• Proceedings of the KAIS Fall Conference
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• 2011.05b
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• pp.602-604
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• 2011

본 연구에서는 알루미늄 폼 샌드위치 복합재료와 알루미늄 허니컴 샌드위치 복합재료의 면내 외 방향 압축실험으로 하중-변위의 관계를 분석하고 압축 특성을 비교하였다. 만능재료시험기로 1 mm/min 의 속도로 압축을 하였으며, 카메라로 실험과정을 촬영하고 로드셀에서 나오는 데이터를 컴퓨터로 저장하였다. 압축실험의 결과로 알루미늄 폼 및 허니컴 샌드위치 복합재료에서 하중이 증가함에 따라 심재에 좌굴이 발생하였다. 면내 방향 압축실험에서 알루미늄 폼 및 허니컴 샌드위치 시험편에 작용하는 압축 최대하중은 비슷하지만 비중을 고려하면 알루미늄 허니컴 샌드위치 복합재료가 더 우수한 것으로 판단되며, 면외 방향 압축실험에서도 알루미늄 허니컴 샌드위치 복합재료의 압축 최대하중이 알루미늄 폼 샌드위치 복합재료보다 높게 나왔다.

• Proceedings of the KAIS Fall Conference
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• 2012.05b
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• pp.646-648
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• 2012

본 연구에서 다루는 복합재료는 알루미늄 폼으로써 다공성 구조체로 고체 알루미늄 금속에 비하여 비중이 1/10 정도로 작고, 충격에너지 흡수가 우수하다. 본 연구에서는 다공성 심재를 갖는 복합재료 알루미늄 폼 코어의 충격실험을 실시하여 기계적 특성을 파악하였다. 시험편은 알루미늄 폼 코어를 갖는 복합재료로써 시험편에 50J의 저 충격에너지를 가하도록 하였다. 그 결과, 모든 실험에서 스트라이커가 상부면재 통과 시 최대하중이 나타났고, 이때의 최대하중 값은 약 5.5 KN으로 나타났다. 또한 최대 하중 발생 시간은 50J일 때 약 4.2 ms가 나왔다. 최대 하중이 발생한 후, 즉 상부 면재 통과 후에 실험에서는 약 10 mm정도를 더 뚫으면서 심재에 까지 손상을 주었지만 하부 면재에는 손상을 주지 못하였다. 이로써 스트라이커가 알루미늄 폼 코어 샌드위치 복합재료를 통과 할 때 상부면재 통과 시 최대 하중이 발생하고 심재를 지나며 서서히 감소되는 것을 볼 수 있었다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.12 no.4
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• pp.1552-1558
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• 2011

In this paper, the automotive beam using aluminium foam is designed and the impact analysis is carried out. The analysis model is the beam of actual size with B- type section structure. At the frontal crash of low speed, ANSYS AUTODYN is used by predicting the behavior of deformation and its internal energy. By the use of 7075-T6 aluminum alloy, the weight is reduced as much as 55% than steel. The deformation at the bumper foam of aluminum is similar with that of steel and the impact energy reduction at aluminum is more than steel. The foam filled with aluminum as much as 50 % has more impact energy absorption than the completely filled aluminum foam.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.12 no.9
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• pp.3802-3807
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• 2011

In this study, in-plane and out-plane compression tests of aluminum foam and honeycomb sandwich composites were carried out. Through these tests, the relationships of load-displacements were analyzed and the compression characteristics were compared with each other. The specimens were compressed with the speed of 1mm/min by using the universal testing machine. Experimental procedures were taken with photograph by the camera and load cell data were stored into computer. Test results showed that buckling was occurred at the aluminum foam core and honeycomb core according to the increase of load. In the in-plane compression test, the maximum load of aluminum foam specimen was similar with that of honeycomb sandwich. The property of honeycomb was better than that of the foam in consideration of specific gravity. In the out-plane compression test, compression maximum load of aluminum honeycomb sandwich composite was higher than that of aluminum foam sandwich composite.

• Proceedings of the Korean Institute of Building Construction Conference
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• 2010.05a
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• pp.41-44
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• 2010

Presently, the apartment house is being constructed by the very various methods. Among them, the formwork having the process rate of 60~70% of the whole construction work is most important. So this study was analyzed comparing euro-form with aluminium-form in the formwork. A case study is using euro-form and aluminum-form in the framework, inquiry into a similar case construction site of below the 20 floor. Then this case analyzed efficiency; construction period, construction cost, workability. Consequently, the aluminum-form is more effective than the euro-form in the construction site of below the 20 floor.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.39 no.10
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• pp.971-977
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• 2015

Because foam metal has the excellent physical characteristics and mechanical performance, they are applied extensively into a lot of advanced technology areas. The aluminum foam with closed cell is one of the foam metals. It is applied widely into automobile and airplane because of the excellent absorption performance of impact energy. In this study, the mechanical characteristics by thickness was analyzed through the impact experiment of closed-cell aluminum foam, and the simulation analysis was performed for the verification. As the simulation analysis method, a finite-element analysis was carried under the same boundary conditions as the experiment by using ANSYS. By comparing with the results of experiment and simulation, it was thought that the case of thickness of 20mm was the most efficient of among the cases of thicknesses of 10mm, 20mm and 30mm. At the case of thickness of 20mm, the absorption energy by comparing with the specimen thickness is shown to become the most among three models. By using the result of this study, it is thought that it can apply the material necessary to develop the mechanical structure with aluminum foam.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.13 no.2
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• pp.478-484
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• 2012

In this study, compression analyses of sandwich composites with porous core were carried out. Finite element models of aluminum foam and honeycomb core sandwich composite material were applied solid element. In the case of aluminum foam core, valid equivalence damage model was applied. In the in-plane compression analysis, the maximum load of aluminum foam core sandwich was similar with that of aluminum honeycomb core sandwich. But in case of aluminum honeycomb core sandwich, the load support region becomes longer in comparison with aluminum foam core sandwich. In the out-plane compression analysis, compression maximum load of aluminum honeycomb core sandwich was higher than that of aluminum foam core sandwich. Through these Simulation analysis, obtains the behavior of sandwich composites.

• Proceedings of the KAIS Fall Conference
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• 2012.05b
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• pp.617-619
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• 2012

본 논문에서는 알루미늄 폼 복합재료로 된 DCB(이중외팔보) 구조체의 파괴 거동을 시뮬레이션 해석하였다. 시뮬레이션 해석에 사용된 모델은 영국 공업규격과 ISO국제규격에 의거하여 3D모델을 설계하였다. 해석 결과 모델의 두께가 두꺼울수록 발생한 크랙의 길이가 길게 나타났고, 높은 하중이 발생하였다. 이와 같은 연구에서 얻어진 해석 결과를 통하여 알루미늄 폼 재질로 접합된 실제 복합재 구조물에 적용시켜 파괴거동을 분석하고 그 기계적인 특성을 파악할 수 있다.

• Proceedings of the Computational Structural Engineering Institute Conference
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• 2010.04a
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• pp.272-275
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• 2010

폭파하중에 대한 구조물 위험평가 해석을 위해 3차원 모델링 기법 중 하나인 변수모델링과 이를 활용한 3차원 유한요소해석 모델을 구축하여 외연적 유한요소해석을 수행하였다. 폭파하중은 ConWep을 이용하였고, 폭파압력 저감을 위해 알루미늄 폼의 밀도와 두께, 그리고 덮개 여부를 해석 변수로 설정하였다. 해석 결과, 알루미늄 폼의 밀도가 낮고 두께가 두꺼울수록 항복강도 수준으로 제어할 수 있었고, 폭발압력을 분산시키기 위해 사용한 강재 덮개는 두께에 대한 그 영향이 뚜렷이 나타났다. 적절한 설계변수 설정을 통해 폭파하중에 대한 구조물의 위험을 줄일 수 있을 것으로 예상된다.

• Proceedings of the Materials Research Society of Korea Conference
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• 2008.05a
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• pp.49.1-49.1
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• 2008