journal article·2016-04

Crashworthiness of carbon fiber hybrid composite tubes molded by filament winding

Jing Xu, Yan Ma, Qianjin Zhang, Toshi Sugahara, Yuqiu Yang, Hiroyuki Hamada

Publisher page

Abstract

Abstract Carbon Fiber Reinforced Composites (CFRPs) with light weights absorbed a large quantity of energy through the progressive crushing modes by a combination of multi micro-crack including fiber fracture and matrix fracture, bending, delamination, splitting, friction and so on. High manufacturing cost of CFRPs was one of the most important reasons for not being used as energy absorption components in wide range. In this study, five types of tubes were manufactured by filament winding method and crashworthiness performance was investigated experimentally. The effects of crushing speed, temperature treatment, raw material and structure including hybrid ratio, fiber orientation and thickness of tube wall on energy absorption capabilities were investigated through quasi-static and dynamic compression tests. Optical microscope observation of cross sections was taken to analyze the mechanism of failure. A hybrid carbon/aramid FRP tube after temperature treatment exhibited the highest Es in quasi-static test (98 kJ/kg in average) and dynamic tests (82 kJ/kg in average), which have excellent energy absorption management.
Source: openaire · Quality: candidate unverified · Source record ↗

Research context

OpenAlex topics: Cellular and Composite Structures · Mechanical Behavior of Composites · Transportation Safety and Impact Analysis

SciVX discovery tags are terminology-based. OpenAlex topics are source-provided classifications.

References (21)

Show source-provided references
1. Experimental study on the axial crushing behaviour of pultruded composite tubes10.1016/j.polymertesting.2009.11.005 ↗
2. Deslauriers P. Numerical modeling of composite structures for advanced automotive applications. M ProQuest; 2006.
3. The interplay of geometric and materials variables in energy absorption10.1115/1.3443419 ↗
4. Experimental investigation of the crash energy absorption of 2.5D-braided thermoplastic composite tubes10.1016/j.compstruct.2014.05.037 ↗
5. Comparison of energy absorption of carbon/epoxy and carbon/PEEK composite tubes10.1016/0010-4361(92)90184-V ↗
6. Effect of resin properties and processing parameters on crash energy absorbing composite structures made by RTM10.1016/S1359-835X(03)00057-5 ↗
7. The effect of fiber and matrix maximum strain on the energy absorption capability of composite materials10.1177/002199838602000401 ↗
8. The effect of fiber orientation on the energy absorption capability of axially crushed composite tubes10.1016/j.matdes.2013.12.009 ↗
9. Experimental and analytical assessment of axial crushing of circular hybrid tubes under quasi-static load10.1016/j.compstruct.2012.01.003 ↗
10. Crashworthy characteristics of axially statically compressed thin-walled square CFRP composite tubes: experimental10.1016/S0263-8223(03)00183-1 ↗
11. The effect of FRP thickness on energy absorption of metal-FRP square tubes subjected to axial compressive loading10.1016/j.compstruct.2015.04.009 ↗
12. Effect of trigger configuration on the crashworthiness characteristics of natural silk epoxy composite tubes10.1016/j.compositesb.2013.05.022 ↗
13. Energy absorption in polymer composites for automotive crashworthiness10.1177/0021998302036007164 ↗
14. Numerical investigation of a crash test of a composite helicopter subfloor structure10.1016/S0263-8223(00)00150-1 ↗
15. A study on the energy absorption properties of CF/AF fiber filament winding composite tube10.1016/j.compstruct.2014.12.067 ↗
16. A unified approach to progressive crushing of fibre-reinforced composite tubes10.1016/0266-3538(91)90031-J ↗
17. Collapse of thin-wall composite sections subject to high speed axial loading
18. Quasi-static and dynamic experiment investigations on the crashworthiness response of composite tubes10.1002/pc.22518 ↗
19. Crushing mechanism of carbon fibre/PEEK composite tubes10.1016/0010-4361(95)98195-Q ↗
20. Effects of heat treatment on the mechanical properties of Kevlar-29 fibre10.1016/S0266-3538(99)00137-2 ↗
21. Thermal aging of an anhydride-cured epoxy resin10.1016/j.polymdegradstab.2015.04.017 ↗