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International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
64
DESIGN ANALYSIS OF BUMPER BEAM SUBJECTED TO
OFFSET IMPACT LOADING FOR AUTOMOTIVE
APPLICATIONS
P. Sampath Rao
Professor, Mechanical Engineering Department,
Vijay Rural Eng. College, Nizamabad, T.S. INDIA.
S.Saikumar
M.Tech Student Mechanical Engineering Department,
Vijay Rural Eng. College, Nizamabad, T.S. INDIA
ABSTRACT
The bumper beam is fixed to front portion of the automobile structure and it is one of the
primary component which undergoes damage and transfers the forces to the rest of the structure.
Thus the modern bumper beam systems should play a key part in the safety concept of an
automobile, ensuring that minimal accelerations are transferred to the passenger. Further the
automotive producers are demanding for robust bumper beam systems showing good and
reproducible impact behavior. The objectives of this study were to increase the physical
understanding of the different phenomena taking place during the offset impact of an automotive
bumper beam-longitudinal system as well as to validate a modeling procedure for the system’s crash
performance. In presented work the attempt has been made with Simulation of forming process for
generating the FE-model of the bumper beam with required curvature. Finally the design and
analysis bumper beam subjected to offset impact loading with different materials using FE-code
ANSYS-LS DYNA and suggested the best material.
Keywords: Bumper Beam, FE-Model, Deflection and ANSYS-LS DYNA
1. INTRODUCTION
Fuel economy and emission gas regulations are the primary concerns in changing over to the
light weight materials in automotive structures. Aluminium alloys are extensively used in various
forms such as extrusions and castings due to its high strength to weight ratio and low density of
aluminum compared to steel. Thus for modern cars aluminum alloys are employed in the front and
INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING AND
TECHNOLOGY (IJMET)
ISSN 0976 – 6340 (Print)
ISSN 0976 – 6359 (Online)
Volume 6, Issue 5, May (2015), pp. 64-71
© IAEME: www.iaeme.com/IJMET.asp
Journal Impact Factor (2015): 8.8293 (Calculated by GISI)
www.jifactor.com
IJMET
© I A E M E
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
65
rear bumper beams, crash boxes, longitudinal-in the extruded form, also in other safety component
such as side door impact beams, frames engine cradles, chassis, and suspension components.
Although the use of the light weight materials helps in reducing fuel consumption and consequently
lower carbon dioxide emissions, another stringent demand from the society is the passive safety
obtained when employing light weight materials for automobile parts like bumper. Thin-walled tube-
like structures have been extensively studied as energy absorbing components by various researchers
and some of their opinions can be found in this literature.
The open literature available on bumper beam studies is vast and the majority of studies
carried out into bumper beam design have been related to the US protection requirements. The
structural performance of aluminum bumper beams is examined by Sharp M.L. et.al [4], from the
standpoint of local damage (i.e. resistance to denting and cracking),with regard to low-velocity
impact (8.3kmph).significant cost savings can be made of being able to damageability of proposed
bumper beam designs from “blue prints”. Tang S.C, [5], investigates computer modeling of bumper
beam impact resistance and Johnson W et.al [6] studied a series of selected car bumper beams by
quasi static loading at their mid-span, and showed that the assumption that a bumper beam could
deform through 102mm before the body of the vehicle would become damaged was an over-
estimate. However, the literature available on bumper beam systems connected to longitudinal is
rather limited or non-existing. In this direction the researchers Lademo O.-G [3] and Hanssen A.G
et.al [7] are studied the elastoplasticity and fracture for the material of aluminium alloys. Barlat F.,
[10] examine the Crystallographic texture, anisotropic yield surfaces and forming limits of sheet
metals found that the yield surface shape has a tremendous effect on the predicted failure limits.
The objectives of this current study were to increase the physical understanding of the
different phenomena taking place during the offset impact of an automotive bumper beam-
longitudinal system as well as to validate a modeling procedure for the system’s crash performance
.For that choose different materials and select the best material for manufacturing the bumper beam
longitudinal system from set of given materials. The objectives were achieved through FE code
ANSYS-DYNA.
2. RESEARCH METHODOLOGY
2.1 Identification of Problem
The problem studied is outlined in Fig. 1 where a trolley, with a given initial velocity and
mass, impacts the bumper beam-longitudinal system at 40% offset. The definition of 40% offset is
taken as the distance from the impact point to the extreme left end of the bumper beam. At impact,
the impact energy (kinetic energy) of the trolley is mainly absorbed in collapsing the bumper beam
as well as the longitudinal at the impacted end, i.e. impacted longitudinal. While the non-impacted
longitudinal experience only minor deformations.
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
66
Fig. 1. Bumper beam-longitudinal system at 40% offset impact.
2.2 Modeling and design of bumper beam
In the design process and crash assessment of vehicles Finite Element Method (FEM) is an
indispensable tool. It enables new design concepts to be evaluated where the optimum interaction
between materials and structural forms can be studied. The value of such numerical analysis is
strongly dependent on a precise description of the mechanical behavior of the material and also the
application of enhanced material models. This means, however, that the code has to be validated
against precision tests in the laboratory to ensure proper modeling of the member geometry,
boundary conditions, material properties and fracture. Thus, in order to establish a reliable
experimental database for the system in Figure 1 only few parameters were varied. The experimental
database was used for the development and validation of modeling procedures for the crash
performance of the bumper beam-longitudinal system with the use of the FE-code ANSYS-DYNA.
The numerical model should be able to predict the collapse mode with a high level of certainty in
order to ensure robust design. The modeling and design has been developed based on the assumption
of ffset impact.
2.3 Bumper beam Material analysis
The bumper beam front part of automobile subjected to different loads in service while in
impact, the selection of materials is important criteria, in this analysis chosen the material from
material library that is aluminum alloy materials AA6060-T1, AA7003-T1 and AA7003-T79 with
mechanical properties mentioned in following table 1
Table.1.Mechanical properties of aluminium alloy for Bumper beam
Property AA6060-T1 AA7003-T1 AA7003-T79
E Modulus of elasticity, Mpa 69500 70000 70500
G Modulus of rigidity, Mpa 26100 26200 26100
Poisson ratio 0.3 0.29 0.31
Ultimate tensile strength, Mpa 150 150 155
Shear stress, Mpa 95 95 95
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
67
3. ANALYSIS, RESULTS AND DISCUSSION
The presented work is design and analysis of bumper beam member for automotive
applications based on the topography optimization. In this investigation the analysis has been carried
out for select the best material for manufacturing the bumper beam longitudinal system from set of
given materials. The objective was achieved through FE code ANSYS-DYNA and results are
presented in table.2
Fig.2: Geometric model of bumper beam
longitudinal system with constraints
Fig.3: Finite element model of bumper beam
longitudinal system
Efforts were taken in constructing the numerical model of the bumper beam as similar as
possible to the reality. The bumper beam and all other components in the system were meshed in
order to make a precise model.
The figures 4 to 7 are shows the deformed shapes of the bumper beam at different time
intervals after impact for the material AA7003-T1.
Fig.4: Deformed shape of bumper beam
longitudinal system at 0.01 sec
Fig.5: Deformed shape of bumper beam
longitudinal system at 0.015 sec
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
68
Fig.6: Deformed shape of bumper beam
longitudinal system at 0.03 sec
Fig.7: Deformed shape of bumper beam
longitudinal system at 0.04 sec
The bumper beam longitudinal system shows maximum deformation at time t=0.015 sec i.e.,
when all the impact energy was absorbed. In the simulations the impact energy is converted to plastic
work.
The figures 8 to, 11 are shows the deformed shapes of the bumper beam at different time
intervals after impact for the material AA7003-T79.
Fig.8: Deformed shape of bumper beam
longitudinal system at 0.01 sec
Fig.9: Deformed shape of bumper beam
longitudinal system at 0.015 sec
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
69
Fig.10: Deformed shape of bumper beam
longitudinal system at 0.03 sec
Fig.11: Deformed shape of bumper beam
longitudinal system at 0.04 sec
The bumper beam longitudinal system shows maximum deformation at time t=0.015 sec i.e.,
when all the impact energy was absorbed. In the simulations the impact energy is converted to plastic
work.
The figures 12 to 15 are shows the deformed shapes of the bumper beam at different time
intervals after impact for the material AA6060-T1.
Fig.12: Deformed shape of bumper beam
longitudinal system at 0.01 sec
Fig.13: Deformed shape of bumper beam
longitudinal system at 0.015 sec
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
70
Fig.14: Deformed shape of bumper beam
longitudinal system at 0.03 sec
Fig.15: Deformed shape of bumper beam
longitudinal system at 0.04 sec
The bumper beam longitudinal shows maximum deformation at time t=0.015 sec i.e., when
all the impact energy was absorbed. In the simulations the impact energy is converted to plastic work
Table.2: Deflections of the bumper beam of different materials at different time intervals
Time(sec)
Dmx-AA7003(T1)
in mm
Dmx-AA7003(T79)
in mm
Dmx-AA6060(T1)
in mm
0.01 399.463 386.248 397.458
0.015 643.241 620.145 636.144
0.02 402.215 386.778 399.151
0.03 499.588 482.887 496.225
0.04 399.943 386.492 396.559
From all the deformation shapes observed AA7003-T79 shows less deformation for the given
load compared to other two alloys. From the table 2 it is clear that alloy AA7003-T79 is better
compared to alloys AA6060-T1 and AA7003-T1 for manufacturing the bumper beam longitudinal
system.
4. CONCLUSIONS
The presented research work is study the dynamic behavior of the bumper beam member by
changing the different materials and structural properties. In this scenario FEA model has been
generated through FE code ANSYS-DYNA for bumper beam member with the specified quality
criteria and analyzed for the optimized results. From the analysis following conclusions are
enumerated.
i. The AA7003-T79 shows high stiffness and plastic flow compared to AA7003-T1 and
AA6060-T1.
ii. AA7003-T79 shows 3% less deformation compared to AA6060-T1 and 2.4% less deformation
compared to AA7003-T1 for the given applied impact load.
iii. Velocities found on the bumper made of AA7003-T79 are less by 5% compared to AA6060-T1
and less by 15% compared to AA7003-T1, which implies that less energy is transferred to the
passengers.
International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print),
ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME
71
iv. Minimal Accelerations are transferred to the passengers in case of Bumper beam made with
AA7003-T79.
REFERENCES
1. Pugsley A and Macaulay M.A., Cars in collision-safe structures. New Scientist 78(596-598),
(1978).
2. Lademo O.-G., Berstad T., Hopperstad O.S. and Pedersen K.O. A numerical tool for
formability analysis of aluminium alloys. Part I: Theory. In: Proceedings of the 10th International
Conference on Metal Forming. Edited by Kusiak, Hartley, Majta, Pillinger and Pietrzyk,Steel
Grips, Suppl Metal Forming 2004, Kraków. (2004a).
3. Lademo O.-G. Engineering models of elastoplasticity and fracture for aluminium alloys. Dr.ing.
Thesis, Department of Structual Engineering, Norwegian University of Science and Technology,
Trondheim. ISBN 82-471-0367-2. (1999).
4. Sharp M.L., Jombock J.R. and Shabel B.S, Structural performance of aluminium bumpers.
SAE Paper No 780140, 569-575, (1978).
5. Tang S.C., Computer modeling of bumper impact resistance. SAE Paper No 790991, 3309-3319.
(1979).
6. Johnson W. and Walton A.C., An experimental investigation of the energy dissipation of a
number of car bumpers under quasi-static lateral loads. International Journal of Impact
Engineering 1(3), 301-308. (1983).
7. Hanssen A.G., Auestad T., Tryland T. and Langseth M., The kicking machine: A device for
impact testing of structural components. International Journal of Crashworthiness 8(4), 1-8,
(2003a).
8. Marciniak Z.,Duncan J.L. and Hu S.J. Mechanics of Sheet Metal Forming. Butterworth-
Heinemann, Oxford. ISBN 0-7506-5300-0,(2002).
9. Dieter G.E., Mechanical Metallurgy. McGraw-Hill, Singapore. (1988).
10. Barlat F., Crystallographic texture, anisotropic yield surfaces and forming limits of sheet metals.
Materials Science and Engineering 91, 55-72. (1987).
11. Barlat F.,Maeda Y.,Chung K., Yanagawa M., Brem J.C., Hayashida Y.,Lege D.J., Matsui
K., Murtha S.J., Hattori S.,Becker R.C and Makosey S.Yield function development for
aluminum alloy sheets. Journal of the Mechanics and Physics of Solids 45(11-12), 1727-1763,
(1997b).
12. Lemaitre J and Chaboche J.L. Mechanics of Solid Materials. Cambridge University Press
(1990).
13. Aretz H, Applications of a new plane stress yield function to orthotropic steel and aluminium
sheet metals. Modelling and Simulation in Materials Science and Engineering 12,491-509,
(2004).
14. Yeh J.R., Summe T.L. and Seksaria D.C, The development of an aluminum failure model for
crashworthiness design. In: Crashworthiness, Occupant Protection and Biomechanics in
Transportation Systems. Edited by Mahmood, Barbat and Baccouche, ASME, New York, (1999).
15. ArkanJawdat Abassa, DhaferSadeq Al-Fatal, “Experimental And Theoretical Study of The
Influence of The Addition of Alumina Powder To 7020 Aluminum Alloy Foam On The
Mechanical Behavior Under Impact Loading” International Journal of Mechanical Engineering &
Technology (IJMET), Volume 3, Issue 3, 2012, pp. 412 - 428, ISSN Print: 0976 – 6340, ISSN
Online: 0976 – 6359.
16. ArkanJawdat Abassa, DhaferSadeq Al-Fatal, “The Effect of Dynamic Impact Loading With
Combined Buckling Stresses on The Dynamic Surface Crack Propagation In Plates Subjected To
Thermal Stresses” International Journal of Mechanical Engineering & Technology (IJMET),
Volume 4, Issue 6, 2013, pp. 122 - 137, ISSN Print: 0976 – 6340, ISSN Online: 0976 – 6359.

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Design analysis of bumper beam subjected to offset impact loading for automotive applications

  • 1. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 64 DESIGN ANALYSIS OF BUMPER BEAM SUBJECTED TO OFFSET IMPACT LOADING FOR AUTOMOTIVE APPLICATIONS P. Sampath Rao Professor, Mechanical Engineering Department, Vijay Rural Eng. College, Nizamabad, T.S. INDIA. S.Saikumar M.Tech Student Mechanical Engineering Department, Vijay Rural Eng. College, Nizamabad, T.S. INDIA ABSTRACT The bumper beam is fixed to front portion of the automobile structure and it is one of the primary component which undergoes damage and transfers the forces to the rest of the structure. Thus the modern bumper beam systems should play a key part in the safety concept of an automobile, ensuring that minimal accelerations are transferred to the passenger. Further the automotive producers are demanding for robust bumper beam systems showing good and reproducible impact behavior. The objectives of this study were to increase the physical understanding of the different phenomena taking place during the offset impact of an automotive bumper beam-longitudinal system as well as to validate a modeling procedure for the system’s crash performance. In presented work the attempt has been made with Simulation of forming process for generating the FE-model of the bumper beam with required curvature. Finally the design and analysis bumper beam subjected to offset impact loading with different materials using FE-code ANSYS-LS DYNA and suggested the best material. Keywords: Bumper Beam, FE-Model, Deflection and ANSYS-LS DYNA 1. INTRODUCTION Fuel economy and emission gas regulations are the primary concerns in changing over to the light weight materials in automotive structures. Aluminium alloys are extensively used in various forms such as extrusions and castings due to its high strength to weight ratio and low density of aluminum compared to steel. Thus for modern cars aluminum alloys are employed in the front and INTERNATIONAL JOURNAL OF MECHANICAL ENGINEERING AND TECHNOLOGY (IJMET) ISSN 0976 – 6340 (Print) ISSN 0976 – 6359 (Online) Volume 6, Issue 5, May (2015), pp. 64-71 © IAEME: www.iaeme.com/IJMET.asp Journal Impact Factor (2015): 8.8293 (Calculated by GISI) www.jifactor.com IJMET © I A E M E
  • 2. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 65 rear bumper beams, crash boxes, longitudinal-in the extruded form, also in other safety component such as side door impact beams, frames engine cradles, chassis, and suspension components. Although the use of the light weight materials helps in reducing fuel consumption and consequently lower carbon dioxide emissions, another stringent demand from the society is the passive safety obtained when employing light weight materials for automobile parts like bumper. Thin-walled tube- like structures have been extensively studied as energy absorbing components by various researchers and some of their opinions can be found in this literature. The open literature available on bumper beam studies is vast and the majority of studies carried out into bumper beam design have been related to the US protection requirements. The structural performance of aluminum bumper beams is examined by Sharp M.L. et.al [4], from the standpoint of local damage (i.e. resistance to denting and cracking),with regard to low-velocity impact (8.3kmph).significant cost savings can be made of being able to damageability of proposed bumper beam designs from “blue prints”. Tang S.C, [5], investigates computer modeling of bumper beam impact resistance and Johnson W et.al [6] studied a series of selected car bumper beams by quasi static loading at their mid-span, and showed that the assumption that a bumper beam could deform through 102mm before the body of the vehicle would become damaged was an over- estimate. However, the literature available on bumper beam systems connected to longitudinal is rather limited or non-existing. In this direction the researchers Lademo O.-G [3] and Hanssen A.G et.al [7] are studied the elastoplasticity and fracture for the material of aluminium alloys. Barlat F., [10] examine the Crystallographic texture, anisotropic yield surfaces and forming limits of sheet metals found that the yield surface shape has a tremendous effect on the predicted failure limits. The objectives of this current study were to increase the physical understanding of the different phenomena taking place during the offset impact of an automotive bumper beam- longitudinal system as well as to validate a modeling procedure for the system’s crash performance .For that choose different materials and select the best material for manufacturing the bumper beam longitudinal system from set of given materials. The objectives were achieved through FE code ANSYS-DYNA. 2. RESEARCH METHODOLOGY 2.1 Identification of Problem The problem studied is outlined in Fig. 1 where a trolley, with a given initial velocity and mass, impacts the bumper beam-longitudinal system at 40% offset. The definition of 40% offset is taken as the distance from the impact point to the extreme left end of the bumper beam. At impact, the impact energy (kinetic energy) of the trolley is mainly absorbed in collapsing the bumper beam as well as the longitudinal at the impacted end, i.e. impacted longitudinal. While the non-impacted longitudinal experience only minor deformations.
  • 3. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 66 Fig. 1. Bumper beam-longitudinal system at 40% offset impact. 2.2 Modeling and design of bumper beam In the design process and crash assessment of vehicles Finite Element Method (FEM) is an indispensable tool. It enables new design concepts to be evaluated where the optimum interaction between materials and structural forms can be studied. The value of such numerical analysis is strongly dependent on a precise description of the mechanical behavior of the material and also the application of enhanced material models. This means, however, that the code has to be validated against precision tests in the laboratory to ensure proper modeling of the member geometry, boundary conditions, material properties and fracture. Thus, in order to establish a reliable experimental database for the system in Figure 1 only few parameters were varied. The experimental database was used for the development and validation of modeling procedures for the crash performance of the bumper beam-longitudinal system with the use of the FE-code ANSYS-DYNA. The numerical model should be able to predict the collapse mode with a high level of certainty in order to ensure robust design. The modeling and design has been developed based on the assumption of ffset impact. 2.3 Bumper beam Material analysis The bumper beam front part of automobile subjected to different loads in service while in impact, the selection of materials is important criteria, in this analysis chosen the material from material library that is aluminum alloy materials AA6060-T1, AA7003-T1 and AA7003-T79 with mechanical properties mentioned in following table 1 Table.1.Mechanical properties of aluminium alloy for Bumper beam Property AA6060-T1 AA7003-T1 AA7003-T79 E Modulus of elasticity, Mpa 69500 70000 70500 G Modulus of rigidity, Mpa 26100 26200 26100 Poisson ratio 0.3 0.29 0.31 Ultimate tensile strength, Mpa 150 150 155 Shear stress, Mpa 95 95 95
  • 4. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 67 3. ANALYSIS, RESULTS AND DISCUSSION The presented work is design and analysis of bumper beam member for automotive applications based on the topography optimization. In this investigation the analysis has been carried out for select the best material for manufacturing the bumper beam longitudinal system from set of given materials. The objective was achieved through FE code ANSYS-DYNA and results are presented in table.2 Fig.2: Geometric model of bumper beam longitudinal system with constraints Fig.3: Finite element model of bumper beam longitudinal system Efforts were taken in constructing the numerical model of the bumper beam as similar as possible to the reality. The bumper beam and all other components in the system were meshed in order to make a precise model. The figures 4 to 7 are shows the deformed shapes of the bumper beam at different time intervals after impact for the material AA7003-T1. Fig.4: Deformed shape of bumper beam longitudinal system at 0.01 sec Fig.5: Deformed shape of bumper beam longitudinal system at 0.015 sec
  • 5. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 68 Fig.6: Deformed shape of bumper beam longitudinal system at 0.03 sec Fig.7: Deformed shape of bumper beam longitudinal system at 0.04 sec The bumper beam longitudinal system shows maximum deformation at time t=0.015 sec i.e., when all the impact energy was absorbed. In the simulations the impact energy is converted to plastic work. The figures 8 to, 11 are shows the deformed shapes of the bumper beam at different time intervals after impact for the material AA7003-T79. Fig.8: Deformed shape of bumper beam longitudinal system at 0.01 sec Fig.9: Deformed shape of bumper beam longitudinal system at 0.015 sec
  • 6. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 69 Fig.10: Deformed shape of bumper beam longitudinal system at 0.03 sec Fig.11: Deformed shape of bumper beam longitudinal system at 0.04 sec The bumper beam longitudinal system shows maximum deformation at time t=0.015 sec i.e., when all the impact energy was absorbed. In the simulations the impact energy is converted to plastic work. The figures 12 to 15 are shows the deformed shapes of the bumper beam at different time intervals after impact for the material AA6060-T1. Fig.12: Deformed shape of bumper beam longitudinal system at 0.01 sec Fig.13: Deformed shape of bumper beam longitudinal system at 0.015 sec
  • 7. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 70 Fig.14: Deformed shape of bumper beam longitudinal system at 0.03 sec Fig.15: Deformed shape of bumper beam longitudinal system at 0.04 sec The bumper beam longitudinal shows maximum deformation at time t=0.015 sec i.e., when all the impact energy was absorbed. In the simulations the impact energy is converted to plastic work Table.2: Deflections of the bumper beam of different materials at different time intervals Time(sec) Dmx-AA7003(T1) in mm Dmx-AA7003(T79) in mm Dmx-AA6060(T1) in mm 0.01 399.463 386.248 397.458 0.015 643.241 620.145 636.144 0.02 402.215 386.778 399.151 0.03 499.588 482.887 496.225 0.04 399.943 386.492 396.559 From all the deformation shapes observed AA7003-T79 shows less deformation for the given load compared to other two alloys. From the table 2 it is clear that alloy AA7003-T79 is better compared to alloys AA6060-T1 and AA7003-T1 for manufacturing the bumper beam longitudinal system. 4. CONCLUSIONS The presented research work is study the dynamic behavior of the bumper beam member by changing the different materials and structural properties. In this scenario FEA model has been generated through FE code ANSYS-DYNA for bumper beam member with the specified quality criteria and analyzed for the optimized results. From the analysis following conclusions are enumerated. i. The AA7003-T79 shows high stiffness and plastic flow compared to AA7003-T1 and AA6060-T1. ii. AA7003-T79 shows 3% less deformation compared to AA6060-T1 and 2.4% less deformation compared to AA7003-T1 for the given applied impact load. iii. Velocities found on the bumper made of AA7003-T79 are less by 5% compared to AA6060-T1 and less by 15% compared to AA7003-T1, which implies that less energy is transferred to the passengers.
  • 8. International Journal of Mechanical Engineering and Technology (IJMET), ISSN 0976 – 6340(Print), ISSN 0976 – 6359(Online), Volume 6, Issue 5, May (2015), pp. 64-71© IAEME 71 iv. Minimal Accelerations are transferred to the passengers in case of Bumper beam made with AA7003-T79. REFERENCES 1. Pugsley A and Macaulay M.A., Cars in collision-safe structures. New Scientist 78(596-598), (1978). 2. Lademo O.-G., Berstad T., Hopperstad O.S. and Pedersen K.O. A numerical tool for formability analysis of aluminium alloys. Part I: Theory. In: Proceedings of the 10th International Conference on Metal Forming. Edited by Kusiak, Hartley, Majta, Pillinger and Pietrzyk,Steel Grips, Suppl Metal Forming 2004, Kraków. (2004a). 3. Lademo O.-G. Engineering models of elastoplasticity and fracture for aluminium alloys. Dr.ing. Thesis, Department of Structual Engineering, Norwegian University of Science and Technology, Trondheim. ISBN 82-471-0367-2. (1999). 4. Sharp M.L., Jombock J.R. and Shabel B.S, Structural performance of aluminium bumpers. SAE Paper No 780140, 569-575, (1978). 5. Tang S.C., Computer modeling of bumper impact resistance. SAE Paper No 790991, 3309-3319. (1979). 6. Johnson W. and Walton A.C., An experimental investigation of the energy dissipation of a number of car bumpers under quasi-static lateral loads. International Journal of Impact Engineering 1(3), 301-308. (1983). 7. Hanssen A.G., Auestad T., Tryland T. and Langseth M., The kicking machine: A device for impact testing of structural components. International Journal of Crashworthiness 8(4), 1-8, (2003a). 8. Marciniak Z.,Duncan J.L. and Hu S.J. Mechanics of Sheet Metal Forming. Butterworth- Heinemann, Oxford. ISBN 0-7506-5300-0,(2002). 9. Dieter G.E., Mechanical Metallurgy. McGraw-Hill, Singapore. (1988). 10. Barlat F., Crystallographic texture, anisotropic yield surfaces and forming limits of sheet metals. Materials Science and Engineering 91, 55-72. (1987). 11. Barlat F.,Maeda Y.,Chung K., Yanagawa M., Brem J.C., Hayashida Y.,Lege D.J., Matsui K., Murtha S.J., Hattori S.,Becker R.C and Makosey S.Yield function development for aluminum alloy sheets. Journal of the Mechanics and Physics of Solids 45(11-12), 1727-1763, (1997b). 12. Lemaitre J and Chaboche J.L. Mechanics of Solid Materials. Cambridge University Press (1990). 13. Aretz H, Applications of a new plane stress yield function to orthotropic steel and aluminium sheet metals. Modelling and Simulation in Materials Science and Engineering 12,491-509, (2004). 14. Yeh J.R., Summe T.L. and Seksaria D.C, The development of an aluminum failure model for crashworthiness design. In: Crashworthiness, Occupant Protection and Biomechanics in Transportation Systems. Edited by Mahmood, Barbat and Baccouche, ASME, New York, (1999). 15. ArkanJawdat Abassa, DhaferSadeq Al-Fatal, “Experimental And Theoretical Study of The Influence of The Addition of Alumina Powder To 7020 Aluminum Alloy Foam On The Mechanical Behavior Under Impact Loading” International Journal of Mechanical Engineering & Technology (IJMET), Volume 3, Issue 3, 2012, pp. 412 - 428, ISSN Print: 0976 – 6340, ISSN Online: 0976 – 6359. 16. ArkanJawdat Abassa, DhaferSadeq Al-Fatal, “The Effect of Dynamic Impact Loading With Combined Buckling Stresses on The Dynamic Surface Crack Propagation In Plates Subjected To Thermal Stresses” International Journal of Mechanical Engineering & Technology (IJMET), Volume 4, Issue 6, 2013, pp. 122 - 137, ISSN Print: 0976 – 6340, ISSN Online: 0976 – 6359.