absorption tube. Circular and rectangular tubes
have similar load-displacements curves under axial
loading where the axial force first reaches the initial peak
which is then followed by a drop and fluctuating mean
force.
 As expected initial crush achieved at higher load
followed by progressive crush
 at lower load.
 Folding pattern is purely axial which is desirable
for maximum energy absorption.
 Physical Test will be carried out to validate with
FEA
The square aluminium tube more energy absorb by
reducing the initial peak force and increasing the precise
crash absorption duringimpactoraxial loading.Tominimize
the initial peak force to avoid and reduce the unwanted
damage and harm to occupant.
The energy absorption of the crushcan duringimpactor
crash are depend on collapse modes. Folding pattern is
purely axial which is desirable for maximum energy
absorption.
REFERENCES
[1] P. Khalili, F. Tarlochan, A.M.S. Hamouda and K. Al –
Khalifa, “Energy absorption capability of thin-
walled aluminium tubes under crash loading”,
Journal of Mechanical Engineering and Sciences.
[2] Zafer Kazancı a,b,*, Klaus-Jürgen Bathe,“ Crushing
and crashing of tubes with implicit time
integration”, International Journal of Impact
Engineering(2012).
[3] Piyush Dube, M. L. J. Suman, *Vinod Banthia,
“Lumped Parameter Model for Design of Crash
Energy Absorption Tubes”.
[4] F. Tarlochan, Samer. F, “Design Of Thin Wall
Structures For Energy Absorption Applications:
Design For Crash Injuries Mitigation Using
Magnesium Alloy”, International Journal of
Research in Engineering and Technology.
[5] Raymond Joseph, Dr. M.A. Kamoji “Crash Analysis
for Energy Absorption of Frontal Rails of a
Passenger Car.” International Research Journal of
Engineering and Technology.
[6] Nitin S Gokhale “Practical Finite Element
Analysis” (2008).
International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056
Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072
© 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 793
BIOGRAPHIES
Mr.Upkar Dattatray Mane post
graduate student of the Dept. of
Mechanical Engg, Maratha Mandal
Engineering College Belgaum. Area of
Interest in machine design,
Manufacturing Tech.
Proff. S.S. mashyal is a HOD in the
Dept. of Mechanical Engg, Maratha
Mandal Engineering College, Belgaum.
His areas of interest include machine
design, Manufacturing Tech.

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Analysis of Energy Absorption Tubes (Crush Can)

  • 1. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 786 ANALYSIS OF ENERGY ABSORPTION TUBES (CRUSH CAN) Upkar mane1, Prof. S.S. Mashyal2 1Post Graduate Student, Department of Mechanical Engineering, MMEC Belgaum, Karnataka, India 2Professor, Department of Mechanical Engineering, MMEC Belgaum, Karnataka, India ---------------------------------------------------------------------***--------------------------------------------------------------------- Abstract- Thin-walled Energy Absorption tube are extensively used as energy absorbers in numerous automotive and aerospace applications as a result of their higher energy absorption capacity. Energy Absorption tube are connecting between Front bumper and Dash Toe pan. They are one of the structural members which will absorb high energiesin frontal impact, so that impact energy won’t transmit to driver/passengers. Consider the energy absorption through dynamic impact, Speed of impact & momentum ofimpactareinfluentialfactors. The analysis has done quasi-staticanalysiswhereassomehave gone for dynamic analysis. EnergyAbsorptiontubelength, and tube cross-sectional aspect ratio, along with friction and impacting mass on crashworthiness parameters such as specific energy absorption contact time, peak force and crush distance. The impact velocity is assumed to be constant at 15 m/s. The various section aluminum tubes analysiswascarried out by using finite element analysis. After providing the necessary interactions and performing meshing, the whole model is run for dynamic explicit code using LS DYNA. Key Words- CAD, FEA, Crash Analysis 1.INTRODUCTION Safety of the occupants of vehicles has continuously been a priority in automobile design. Earlier efforts during this direction were focussedondevelopingsystemsand parts for preventing accidents. Future stage of development was to make a safer close for restrained occupants. Post1960, with legislated safety rules, crashworthiness of automobile structure became focus of attention. Saving of vehicles additionalattention. Saving of vehicles additional necessitate d development of novel structural designs to boost occupier safety. One of the structural designs used conspicuously for controlling slowin g and energy absorption consists of tubes destined within the longitudinal direction. Withinthe eventofa frontal crash, these tubes, subjected to compressive axial loading, fail through through crippling of the walls and corners. Energy dissipated during this processhelpsreduce kinetic energy of the vehicle, and ultimately brings it to a stop. Post-crippling kinematics of the tube and resisting load generated by it depends on geometric dimensionsofthe cross-sectional and yield strength of the material. A typical tube deformation pattern and corresponding load-time characteristics for a crush underdynamicloading. Slowing ofthevehicledepends on this force. Since potential of injuries to occupants, either due to restraint force or impact with the inside, is directly proportional to vehicle slowing, limiting magnitude of this force may be a key goal in design. Design of those tubes involves correct proportioning of 2 sides of rectangular cross-sectional, wall thicknesses and corner geometry and non-linear properties of the material. With no easy analytical answer out there for this complicated drawback, in earlier years, designersdepended heavily on testing tocomeback upwith neededtube designs. This was a protracted, tedious andcostlyprocessprototypes testing. The crash of a car is nowadays of great important. Strict standards have to be compelled to be adhered to within the trade, above all to guard human life. The aim to improve better performance, the design variables of vehicles and higher protection capabilities for driver and passengers. So on decrease design time, Reduce Prototype and Improve design standards of crashandcrush ofvehicles, and components, tests are generally performed in numerical simulations. The crash and crush analysisortests results are used for entire improvement of a replacement design. The FEA simulation results whereas not manufacturing any physical model, and should be performed quickly. This enables Design optimisation of the vehicle components before an physical model of the vehicle must be built. The foremost necessary development is to absorb the kinetic energy during a crash situation . Crash tubes are designed for absorb max. kinetic energy and convert max kinetic energy into plastic strain energy under different loading conditions. During the axial crashing and crushing behaviour of tubes or structure. 1.1 FEA Analysis This paper presents the FEA of the Energy absorption tubes of a passenger car. Front rails connect between Dash Toe pan and Front bumper. It is a structural memberswhich will absorb high kinetic energy during front impact, so that impact energy won’t transmit to driver/passengers. The material is used for rails Steel. The whole meshing, deck preparation and the solution is run in dynamic explicit code using ABAQUS 6.11 PR3. The resultsofKineticEnergy,Strain Energy, Total Energy andInternal Energyarecomparedwith that of standard square tube. It was found that Kinetic
  • 2. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 787 Energy decreased with time, Internal Energy increasedwith time, and Total Energy of the system remained the same. The SEA is calculated for two different velocities i.e. at 20 and 30 mph and different material aluminium and steel. 2. OBJECTIVE AND SCOPE OF THE WORK 2.1 Objective of Project  The objective of this projectis tofind the effectof impact on different types of Energy Absorption tubes.  Ability of vehicle structure and Subsystems to guard the occupants in survivable Crashes with affordable slowing pulse.  Restrain system give extra protection to reduce injury to occupier.  To investigate effect axial crush behavior of   various structures energy absorption aluminium tubes through finite element analysis and experimen 2.2 Scope of Project: •Study of Energy Absorption tubes •Design of Energy Absorption tubes •Finite element Meshing, loading, boundary conditions etc. • Finite element Analysis 2.3 FE Model- The CAD geometry of crush can as shown in fig 4.2 is imported as an input in <.stp> form into Hypermesh for the preparation of meshing. The sensitive region has been remeshed by manually considering shape and size of part. 3D model is prepared by using Pro-W Creo2.0. The CAD Model of Crash tube specification is Length-200mm, Width- 38.1mm, Height- 63.5mm and thickness 1.6mm. Fig -1: Schematic of a CAD model 2.2.1 Meshing Details The 3d cad geometry prepare in ProE creo2.0 and export in .stp and then import in hypermesh and prepare for meshing. Parabolic quaditateral element is used for analysis. Fig-2: meshing model CAD model in .igs file format is imported in HyperMesh. 2D Quad meshing is carried out on surfacesofthe geometry. The element size chosen is 4mm. no. of element- 2466 no. of nodes-2552 2.4Quality Criteria Quality Parameter Allowable Quad Meshing 1. maximum aspect ratio < 5 2. maximum Warpage Angle < 10 3. Minimum Quads < 45 4. Maximum Quads < 135 5. Minimum Tria < 15 6. Maximum Tria < 120 Warpage Aspect Ratio
  • 3. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 788 Skew Jocobian 2.5 Material Properties Material is one of the important properties that define the behaviour of geometry. An aluminium material was wont to describe the material behaviour of Tubes in dynamic analysis. Material properties used are described below For Tubes – aluminium Al6063 Young’s modulus = E= 6.9×10e4MPa, Poisson ratio = μ =0.33, Density of steel = ρ = 2.8×10e-9 tons/mm3 Yield strength= 210MPa Ultimate strength= 234MPa % of elongation= 12.8 2.6 Boundary Conditions: The boundary condition that's used here includes totally different kind of loads,i.e.Constraints,supportsorboundary field specification. The Aluminiumtubeone endisconstraint in all rotational and translational dof of all nodes on tube edge (rigid body). The another end of aluminium tube can constraint in five degree of freedom which can move axially towards the fixed plate or except the direction of the moving impact. At the fixed end reactions is calculated and other end on (moving plate) impactor. Fig-3: Loading The Impactor was modelled only linear displacement is allowable can move axially towards the fixed plate. Other linear and rotational dof are constraint. The energy absorbing structure is capable to absorbing max crash energy can be absorbed bytwoaluminiumtubesismuchless than 50 %. Chart-1: Prescribed displacement of 150mm Given to movable platen in the direction of Tube axis. 3. RESULTS 3.1 Square Section Dynamic explicit analysis on the passenger car aluminium crush can at velocities15m/s. when theaccident or front impact of energy absorption tubes at the displacement determined was a hundred and fifty millimetre. Axial deflection structural behaviour of the crash can subjected to the initial speed of 15 m/s. The deflection obtained from FEA solutions are shown in Figure and validate with the experimental testing. within the explicit solution, the collapse at the highest has been predicted but the deformations close to the centre of the tube. Energy absorb by axial loading is higher than oblique loading because axial loading subjected to bending and compressive nature.
  • 4. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 789 Chart-2: Energy Graph Chart-3: Force vs. Time Fig-4: Displacement Contour plot Fig-5: Von-mises stress contour plot Results:- Peak Initial crush force=73.8kN 3.2 Circular Section Fig-6: Meshing model Chart-4:EnergyGraph Chart-5-: Force vs. Time Fig-7 : Displacement Contour plot
  • 5. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 790 Fig-8: Von-mises stress contour plot Results:- Peak Initial crush force=205kN 3.3 Rectangular Section Fig-9: Meshing model Chart-6: Energy Graph Chart-7: Force vs. Time Fig-10 : Displacement Contour plot Fig-11: Vonmises stress contour plot Results:- Peak Initial crush force=138kN 3.4 Square with holes Section Fig-11: Meshing model
  • 6. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 791 Chart-8: Energy Graph Chart-9: Force vs. Time Fig-12: Displacement Contour plot Fig-13: Vonmises stress contour plot Results:- Peak Initial crush force=190Kn 4. Experiment 4.1 Experimental Testing There are two failure criteria descrbed for crush can crash test standards. The first criteria is that fracture or buckling occurs and second criteria is progressive crush.Requirement: Crushing behaviour during impact. Failure will be defined as any permanent deformation, fracture, breakage, loosening or other inability to mechanical function. Fig-14:Schematic of Impact Test Machine 4.2 Experimental setup: A UTM (universal testing machine) is used for standard tensile and compressive strength of material. The crush can is mounted on machine fixture and extensometer is placed to record displacement or changeinlengthofcrush can during experimentation. Once the crush can is fix the impact load is applied on crush can by UTM and data acquisition system give the output of load, tensile or compression of crush can. Fig-15:Test Setup
  • 7. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 792 Fig-16:Test Sample As shown in above Fig. UTM and Aluminium Test sample. Energy absorption tube is fixed in a fixture. A Impact force is applied in the axial direction. Fig-17:Deformation Modes of Energy Absorbers Table -1 Result Results Original Guage length(mm) 50 Final guage length(mm) 56.4 Pre Load(%) 0.2 Machine Capacity (KN) 600 Specimen Type Flat Thickness (mm) 3mm 5. CONCLUSION:- From the analytical and experimental investigation on Energy absorption tube. Circular and rectangular tubes have similar load-displacements curves under axial loading where the axial force first reaches the initial peak which is then followed by a drop and fluctuating mean force.  As expected initial crush achieved at higher load followed by progressive crush  at lower load.  Folding pattern is purely axial which is desirable for maximum energy absorption.  Physical Test will be carried out to validate with FEA The square aluminium tube more energy absorb by reducing the initial peak force and increasing the precise crash absorption duringimpactoraxial loading.Tominimize the initial peak force to avoid and reduce the unwanted damage and harm to occupant. The energy absorption of the crushcan duringimpactor crash are depend on collapse modes. Folding pattern is purely axial which is desirable for maximum energy absorption. REFERENCES [1] P. Khalili, F. Tarlochan, A.M.S. Hamouda and K. Al – Khalifa, “Energy absorption capability of thin- walled aluminium tubes under crash loading”, Journal of Mechanical Engineering and Sciences. [2] Zafer Kazancı a,b,*, Klaus-Jürgen Bathe,“ Crushing and crashing of tubes with implicit time integration”, International Journal of Impact Engineering(2012). [3] Piyush Dube, M. L. J. Suman, *Vinod Banthia, “Lumped Parameter Model for Design of Crash Energy Absorption Tubes”. [4] F. Tarlochan, Samer. F, “Design Of Thin Wall Structures For Energy Absorption Applications: Design For Crash Injuries Mitigation Using Magnesium Alloy”, International Journal of Research in Engineering and Technology. [5] Raymond Joseph, Dr. M.A. Kamoji “Crash Analysis for Energy Absorption of Frontal Rails of a Passenger Car.” International Research Journal of Engineering and Technology. [6] Nitin S Gokhale “Practical Finite Element Analysis” (2008).
  • 8. International Research Journal of Engineering and Technology (IRJET) e-ISSN: 2395-0056 Volume: 04 Issue: 09 | Sep -2017 www.irjet.net p-ISSN: 2395-0072 © 2017, IRJET | Impact Factor value: 5.181 | ISO 9001:2008 Certified Journal | Page 793 BIOGRAPHIES Mr.Upkar Dattatray Mane post graduate student of the Dept. of Mechanical Engg, Maratha Mandal Engineering College Belgaum. Area of Interest in machine design, Manufacturing Tech. Proff. S.S. mashyal is a HOD in the Dept. of Mechanical Engg, Maratha Mandal Engineering College, Belgaum. His areas of interest include machine design, Manufacturing Tech.