NUMERICAL ANALYSIS OF HYBRID METAL COMPOSITE CRASHBOX UNDER OBLIQUE IMPACT LOADING
Transportation is a critical aspect of the economic sustainability of a country. Land transportation was built to create a safe and ordered system. Therefore, in order to achive safe land transportation, crashworthiness as the vehicle's ability to withstand crush is needed to be implemented....
Saved in:
Main Author: | |
---|---|
Format: | Final Project |
Language: | Indonesia |
Online Access: | https://digilib.itb.ac.id/gdl/view/70169 |
Tags: |
Add Tag
No Tags, Be the first to tag this record!
|
Institution: | Institut Teknologi Bandung |
Language: | Indonesia |
Summary: | Transportation is a critical aspect of the economic sustainability of a country. Land
transportation was built to create a safe and ordered system. Therefore, in order to
achive safe land transportation, crashworthiness as the vehicle's ability to withstand
crush is needed to be implemented. The reference that can be used is Federal
Motor Vehicle Safety Standard (FMVSS) Number 208. One form of crush condition
that is defined in this standard is a frontal oblique crush, the condition for crush at
an angle of ±30 degrees and speed of up to 48 km/hour.
Another aspect that is also important is material selection of the crashbox which has
been developed in the form of hybrid metal composites. With this background, the
analysis of oblique loading and impact column made from hybrid metal composite
become the topic of this research. The hybrid metal composites used is aluminum
AA6063 T52 coated by unidirectional30 e-glass fiber-reinforced epoxy. This
research uses nonlinear dynamic finite element analysis carried out in the form of
parameter variations. Loading is simulated in quasi-static conditions under 1 mm/ms
velocity.
The parameter variations are crash angle, aluminum width, thickness, composite
orientation, and crashbox height. Crash angle variations are from 0 to 30 with a
5-degree increment. Alumunium width variation are 8.33 mm, 12.5 mm, 25 mm, 50
mm, and 75 mm. Thickness variations are conducted on aluminum and
composite. Alumunium thickness variations are 0.4 mm, 0.8 mm, 1.6 mm, 3.2 mm,
and 6.4 mm. Composite thickness variations are 0.3 mm, 0.6 mm, 1.2 mm, 2.4 mm,
and 4.8 mm. Composite orientation variations are [0], [30,-30], [45,-45],
[60,-60], [90], and quasi-isotropic [0,90,45,-45]s. Height variations are 127 mm,
150 mm, 200 mm, and 250 mm.
In crash angle variation, higher angle crushes give two different failure modes, axial
and bending. The axial gives stable Specific Energy Absorption (SEA) results despite
of crash angle increase. Bending gives decreasing SEA results by the higher crash
angle. The transition angle from axial to bending mode is called the critical
angle. The critical angle of the baseline model is 20o and has the lowest value at 30
degrees. The SEA performance of the crash box has the optimum value at an
aluminum width variation of 50 mm, an aluminum thickness of 6.4 mm, a composite
thickness of 4.8 mm, and Quasi Isotropic [0,90,45,-45]s orientation with the
maintained 127 mm height. The association of all optimum variations gives
the enhancement until 284.46% at 30o and postpones the critical angle by 29
degrees.
|
---|