Energy Absorption Characteristics of Crash Box of New Honeycomb Core Structure With Foam-Filled
Energy Absorption Characteristics of Crash Box of New Honeycomb Core Structure With Foam-Filled
Energy Absorption Characteristics of Crash Box of New Honeycomb Core Structure With Foam-Filled
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Xiang Li1, 2)*, Yanmiao Wang2), Xingxing Xu2), Xiangbin Cao2) and Rui Li2)
1)
Hubei Key Laboratory of Hydroelectric Machinery Design & Maintenance, China Three Gorges University,
Yichang, Hubei 443002, China
2)
College of Mechanical and Power Engineering, China Three Gorges University, Yichang, Hubei 443002, China
ABSTRACT–By combining honeycomb core with the traditional crash box, an innovative foam-filled honeycomb core
structure crash box is proposed to improve safety performances. Three kinds of honeycomb core crash boxes were obtained
by filling the inside of the traditional crash box with the quasi-honeycomb core, the quasi-square honeycomb core and
hexagonal honeycomb core. It is deduced that the energy absorption of the quasi-honeycomb core crash box increased by
42.2 %, the peak of the collision force reduced by 8.9 %. The hexagonal honeycomb core crash box and the quasi-square
honeycomb core crash box also enhance the energy absorption characteristics, but the peak impact force increased by 5.6 %
and 9.6 %. After filling of the Expanded Polypropylene (EPP) foam, the peak collision force of the EPP hexagonal
honeycomb core crash box and the EPP quasi-square honeycomb core crash box increased by 10 %, while Fmax of the EPP
quasi-honeycomb core crash box reduced by 2.3 % and the energy absorption increased by 54.6 %. Six structures were
compared to highlight the energy absorption characteristics of the filling the inside of the traditional crash box with the light
in weight honeycomb core and EPP foam. The research results provide a new idea for the design of crash box.
KEY WORDS : Crash box, Low-speed collision, Energy absorption characteristics, Honeycomb core
221
222 Xiang Li et al.
is on the design general standards premise that the mass of the the crash box is fixed. Nonlinear finite element solver
three different EPP honeycomb core crash boxes should be the Hypermesh software is used to simulate the collision process,
same as possible. The size and mass parameters are shown in and the contact mode between the honeycomb core and the
Table 1. The shell mass is 138 g. The honeycomb core and shell of the crash box, the foam and the honeycomb core are
shell of the crash box materials are aluminum alloy. all defined as single surface contact algorithm. Two rigid walls
were made at the upper and lower ends of the crash box. The
2.2. Numerical Method rigid upper wall, which has 4.4 m/s initial velocity collided
The FEM model of the honeycomb core filled the crash box, with the traditional crash box, the honeycomb core crash box
which was imported into Hypermesh for mesh division, is and the foam-filled honeycomb core crash box during 30 ms
established based on the solidworks model. There are finite to simulate a frontal collision between a vehicle and the rigid
element model of the crash boxes, as shown in Figure 4 ~ 5. wall. Static and dynamic friction factors are set at 0.3 and 0.2
There is the main hypothesis for establishing the computation respectively. In order to prevent the hourglass can be higher
model for structural analysis: the thickness of the shell of the than 5 %, the time step is set at -3e-007. The output K file is
crash box and the honeycomb core is small enough the feature imported into the LS-DYNA solver for analysis.
sizes. Based on this hypothesis, the mechanical properties can
be considered as constant along the thickness direction. 2.3. Model Validation
Therefore, a two dimensional sandwich panel model can be In order to prove finite element simulation model we take a
adopted to replace the actual three dimensional model to correlation was performed by comparing experimental data of
simplify the problem. The shells of the six crash boxes are all Tarigopula et al. (2006) with results of finite element
shell element. The mesh size of the honeycomb core and the simulation. The purpose of the experimental data was to be
crash box shell is 0.6 mm, and the mesh size of the foam is considered only for comparison and correlation with the
1 mm. The number of elements and nodes were shown in simulation. The finite element analysis was similar to the
Table 2. They are all divided by a quadrilateral mesh. In the method used in experiment of Tarigopula et al. (2006). For the
actual processing and manufacturing, the honeycomb core reason of equivalence, the finite element model was built to
combines with the inner cavity of the traditional crash box, replicate the experimental specimen, with dimensions of the
which is generally firmly combined by means of adhesive or crash box specimen as 309 mm length, cross section as 58.8 ≤
welding. Nonlinear finite element solver Hypermesh software 57.0 mm and thickness 1.18 mm with an impact velocity of
is used to simulate the collision process, and the contact mode 5.1 m/s. The weight of the rigid upper wall was 600 kg.
between the honeycomb core and the shell of the crash box, Figures 6 ~ 7 shows the axial force vs. displacement curve and
the foam and the honeycomb core are all defined as single deformation modes of comparison of the test result with the
SingleSuface contact algorithm. In this way, the shell of the finite element simulation. As shown in the Table 2, we
crash box and the honeycomb core as a whole are compression compared force parameter between simulation and
deformation under low-speed collision. The type is to be experimental result of the crash box. The finite element
Eroding. The shell material of the crash box is 6063 aluminum simulation outputs are significantly correlated with the
alloys and the foam material is EPP. Table 3 is the main experimental results. The error of Fmax between experiment
parameters. In this section, the reliability and accuracy of the and finite element model is 4.2 % and the error of mean force
model are verified by simulation according to the low-speed between experiment and FEA is 11.9 %. Little error still exists
collision requirement of RCAR legislation (Zhu et al., 2011; between the finite element model and experiment and it is
Kang, 2016). In the simulation, the bottom end of the shell of acceptable. A good agreement between simulation results and
Figure 5. Finite element model of the crash boxes filled with six kinds of EPP honeycomb cores.
Table 5. Average collision force and specific energy absorption of crash box.
Hexagonal Quasi-square
The crash Quasi- Traditional EPP hexagonal EPP quasi-square EPP quasi-
honeycomb honeycomb
box types honeycomb core crash box honeycomb core honeycomb core honeycomb core
core core
Fm(kN) 87.5 78 66.1 46.5 90.87 81.25 71.87
SEA(J/kg) 35.3×103 31.5×103 26.9×103 26.9×103 34.6×103 31.1×103 27.5×103
ENERGY ABSORPTION CHARATERISTICS OF CRASH BOX OF NEW HONEYCOMB CORE STRUCTURE 229
core crash box and EPP foam-filled honeycomb core crash box ACKNOWLEDGEMENT–This research work was supported by
were studied under low-speed impact load. The main Yichang Key Laboratory of Robot and Intelligent System, China Three
conclusions are as follows: Gorges University, Yichang 443002, China (JXYC00015), the
Hydropower Machinery Equipment Design and Maintenance Hubei
After filling the honeycomb core, the folding deformation of Provincial Key Laboratory Open Fund Project (2017KJX04) and
the traditional crash box becomes more stable than before. It Sponsored by Research Fund for Excellent Dissertation of China
is shown that the deformation of the hexagonal honeycomb Three Gorges University (2020SSPY034). The authors would like to
core box and the quasi-honeycomb core crash box is express their appreciation for above fund supports.
completely symmetrical and superposition mode, and the
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