• 한국안전학회지
• /
• 제12권4호
• /
• pp.57-62
• /
• 1997

The combined structure of hybrid composite made through the bonding process of materials of different properties greatly defines its mechanical characteristics, as the results of the experiments on materials of different properties show much dissimilarity. When carbon/epoxy materials are applied to hybrid composite, the carbon materials helps to improve the mechanical properties of the hybrid composite, and the epoxy reduces its fracture strain and impact resistance. Carbon fiber which is now in general commercialization is classified as high modulus or high strength system, and its manufacturing methods are various. The study of the materials having combined structure is focused on the numerical analysis of the layers of bonding surface in materials with difference modulus. The hybrid composite made through the multilayered bonding of reinforced aluminium sheets with aramid fiber now faces the marketing phase, and especially its excellent fatigue resistance and mechanical properties promote active researches on the similar products of hybrid composite. This study aims to investigate the effects of CFRP volume ratio and fiber's orientation over the properties of mechanical strength and fatigue life of the hybrid composite, AI7075/CFRP. To carry out this study, static tensile and fatigue tests were given to some of the panels which, made through the co-cure processing in an autoclave, have different CFRP volume ratio and carbon fiber orientations.

• 대한기계학회:학술대회논문집
• /
• 대한기계학회 2000년도 추계학술대회논문집A
• /
• pp.231-237
• /
• 2000

A15052/AFRP laminates were developed principally to obtain a material with good fatigue strength, in which possible cracks would grow very slowly. Weight savings of more than 30% should be attainable in practice. Also, the crack bridging fibers could still was carry a significant part of the load over the crack, thus the COD and stress intensity factor was reduced at the crack tip. A15052/ AFRP laminates consists of three thin sheets of 5052-H34 aluminum alloy and two layers of [0] unidirectional aramid fiber prepreg. The cyclic-bending moment test was investigated based on applying the five kinds of bending moments. The size of the delamination zone produced between 5052-H34 aluminum alloy sheets and fiber-adhesive layers was measured from ultrasonic C-scan pictures taken around the fatigue crack. In addition, the relationship between the cyclic-bending moment and the delamination zone size was studied and the effect of fiber bridging mechanism was also considered.

• 한국정밀공학회지
• /
• 제16권8호
• /
• pp.149-154
• /
• 1999

FRMLs(Fiber Reinforced Metal Laminates) is a new type of hybrid materials. FRMLs consists of high strength metal and fiber which are laminated using a structural adhesive bond(epoxy resin). The effect of resin mixture ratios on the fatigue crack propagation behavior and mechanical property of Aramid fiber reinforced aluminum composites was investigated. The epoxy, diglycidylether of bisphenol A(DGEBA) was cured with methylene dianiline(MDA) with or without accelerator(K-54). Eight kinds of resin mixture ratio were tested for the experiment ; five kinds of FRMLs(1))epoxy & curing agent) and three kinds of FRMLs(2)(epoxy & curing agent & accelerator). FRMLs(2) have a more effective characteristics on the fatigue crack propagation behavior and mechanical property than FRMLs(1)

• Composites Research
• /
• 제13권3호
• /
• pp.21-29
• /
• 2000

The optimum design of hybrid laminated composites for iso-strain structure has been studied by controling fiber orientations and thicknesses of each layer. Fiber orientations and thicknesses of each layer for iso-strain structure were designed. Combining the laminates of each layer of different reinforcing material, the constitutions of hybrid laminated composite for iso-strain structure were obtained. All these calculations were formed on computer systems, automatically for the hybridization. Using the data of some specific laminated composite such as glass and aramid reinforced composites, the constitutions of hybrid laminated composites for iso-strains structure were designed and verified by lamination theory. The strains of each layer of hybrid laminated composites are calculated and they turned out to be good agreements with the results obtained lamination theory.

• 한국콘크리트학회:학술대회논문집
• /
• 한국콘크리트학회 1996년도 가을 학술발표회 논문집
• /
• pp.501-507
• /
• 1996

The final objectives of this study are to present the theoretical formula for reasonable structural analysis and practical codes on the repair/strengthening of damaged reinforced concrete structrues. For that purpose, in last year, preliminary experiments for flexure and shear of beam structure using carbon sheet and steel plate were performed, and in sequence, in this year, using aramid fiber sheet and steel plate more extensive experiment were performed. Repair for the performance of flexure and shear was focused on, and main variables were selected considering aplicablilty for practical field, such as, spacing of anchor bolt, lapping, jacking up, preloading level, and fiber difection as well as length of repairing plate and thickness. so new results from various angles are to be presented.

• 한국콘크리트학회:학술대회논문집
• /
• 한국콘크리트학회 1997년도 봄 학술발표회 논문집
• /
• pp.598-604
• /
• 1997

In recent years, strengthening by epoxy-bonded steel plates, carbon fiber sheets, aramid fiber sheets and so on, is spotlighted. Among them, the method using steel plates is most widely applied. Most studies have dealt with strengthening by epoxy-bonded steel plates. However the actual behavior of strengthened RC beams are not well established. Particularly, the studies on the separation load thar affects failure load of the beam are relatively insufficient. In this study, test parameters are the magnitude of pre-load, plate length, plate thickness, existence and spacing of anchor bolt, the number of plate layer and the height of side strengthening, 17reinforced concrete beams are strengthened by steel plates according to test parameters. Deflection, failure load, strains of reinforcing bar, concrete and plate are measured from tests(4 points loading). The failure mode, and separation load are analyzed from these measured data. The difference between Robert's theory and test results is discussed, and the prediction equation for separation load in the case of rip off is proposed.

• 한국구조물진단유지관리공학회 논문집
• /
• 제10권6호
• /
• pp.154-163
• /
• 2006

본 논문에서는 철근 콘크리트보의 인장면에 고강도이며 경량인 섬유시트를 외부 부착한 보강보의 휨 실험결과를 바탕으로 섬유시트로 보강된 RC 휨부재의 비선형 해석 기법을 제시한다. 섬유시트의 인장성능을 측정하기 위하여 총 120개의 섬유시트 인장시험편을 제작하여 시험하였으며, 섬유시트 보강 RC보의 여러 가지 보강특성 및 섬유시트의 적절한 파단변형률을 평가하기 위한 실험적 연구를 위해 75개의 비교적 큰 규모의 보를 시험하였다. 콘크리트의 비선형 압축 분포 및 인장성능을 고려한 비선형 단면 해석과정을 전개하였으며, 이러한 비선형 해석기법이 섬유시트 보강 RC보의 하중-변위 응답 및 휨거동 특성을 정확하게 예측함을 확인하였다.

• 한국재료학회지
• /
• 제6권8호
• /
• pp.786-795
• /
• 1996

열가소성 고분자 복합재료 개발을 위하여 매트릭스 수지로는 폴리프로필렌섬유(PP)를 사용하고 유기계 강화소재로 폴리비닐알코올(비닐론, VF), 아라미드(케블라-49, KF) 및 폴리아미드섬유(PAF)등을 사용하였다. 복합매트제조장치로서 복합매트를 제조하고 가열.압축하여 고분자 복합재료를 성형하였다. 제조한 고분자 복합재료의 형태학, 유변학적 및 기계적특성 등을 측정하였다. 형태학에서 미트릭스와 강화섬유 간의 젖음성은 강화섬유의 함량이 증가함에 따라 감소하는 경향을 보였다. PAF/PP와 VF/PP 복합재료에 대한 점성도는 낮은 주파수 영역에서 강화섬유의 함량이 증가됨에 따라 증가하였으나, 높은 주파주 영역에서 5-20wt%로 강화된 복합재료는 매트릭스인 PP에 근접하게 감소된 점성도를 나타냈다. 기계적 특성은 강화 섬유의 함량에 따라 변하였으며, VF/PP 및 KF/PP 복합재료가 PAF/PP 계에 비해 우수한 현상을 보였다.

• 접착 및 계면
• /
• 제22권4호
• /
• pp.118-127
• /
• 2021

본 연구에서는 NBR 고무의 물성을 향상시키기 위해서 충진재의 함량 조절 및 복합화를 통한 가황고무의 기계적 특성에 대해 실험하였다. 충진재는 내열성이 우수하다고 알려진 아라미드 섬유와 유리 섬유를 사용하였고, 상호보완 효과를 기대하여 세라믹을 적용하였으며, 적용된 세라믹 재료는 형상에 따라 침상구조의 세라믹과 판상구조의 세라믹을 적용하였다. 각 충진재의 기초 물성 조사를 위해 각 충진재는 5.0, 10.0, 15.0, 20.0 phr의 양으로 사용되었으며, 증량에 따른 물리적 특성을 비교 및 분석하였다. 세라믹 적용을 통한 상호 보완 효과를 확인하기 위해 각 10.0 phr 섬유와 세라믹을 1 : 1 복합 충진하여 기계적 물성 특성에 관한 평가를 하였다. 그 결과, 충진재 단독적용의 경우 아라미드 섬유, 침상 세라믹, 유리 섬유, 판상 세라믹 순으로 열 노화 후 인장강도 감소율이 작은 것으로 확인되었다. 또한 섬유와 세라믹 기반의 복합 충진재가 적용된 가황고무의 기계적 특성을 평가하였으며, 복합 충진재가 열 노화에 대한 상호보완 효과를 가지는 것을 확인하였다.

• 한국초전도ㆍ저온공학회논문지
• /
• 제24권1호
• /
• pp.8-12
• /
• 2022

Recently, research on applying composite materials to various industrial fields is being actively conducted. In particular, composite materials fabricated by Fused Deposition Modeling 3D printers have more advantages than existing materials as they have fewer restrictions on manufacturing shape, reduce the time required, weight. With these advantages, it is possible to consider utilizing composite materials in cryogenic environments such as the application of liquid oxygen and liquid hydrogen, which are mainly used in an aerospace and mobility. However, FDM composite materials are not verified in cryogenic environments less than 150K. This study evaluates the characteristics of composite materials such as tensile strength and strain using a UTM (Universal Testing Machine). The specimen is immersed in liquid nitrogen (77 K) to cool down during the test. The specimen is fabricated using 3D print, and can be manufactured by stacking reinforced fibers such as carbon fiber, fiber glass, and aramid fiber (Kevlar) with base material (Onyx). For the experimental method and specimen shape, international standards ASTM D638 and ASTM D3039 for tensile testing of composite materials were referenced.