• 공업화학
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• 제23권3호
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• pp.339-343
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• 2012

우수한 기계적 강도를 가지고 있는 폴리올레핀케톤 고분자를 합성하고, 우레탄과 아미노실란으로 표면 처리 된 유리섬유를 도입하여 엔지니어링 플라스틱용 복합재료를 제조하였다. 유리섬유와 폴리올레핀케톤의 상용성을 확인하기위해 주사 전자 현미경으로 복합재료의 파단면 형상을 확인하였고, 함유된 유리섬유의 크기와 양, 그리고 바인더의 종류에 따른 복합재료의 기계적 물성을 관찰하였다. 적절한 표면처리를 한 유리섬유로 강화된 폴리올레핀케톤 복합재료는 좋은 계면 상용성을 보이며 향상된 기계적 강도를 가지고 엔지니어링 플라스틱 분야에서의 응용 가능성을 확인 할 수 있었다.

• 한국군사과학기술학회지
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• 제18권3호
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• pp.293-299
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• 2015

We analyzed the damage effect on Glass Fibre Reinforced Plastics(GFRP) under air flow by irradiation of continuous wave near-IR laser. Damage process and temporal temperature distribution were demonstrated and material characteristics were observed with laser intensity, surface flow speed and angle. Surface temperature on GFRP rapidly increased with laser intensity, and the damaged pattern was different with flow characteristics. In case of no flow, penetration on GFRP by burning and flame generation after laser irradiation was appeared at once. GFRP was penetrated by the heat generated from resin ignition. In case of laser irradiation under flow, a flame generated after burning extinguished at once by flow and penetration pattern on GFRP were differently shown with flow angle. From the results, we presented the damage process and its mechanism.

• 한국공간구조학회지
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• 제5권1호
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• pp.20-26
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• 2005

기존의 고정관념의 틀을 깨고 새로운 것을 추구하는 인류의 행태는 보다 뛰어난 기술을 잉태하는 모체가 되어왔다. 그럼에도 불구하고 많은 건축 재료들 가운데서 플라스틱을 이용한 건축재료는 풍부한 가능성과 장점에도 불구하고 기존재료에 대한 고정관념에 사로잡혀 다른 분야에 비해 그 발전 속도가 현격하게 떨어지고 있는 것이 사실이다. 다시 말해 우리 주변의 실제 구조물에 훌륭히 적용할 수 있는 가능성을 쉽게 놓쳤다고 말할 수 있는 것이다. 따라서 본 슈트트가르트대학교 건축학과 구조디자인 연구실에서는 유리강화플라스틱 (GFRP)를 이용해서 본 재료가 갖고 있는 장점을 최대한 살려 실제 구조물에 적용할 수 있는 가능성을 찾고 연구하고자 한다. 이를 위해 총 2회에 걸쳐 기존의 연구동향과 적용 가능성을 검토하고 본 연구실에서 이루어지고 있는 Prototyp을 소개하고자 한다.

• 대한기계학회논문집A
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• 제38권8호
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• pp.849-855
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• 2014

유리섬유강화 플라스틱 복합재료의 압축성형 시, 모재와 유리섬유의 분리 없이 유동성이 우수하고, 불균질한 섬유배향이 없는 GFRP 복합재료 개발에 관한 체계적인 연구결과는 미흡한 실정이다. GFRP 복합재료를 사용하여, 자동차 부품 성형 시 발생하는 불균질도와 섬유배향 발생을 억제하는 많은 연구를 해왔으나 아직 해결되고 있지 않다. 본 연구에서는 위의 문제점들을 해결하기 위해 섬유유동성이 뛰어나고, 섬유배향이 발생하지 않고, 불균질성이 없으며, 구조안정성, 함침도, 기계적 특성 및 재활용성 등이 우수한 유리섬유강화 플라스틱 프리프레그를 제조하여, 수직교차형 평직직조방법을 적용하여, GFRP(Glass Fiber Reinforced Plastic) Sheet 를 제조한다.

• 한국해양공학회지
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• 제16권4호
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• pp.48-53
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• 2002

Fiber-reinforced composites are extensively used in electronic, ship and aerospace applications due to their high strength and high toughess. In these applications, they are often subjected to localized heat damage due to various sources. In order to ensure their reliability, it is important to predict their residual properties using nondestructive evaluation thchniques. Fabric fiber composite specimens were manufactured with six layers of the glass-fiber prepreg and the carbon-fiber prepreg, respectively. The specimens were subjected to a localized heat damage using a heated copper tip with a diameter of 10mm at 35$0^{\circ}C$(CFRP) and 30$0^{\circ}C$(GFRP), respectively. The specimens were then subjected to tension tests while acoustic emission (AE) activities of specimens were collected. The AE activity of all specimens showed three types of distinct frequency regions. Those are matrix cracking, failure of the fiber/matrix interface and fiber breakage.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집A
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• pp.616-622
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• 2001

In this paper, we analyzed the laminated composite sandwich plate structure of honeycomb core with changing values of the designing parameters. As a result, in designing parameters of that, the more height and thickness of the laminated composite plate's core, the more increase of natural frequency. The laminated angle has the maximum value when the plate of honeycomb core is join to opposite direction. This paper shows that the natural frequency of CFRP is higher than that of GFRP, and also impact strength marks maximum value in case of antisymmetry than symmetry of core. Also it shows that the mode shapes are various along with the angle-ply of laminated composite plate.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2001년도 추계학술대회논문집A
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• pp.703-709
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• 2001

In this paper, we analyzed the laminated composite sandwich plate structure of truss core with changing values of the designing parameters. As a result, in designing parameters of that, the more height and thickness of the laminated composite plate's core, the more increase of natural frequency. In this type of structure, in the case of applying core of the laminated composite plate and antisymmetric stacking, natural frequency has high value and we calculated the optimum angle-ply making natural frequency maximum. Natural frequency of CFRP is higher than that of GFRP. Both are materials of the laminated composite plate. The mode shapes are various along with the angle-ply of the laminated composite plate.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 1997년도 추계학술대회 논문집
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• pp.710-715
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• 1997

This paper deals with the analysis of the optimum value of honeycomb core considering variable design parameter. As thickness and height of core rises in design parameter, natural frequency of laminated composite plate increases. The angle-phy has the maximum value when the plate of honeycomb core join to opposite direction. This paper shows that the natural frequency of CFRP was higher than that of GFRP and mode shapes were various at angle-ply.

• 한국항공운항학회지
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• 제17권4호
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• pp.42-47
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• 2009

Recently, the wide range of the composite materials is used for the making airplanes, trains and automobiles body for the lightweight. Despite having complex structures, composite materials usually have well defined mechanical characteristics. However, composite materials are difficult to understand the fracture mechanism clearly by simple mechanical test. Nondestructive evaluation (NDE) combined with mechanical testing can play a more important role and especially Acoustic Emission Testing (AET) would become known to be a useful tool to assess damage and fracture behavior of composites. In this study The experiment was performed to acquire the acoustic emission signal during tensile test using unidirectional CFRP specimen and the data was analyzed the acoustic emission parameters with the waveform.

• 대한기계학회논문집A
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• 제32권9호
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• pp.788-795
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• 2008

To understand the tensile behaviors of GFRP at low temperature, three types of specimen have been used in this study. Tensile properties and fracture mechanisms for three orthogonal orientations of plain weave glass fabric reinforced epoxy resin laminate were investigated at temperature range of about -30 to $15^{\circ}C$. The tensile properties of axial and edge type specimen decrease slightly with decreasing temperature to $-20^{\circ}C$. However, at $-30^{\circ}C$ the decreases in the tensile properties increased considerably. Below $-20^{\circ}C$, thickness type specimen showed a marked decreases in the tensile properties. It was obvious that the fracture manner of thickness type specimen was adhesive failure at above $-10^{\circ}C$ and a mixed adhesive and cohesive failure at below $-20^{\circ}C$.