• Journal of Advanced Marine Engineering and Technology
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• 제27권1호
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• pp.76-81
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• 2003

The purpose of this study is to analyze the collapse characteristics of widely used spot welded section members coated damping material Y1000 and to develop an analysis method for acquiring exact collapse loads and energy absorption ratio. Hat-shaped thin-walled members have the biggest energy absorbing capacity in a front-end collision. The sections were tested on quasi-static and impact loads. Specimens with two type thickness, width ratio and spot weld pitch on the flange have been tested in impact velocities(6.73n0sec and 7.54n1sec) which imitate a real-life car collision. As a result, it was developed the system for acquiring impact energy absorbing characteristics of structure united thin-walled member and damping materials.

• 대한기계학회논문집A
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• 제38권9호
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• pp.959-965
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• 2014

본 연구에서는 Al/CFRP 혼성 구조부재가 승용차용 사이드부재에 사용될 것을 상정하여 Al/CFRP 혼성 구조부재의 단면형상의 변화, 최외각층의 변화가 압궤 특성에 어떠한 영향을 미치는가를 실험적으로 고찰하여 수송기계의 경량화를 위한 사이드부재로 사용될 수 있는 설계 데이터를 얻고자 하였다. 실험결과 다음과 같은 결론을 얻었다. 최외층각이 $0^{\circ}$로 적층된 원형 Al/CFRP 혼성 충격 흡수부재가 사각 Al/CFRP 혼성 충격 흡수부재 보다 52,9%, 모자형 Al/CFRP 혼성 충격 흡수부재 보다 49.93% 높게 나타났으며, 최외층각이 $90^{\circ}$로 적층된 경우 원형 Al/CFRP 혼성 충격 흡수부재 사각 Al/CFRP 혼성 충격 흡수부재 보다 50.49%, 모자형 Al/CFRP 혼성 충격 흡수부재 보다 49.2% 높게 나타났다.

• 대한기계학회논문집A
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• 제25권7호
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• pp.1131-1138
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• 2001

This paper concerns the crashworthiness of the widely used vehicle structure, the spot welded hat and double hat shaped section members, which are excellent on the point of the energy absorbing capacity and low production cost. The target of this paper is to analyze the energy absorption capacity of the structure against the front-end collision, and to obtain useful information for designing stage. Changing the spot weld pitches on the flanges, the hat and double hat shaped section members were tested on the axial collapse loads in impact velocities of 4.72m/sec, 6.54m/sec, 7.19m/sec and 7.27m/sec. To efficiently review the collapse characteristics of these sections, the simulation have been carried out using explicit FEM package, LS-DYNA3D. The solutions are compared with results from the impact collapse experiments.