• 한국생산제조학회지
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• 제21권4호
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• pp.588-592
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• 2012

This study concentrates the effect of hybridisation on the collapse mode and energy absorption for composite cylinders. The static collapse behavior of laminated(Al/CFRP/GFRP) circular-cylindrical composite shell under quasi-static axial compressive load has been investigated experimentally. Eight different hybrids of laminated(Al/CFRP/GFRP) circular-cylindrical composite shell were fabricated by autoclave. Eight types of composites were tested, namely, Al/carbon fiber/epoxy, Al/glass fiber/epoxy, Al/carbon-carbon-glass/epoxy, Al/carbon-glass-carbon/epoxy, Al/carbon-glass-glass/epoxy, Al/glass-glass-carbon/epoxy, Al/glass-carbon-glass/epoxy and Al/glass-carbon-carbon/epoxy. Collpase modes were highly dominated by the effect of hybridisation. The results also showed that the hybrid member with material sequence of Al-glass-carbon-carbon/epoxy exhibited good energy absorption capability.

• Composites Research
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• 제12권1호
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• pp.47-58
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• 1999

다양한 형상 및 경계조건을 갖는 적층 복합재료 및 혼합적층 복합재료 판의 자유진동해석을 위한 실험적 연구결과에 대하여 고찰하였다. 실험에 사용한 판의 재료는 탄소섬유강화(CFRP), 유리섬유강화(GFRP) 복합재료, 알루미늄-GFRP, CFRP-GFRP 혼합적층 복합재료이다. 충격해머와 가속도계를 이용한 충격가진법을 통하여 판의 고유진동수 및 노달패턴을 얻었고, 결과는 무차원화된 진동수매개변수로 제시하였다. 복합재료의 물성, 적층강도, 판의 기하학적 형상과 경계조건 등이 복합재료 판의 진동특성에 미치는 영향에 대하여 평가하였다. 실험결과의 비교/검증을 위하여 유한요소해석을 수행하였고, 서로 잘 일치함을 보였다.

• Tribology and Lubricants
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• 제36권3호
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• pp.133-138
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• 2020

In this paper, we present an experimental investigation of the friction coefficient and wear area change of carbon/epoxy and E-glass/epoxy composites depending on the fiber direction (0°/90°). We compared the results of the case where the sliding direction is parallel to the fiber direction (0°) with that of the case where it is perpendicular to the fiber direction (90°). The ball-on-plate wear test equipment was used to cause wear in both directions. Two types of specimens were prepared with thicknesses of 3 mm-one made of carbon fiber reinforced plastic composite (CFRP) and the other of glass fiber reinforced plastic composite (GFRP). A normal force of 20 N was applied to the specimen and the sliding speed was 10 mm/s and the sliding distance was set to 20 m to perform the wear test. The CFRP demonstrates superior tribological characteristics compared to the GFRP. This outcome is attributed to graphitization of carbon, which serves as solid lubricating particles. In addition, both CFRP and GFRP are worn more in the 90° direction than in the 0° direction. This is due to the greater occurrence of fiber breakage and separation in the 90° direction than in the 0° direction. This study is expected to be utilized as basic data for understanding the friction and wear characteristics of CFRP and GFRP composites along the fiber direction and to apply the appropriate material.

• 대한금속재료학회지
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• 제50권2호
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• pp.93-99
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• 2012

The mechanical properties of nano composites were evaluated for structural performance in order to enhance their applicability to the car and machine industrial fields. Carbon fiber reinforced plastics (CFRP) and GFRP were manufactured by vacuum-assisted resin transfer molding (VARTM) process with good mechanical properties. Tensile test was conducted to obtain the process factor of each composite. Also, carbon nano fiber (CNF) was dispersed in the composites and the relationship between the mechanical property and the CNF fraction was compared. The tensile strength and stiffness of 0/90 laminated CFRP were the best. CFRP/CNF (0.5 wt.%) was confirmed to be an excellent material for its elasticity and tensile strength.

• 동력기계공학회지
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• 제19권4호
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• pp.17-23
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• 2015

Because of the energy resources shortage and global pollution, the wind power systems have been developed consistently. Among the components of the wind power system, the rotor blades are the most important component. Generally it is made of GFRP material. Recently, GFRP material has been replaced by CFRP composite material in the blade which has an aerodynamic profile and twisted tip. However the failures has occurred in the trailing edge of the blade by the severe wind loading. Thus, tougher material than CFRP material is needed as like the aramid fiber. In this study, we investigated the mechanical behaviors of the blade using aramid fiber composites about wind speed variation. One-way FSI (fluid-structure interaction)analysis for the wind rotor blade was conducted. The structural analyses using the surface pressure loading resulted from wind flow field analysis were carried out. The results and analysis procedure in this paper can be utilized for the best strength design of the blade with aramid fiber composites.

• Composites Research
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• 제34권1호
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• pp.35-46
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• 2021

본 논문은 차량에 사용되는 B필러의 강화재를 기존의 스틸 소재에서 CFRP(Carbon Fiber Reinforced Plastics)와 GFRP(Glass Fiber Reinforced Plastics)로 대체하여 경량화하는 것이 목표다. 이를 위해서는 무게는 감소시키면서 기존 B필러를 대체할 수 있는 구조안정성을 확보해야 한다. 기존 B필러는 스틸 아우터(outer)를 포함하여 다양한 형상의 스틸 강화재로 구성되며, 이와 같은 스틸 강화재 중 2가지의 스틸 강화재를 복합재로 대체하고자 한다. 이와 같은 스틸 강화재는 강화재 각각을 따로 제작하여 용접을 통해 결합되지만, 복합재 강화재는 패치(patch) 형태의 CFRP와 리브(rib) 구조의 GFRP를 활용하여 압축과 사출 공정을 통해 한번에 제작된다. CFRP는 B필러의 고강도부에 부착되어 측면 하중에 저항하도록 하였으며, GFRP 리브는 위상 최적화(Topology optimization) 기법을 통해 비틀림과 측면 하중을 저항하도록 설계하였다. 구조해석을 통해 기존 스틸 강화재와 비교 분석을 수행하였고, 경량화율을 산출하였다.

• Composites Research
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• 제35권6호
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• pp.447-455
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• 2022

현재 해양 미세플라스틱에 의한 해양 환경 오염문제가 국제적으로 심각하게 대두되고 있다. 이와 관련하여 본 연구에서는 휴대용 미세플라스틱 수거 장비의 경량화 개발을 위해 대한민국 전국 21개소 해안가에서의 미세플라스틱종류와개수를조사하였고, 미세플라스틱수거장비진공장비의내구성, 내부식성, 경량화를위해 CFRP(Carbon Fiber Reinforced Plastic), GFRP(Glass Fiber Reinforced Plastic), ABS(Acrylonitrile Butadiene Styrene copolymer), aluminum과 같은 다양한 소재를 적용하여 설계 및 해석을 수행하였다. 해안가에서의 시료 채취 및 분류결과 함덕해수욕장에서 미세플라스틱이 가장 많이 분포되어 있는 것을 확인하였고, 주로 폴리스타이렌(Polystyrene)의 미세플라스틱이 분포되어 있는 것으로 나타났다. 해안가 현장 조사를 통한 입자정보 분석과 전산유체해석을 통해 모래 및 불순물 등의 입자 유동속도 및 분포를 분석하였고, 이를 진공 본체 내부의 중요 부품인 싸이클론 장치의 구조해석에 적용하였다. 싸이클론 장치의 모래 및 불순물 흡입 시 발생되는 입자 충격을 고려한 구조해석 결과 CFRP, GFRP, aluminum, ABS의 순으로 구조적 안전성이 우수한 것으로 평가되었다. 경량화 측면으로는 싸이클론 장치에 aluminum 소재를 적용했을 때와 비교하여 CFRP는 53%, GFRP는 47%, ABS는 61%의 경량화가 가능한 것으로 나타났다.

• Composites Research
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• 제22권3호
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• pp.1-8
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• 2009

이 논문에서는 강수도관에 사용되는 GFRP관의 구조적 거동에 대한 실험적, 이론적 연구의 결과를 제시하였으며, 관의 단면은 두개의 CFRP층과 그 층 사이의 폴리머 모르타르 층으로 구성되어 있다. GFRP는 경량성, 부식저항성, 관의 내부 표면조도 향상, 유연성 등이 뛰어나기 때문에 강수 계통의 관으로써 시용이 계속적으로 증가되고 있는 추세이다. 그러므로 더욱 최적화된 구조설계법이 개발되어야 한다. 이 연구에서 CFRF관의 하중-원주방향변위에 대한 특성을 이론적, 해석적으로 조사 하였으며 추가적으로 원강성시험을 하였다. 시험결과를 이론적, 해석적 연구결과와 비교하였으며, 원주방향의 변위가 5% 이내에서는 결과들이 서로 잘 일치하였다. 결과적으로 상수도 계통에 사용되는 CFRP관은 업계의 요구조건을 충분히 만족함을 알 수 있었다.

• Steel and Composite Structures
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• 제15권3호
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• pp.267-279
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• 2013

This article describes a simple and cost effective fabrication procedure by using hand lay-up technique that is employed for the manufacturing of thin-walled axi-symmetric composite shell structures with carbon, glass and hybrid woven fabric composite materials. The hand lay-up technique is very commonly used in aerospace and marine industries for making the complicated shell structures. A generic fabrication procedure is presented in this paper aimed at manufacture of plain Carbon Fabric Reinforced Plastic (CFRP) and Glass Fabric Reinforced Plastic (GFRP) shells using hand lay-up process. This paper delivers a technical breakthrough in fabrication of composite shell structures without any joints and wrinkling. The manufacture of stiffened CFRP shells, laminated CFRP shells and hybrid (carbon/glass/epoxy) composite shells which are valued by the aerospace industry for their high strength-to-weight ratio under axial loading have also been addressed in this paper. A fabrication process document which describes the major processing steps of the composite shell manufacturing process has been presented in this paper. A study of microstructure of the glass fabric/epoxy composite, carbon fabric/epoxy composite and hybrid carbon/glass/fabric epoxy composites using Scanning Electron Microscope (SEM) has been also carried out in this paper.

• 한국안전학회지
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• 제29권6호
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• pp.9-14
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• 2014

Recently many efforts and researches have been done to cope with industrial facilities that require a low energy machines due to the gradual depletion of the natural resources. The fiber-reinforced composite materials in general have good properties and have the proper mechanical properties according to the change of the ply sequences and fiber distribution types. However, in the fiber-reinforced composite material, there are several problems, including fiber breaking, peeling, layer lamination, fiber cracking that can not be seen from the metallic material. Particularly, the fracture and delamination are likely to be affected by the thickness of the stacking laminates when the bi-material laminated structure is subjected to a load of the mixed mode. In this study, we investigated the effect of the thickness ratio of the difference in the CFRP/GFRP bi-material laminate composites by measuring the cracking behavior and the AE characteristics in a mixed mode loading, which may be generated in the actual structure. The results show that the thickness of the CFRP becomes more thick, the mode I energy release rate becomes a larger, and also the influence of mode I is greater than that of mode II. In addition, AE amplitude which shows the level of the damage in the structure was obtained the more damage in the CFRP with the thin thickness.