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ISSN No:-2456-2165
Abstract:- Helmet plays an essential role in reducing the contact hard road surfaces. This is why wearing a helmet is
rate of accidents. Motorcyclists are more prone to crash so important.
injuries than car drivers because motorcycles are
unenclosed, leaving the rider vulnerable to contact hard II. MATERIALS USED
road surfaces. There are many types of helmets depend
upon the field where it is using like riding, sports, etc. Types of synthetic fiber used to make some helmets:
The objective of the work deals with the design and Carbon Fiber
analysis of the helmet under specified boundary Acrylonitrile Butadiene Styrene (ABS)
conditions and loadings for the three different materials Glass Fiber Reinforced Polyester resin (GFRP)
namely, Carbon Fiber, Acrylonitrile Butadiene Styrene
(ABS) and Glass Fiber Reinforced Polyester resin In former times lightweight non-metallic protecting
(GFRP). We are deigning the module in PTC Creo and materials and strong transparent materials for visors were not
compare the impact resistance of the three materials available. Most helmets are made from resin or plastic,
using Ansys and suggesting the best material for better which may be reinforced with fibers as the above mentioned
performance. This type of impact resistance analysis is ones.
likely to carry out to determine the best suitable material
for the given conditions. III. DESIGN AND ANALYSIS OF HELMET
Keywords:- Carbon Fiber, Acrylonitrile Butadiene Styrene The present work explains the behaviour of the helmet
(ABS) and Glass Fiber Reinforced Polyester resin (GFRP), made of different materials virtually under static as well as
Impact Resistance. dynamic loading. The model of helmet is prepared in PTC
Creo software; meshed using Hypermesh and ANSYS as a
I. INTRODUCTION FEM tool to study the behaviour of the helmet under
different loads. Analysis is performed with different
Head injuries due to motorcycle accident cause a great materials i.e Carbon Fiber, ABS and GFRP in three different
deal of concern because it may lead to death and permanent directions to predict the suitable material for making the
disability. Several analyses and experiments on the helmet. A set of estimated results are found out by using the
motorcycle helmet have been performed. Vetter and analyzing software.
Vanderby (1987) developed a non linear finite element
model for the static analysis of helmet. Gilchrist and Mills For designing a helmet model, the standard designing
(1994) performed impact analysis of a motorcycle helmet by parameters are followed. The British, American standards as
using an equivalent model of mass, spring, and damper. well as the IS are preferred mostly.
Yetham et al (1994) carried out a finite element parametric
study of impact response of the helmet. However, the
accuracy of their model was limited because used coarse
mesh. Recentlt, Kostopouls et al (2002) performed impact
analysis of a helmet-head form system using the finite
element code LS-DYNA3D.
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
A. Circumference of the helmet the import of CAD geometry to exporting ready-to-run
Table 1. shows the various sizes of the helmets used in solver file.
all the countries. In this work the medium sized helmet is
considered for analysis. Meshed Model of Helmet
In this meshed model, SHELL 63 is used as element type.
X XX
Size XXS S M L XL
S L
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
Figure 8. Shows drop test helmet after hitting the anvil Figure 12. Shows drop test helmet after hitting the
at 8.5 m/s anvil at 9.5 m/s.
B. Drop Test at a Velocity of 9.5 m/sec Fig 14:- Deformed shape of helmet after hitting the anvil
Figure 11. Shows drop test of helmet before hits the
anvil at 9.5 m/s. Velocity (m/s) Maximum stress (MPa)
8.5 5165
9.5 5985
Table 2. Drop Test Results
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
V. STRUCTURAL ANALYSIS
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
Fig 23:- Stress Distribution at 1400 N Fig 27:- Stress distribution at 1400 N
Fig 24:- Stress distribution at 350 N Fig 28:- Stress distribution at 350 N
Fig 25:- Stress distribution at 700 N Fig 29:- Stress distribution at 700 N
Fig 26:- Stress distribution at 1050 N Fig 30:- Stress distribution at 1050 N
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
Fig 31:- Stress distribution at 1400 N Fig 35:- stress distribution at 1400 N
Fig 32:- Stress distribution at 350 N Fig 36:- stress distribution at 350 N
Fig 33:- Stress distribution at 700 N Fig 37:- stress distribution at 700 N
Fig 34:- stress distribution at 1050 N Fig 38:- Stress distribution at 1050 N
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
Fig 39:- stress distribution at 1400 N Fig 43:- Stress distribution at 1400 N
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
Fig 47:- Stress distribution at 1400 N Fig 51:- Stress distribution at 1400 N
Fig 50:- Stress distribution at 1050N Fig 54:- Stress distribution at 1050 N
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
Fig 63:- Stress distribution at 1400 N Fig 67:- Stress distribution at 1400 N
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
Load (N)
Shell Material
350N 700N 1050N 1400N
Carbon Fiber 7.219 15.66 27.643 33.42
ABS 8.063 16.556 25.065 33
GFRP 8.439 15.514 28.61 32.5
Table 7. Maximum stress (MPa) for helmet when applied on
the side surface
Load (N)
Shell Material
350N 700N 1050N 1400N
Carbon Fiber 0.031 0.133 0.2 0.2231
Fig 79:- Stress distribution at 1400 N
ABS 0.0599 0.117 0.177 0.234
D. Comparing between Maximum Stress and Deflection for GFRP 0.5249 1.054 1.742 2.079
Different Materials on Different Surfaces of Helmet Table 8. Maximum deflection (m) for helmet when applied
on the side surface
Load (N)
Shell Material Load (N)
350N 700N 1050N 1400N Shell Material
Carbon Fiber 9.67 20.074 29.88 40.148 350N 700N 1050N 1400N
ABS 9.621 18.399 29.02 40 Carbon Fiber 5.852 10.822 14.057 21.644
GFRP 9.019 17.396 28.441 39.316 ABS 5.345 10.682 15.331 20.441
Table 3. Maximum stress (MPa) of helmet when load applied GFRP 3.685 7.416 14.08 16.879
on the top surface Table 9. Maximum stress (MPa) for helmet when applied on
the chin surface
Load (N)
Shell Material Load (N)
350N 700N 1050N 1400N Shell Material
Carbon Fiber 0.0741 0.154 0.23 0.309 350N 700N 1050N 1400N
ABS 0.128 0.243 0.39 0.5469 Carbon Fiber 0.00584 0.0107 0.0109 0.0215
GFRP 1.084 2.085 3.466 4.84 ABS 0.008 0.0175 0.028 0.0379
Table 4. Maximum deflection (m) for helmet when load GFRP 0.0652 0.132 0.246 0.298
applied on the top surface Table 10. Maximum deflection (m) for helmet when applied
on the chin surface
Load (N)
Shell Material Load (N)
350N 700N 1050N 1400N Shell Material
Carbon Fiber 2.103 4.233 6.166 8.645 350N 700N 1050N 1400N
ABS 2.03 4.03 6.03 7.2 Carbon Fiber 5.417 11.255 17.641 21.782
GFRP 2.129 3.974 6.09 7.314 ABS 5.513 12.599 16.899 20.457
Table 5. Maximum stress (MPa) for helmet when applied on GFRP 5.508 13.811 16.653 19.334
the rear surface Table 11. Maximum stress (MPa) when applied load on the
forehead surface
Load (N)
Shell Material Load (N)
350N 700N 1050N 1400N Shell Material
Carbon Fiber 0.0147 0.0297 0.0433 0.0594 350N 700N 1050N 1400N
ABS 0.0249 0.049 0.0779 0.0881 Carbon Fiber 0.00584 0.0107 0.01094 0.0215
GFRP 0.2354 0.438 0.6707 0.806 ABS 0.0310 0.1323 0.2 0.2231
Table 6. Maximum deflection (m) for helmet when applied GFRP 0.4581 1.373 1.439 1.546
on the rear surface Table 12. Maximum deflection (m) when applied load on the
forehead surface
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Volume 3, Issue 7, July – 2018 International Journal of Innovative Science and Research Technology
ISSN No:-2456-2165
concluded from the table that different materials behave
differently for varying conditions of loading and also
CARBON FIBER posseses good characteristics under
different loading conditions.
REFERENCES
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