• 한국철도학회:학술대회논문집
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• 한국철도학회 2005년도 춘계학술대회 논문집
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• pp.251-256
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• 2005

This study was performed the heat transportation ratio of three types of the following sandwich panel by KS F 2278(2003) ; Type ${\sharp}1$ : Carbon/epoxy Aluminum Honeycomb and Balsa Core Sandwich Panel(Thickness : 37mm), Type ${\sharp}2$ : Carbon/epoxy Aluminum Honeycomb Core Sandwich Panel(Thickness : 57mm), and Type ${\sharp}3$ : Carbon/epoxy Aluminum Honeycomb Core Sandwich Panel(Thickness : 37mm). Also was performed the heat transportation of next three types of the following sandwich panel by KS F2277(2002) ; Type ${\sharp}4$ and ${\sharp}5$ : 27mm, and 35mm thick-Aluminum Honeycomb Sandwich Panels, and Type ${\sharp}6$ : 27mm thick-Foaming Aluminum Sandwich Panel. It is the larger area between the skin and core, the heat transportation ratio is the higher, and when it is composed of the hybrid composite structure, good insulation property was shown.

• 한국산학기술학회논문지
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• 제13권2호
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• pp.478-484
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• 2012

본 연구에서는 다공성 심재를 갖는 샌드위치 복합재료의 압축해석을 수행하였다. 알루미늄 폼 및 허니컴 코어 샌드위치 복합재료의 유한요소모델은 솔리드 요소를 적용하였다. 알루미늄 폼 코어의 경우에는 유효등가손상모델을 적용하였다. 면내 압축해석에서 알루미늄 폼 및 허니컴 코어 샌드위치의 압축 최대하중이 비슷했다. 그러나 알루미늄 허니컴 코어 샌드위치의 하중 지지구간이 더 길었다. 면외 압축에서는 알루미늄 허니컴 코어 샌드위치의 압축 최대하중이 알루미늄 폼 코어 샌드위치보다 높게 나왔다. 시뮬레이션 해석을 통하여 샌드위치 복합재료의 압축 거동을 얻을 수 있었다.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2004년도 추계학술발표대회 논문집
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• pp.61-64
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• 2004

The strength characteristics as well as deformation behaviors of honeycomb sandwich composite (HSC) structures were investigated under bending in consideration of various failure modes such as skin layer yielding, interface-delamination, core shear deformation and local buckling. Deformation behaviors of honeycomb sandwich plates were observed with various types of aluminum honeycomb core and skin layer. Their finite-element analysis simulation with a real model of honeycomb core was performed to analyze stresses and deformation behaviors of honeycomb sandwich plates. Its results were very comparable to the experimental ones. Consequently, the increase in skin layer thickness and in cell size of honeycomb core had dominant effects on the strength and deformation behaviors of honeycomb sandwich composites.

• 한국산학기술학회논문지
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• 제19권1호
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• pp.666-671
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• 2018

허니콤 판재(honeycomb panel)는 벌집 모양의 코어(core) 양쪽면에 표면판재를 부착시켜 만든 판재이다. 허니콤 판재는 비강도가 뛰어나며, 재료에 압축하중이 가해졌을 때 재료가 수차례의 좌굴을 반복하기 때문에 에너지 흡수성이 우수하여 내충격성이 요구되는 부위에 사용하기에 적합하다. 특히 최근에는 수송기기의 경량화에 대한 요구가 증가함에 따라 알루미늄 허니콤 판재를 자동차 및 고속전철 등의 차체 재료로 이용하려는 연구가 진행되고 있다. 이 밖에도 허니콤 판재는 흡음성과 평활성이 우수하며, 단열성과 내피로성도 우수하다. 연료 경제성을 증가시키기 위하여 알루미늄 합금 소재와 같은 경량 소재를 허니콤 판재 주 재료로 사용하여 무게를 감량시키는 것에 관한 연구를 진행 하였다.본 연구에서는 허니콤 판재의 설계기술, 알루미늄 허니콤 코어 및 허니콤 판재 제조 기술에 대한 연구를 수행하였으며, 또한 제조된 허니콤 판재의 각종 기계적 특성평가를 행하여 그 결과를 바탕으로 알루미늄 허니콤 판재의 제조 공정 설계, 판재 제작 및 특성 평가방안을 마련하였다. 연구결과 허니콤 판재의 우수한 에너지 흡수성은 코어 버클링의 반복에 기인하며 압축강도가 높을수록 접합면적당 강도 또한 높은 값을 나타내었다.

• 한국산학기술학회논문지
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• 제12권9호
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• pp.3802-3807
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• 2011

본 연구에서는 알루미늄 폼 및 허니컴 샌드위치 복합재료의 면내 외 압축실험을 수행하였다. 실험을 통하여 하중-변위의 관계를 분석하고 압축 특성을 비교한다. 시험편은 만능재료시험기를 사용하여 1 mm/min로 압축을 하였다. 실험과정은 카메라로 촬영하고, 로드셀에서 나오는 데이터는 컴퓨터로 저장하였다. 실험결과를 보면 하중이 증가함에 따라 알루미늄 폼 및 허니컴 심재에 좌굴이 발생하였다. 면내 압축실험에서 알루미늄 폼 및 허니컴 샌드위치 시험편의 압축 최대하중은 비슷하였다. 그러나 비중을 고려하면 허니컴이 폼보다 압축 특성이 더 우수하다. 면외 압축실험에서도 알루미늄 허니컴 샌드위치 복합재료의 압축 최대하중이 알루미늄 폼 샌드위치 복합재료보다 높게 나왔다.

• 한국해양공학회:학술대회논문집
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• 한국해양공학회 2000년도 춘계학술대회 논문집
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• pp.89-94
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• 2000

Because the structural elements used in the automobile, astronautic and ship industries are put in dynamic loading environments, much interest is given to the damping of the structural elements, as well as high flexural rigidity and strength per density. Therefore, in this study, the structural damping value of the aluminum honeycomb sandwich plate(AHCP) has been experimentally extracted, and directly applied to the finite element, for the dynamic analysis of the plate considering the structural damping. The analysis results of this theory was compared with the results of the actual modal analysis method. It was observable that the two analyses concurred, establishing the structural damping and analysis method of the AHSP.

• Computers and Concrete
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• 제27권4호
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• pp.369-383
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• 2021

This article deals with the frequency analysis of viscoelastic sandwich disk with graphene nano-platelets (GPLs) reinforced viscoelastic concrete (GPLRVC) face sheets and honeycomb core. The honeycomb core is made of aluminum due to its low weight and high stiffness. The rule of the mixture and modified Halpin-Tsai model are engaged to provide the effective material constant of the concrete. By employing Hamilton's principle, the governing equations of the structure are derived and solved with the aid of the Generalize Differential Quadrature Method (GDQM). In this paper, viscoelastic properties are modeled according to Kelvin-Voigt viscoelasticity. The deflection as the function of time can be solved by the fourth-order Runge-Kutta numerical method. Afterward, a parametric study is carried out to investigate the effects of the outer to inner radius ratio, hexagonal core angle, thickness to length ratio of the concrete, the weight fraction of GPLs into concrete, and the thickness of honeycomb core to inner radius ratio on the frequency of the viscoelastic sandwich disk with honeycomb core and FG-GPLRVC face sheet.

• 수산해양기술연구
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• 제40권4호
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• pp.351-359
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• 2004

본 연구에서는 실선에 적용된 알루미늄 하니콤 샌드위치 판 (AHSP)을 저자가 제안한 심재의 형상이 피라미드인 알루미늄 샌드위치 판의 구조적 특성 및 진동특성을 검토해 보았다. 알루미늄 피라미드 샌드위치 판(APSP)의 기초 자료로 쓰일 수 있게 심재의 각도변화, 높이변화 및 면재와 심재의 두께변화에 따른 구조적 특성을 검토한 결과 APSP가 강도 및 강성에서 우수함을 보였으며, 질량대비 큰 강성 때문에 고유진동수도 다소 크게 평가되었다.

• 대한기계학회논문집A
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• 제33권1호
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• pp.64-71
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• 2009

In this paper, a study on low-velocity impact response of honeycomb sandwich panels was done for the changes of impact location and core fabrication angles. The test specimens were made of glass/epoxy laminate facesheet and aluminum honeycomb core. Square samples of 100mm and 100mm sides were subjected under low-velocity impact loading using instrumented testing machine at three energy levels. Impact parameters like maximum force, time to maximum force, deflection at maximum force and absorbed energy were evaluated and compared for the changes of impact location and core fabrication angle. The impact damage size were measured at facesheet surface by 3-Dimensional scanner. Also, sandwich specimens after impact test were cut to analyse the failure mode.

• Advanced Composite Materials
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• 제17권1호
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• pp.41-56
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• 2008

In this research, optical fiber sensors and shape memory alloys (SMA) were incorporated into sandwich panels for development of a smart honeycomb sandwich structure with damage detection and shape recovery functions. First, small-diameter fiber Bragg grating (FBG) sensors were embedded in the adhesive layer between a CFRP face-sheet and an aluminum honeycomb core. From the change in the reflection spectrum of the FBG sensors, the debonding between the face-sheet and the core and the deformation of the face-sheet due to impact loading could be well detected. Then, the authors developed the SMA honeycomb core and bonded CFRP face-sheets to the core. When an impact load was applied to the panel, the cell walls of the core were buckled and the face-sheet was bent. However, after the panel was heated over the reverse transformation finish temperature of the SMA, the core buckling disappeared and the deflection of the face-sheet was relieved. Hence the bending stiffness of the panel could be recovered.