• Korean Journal of Materials Research
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• v.8 no.2
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• pp.161-164
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• 1998

탄소섬유-에폭시 복합재료의 전파 반사특성을 전파전송 이론에 근거하여 해석하였다. 탄소섬유 복합재료의유전상수를 투과/반사법에 의해 4-12GAz 주파수 범위에서 측정하였다. 측정된 재료정수로부터 반사손실을 시편의두께와 주파수의 함수로 계산하였다. 탄소섬유 복합재료는 높은 유전상수와 도전손실 특성에 의해 전파의 반사율이 매우 높았다. 그러나 파장에 비해 시편의 두께가 작은 경우 반사손실은 두께에 매우 민감하였으며, 이는 입력 임피던스의 변화에 기인하는 것으로 해석되었다. 이러한 결과로부터 전자파 차폐를 극대화시키기 위해서는 특히 저주파 대역에서 시편의두께 조절이 매우 중요함을 제시할 수 있었다.

• Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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• 1998.04a
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• pp.64-68
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• 1998

본 연구에서는 다양한 종류의 섬유를 일방향으로 배향시켜 제작한 복합재료의 트라이볼로지 연구를 수행하였으며 특히 섬유의 배향과 활주속도가 트라이볼로지 성질에 미치는 영향을 연구하였다. 실험에 쓰인 시편은 유리 섬유, 아라미드 섬유, 그리고 고탄성 탄소 섬유를 보강재료로 에폭시 수지를 모재로 사용한 일방향섬유 복합재료이며 각각의 시편을 스테인레스 강 상대 마찰면에 마찰시켜 마모량과 마찰 계수를 구하였다. 실험조건으로 사용한 여러 활주속도에서 탄소섬유복합재료가 모든 섬유배열방향에서 아라미드섬유복합재료와 유리섬유 복합재료보다 마모율과 마찰계수가 낮은 경향을 보였으며 특히 높은 속도에서는 탄소섬유복합재료의 특성이 뛰어남을 알 수 있었다.

• Journal of the Korean Society for Nondestructive Testing
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• v.21 no.3
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• pp.313-318
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• 2001

To establish nondestructive test method for aerospace composite materials, various composite specimens were tested and analyzed using acoutic emission. The hit rate of acoustic emission closely was rotated with crack initiation and propagation. This report also presents defection capability of crack initiation pressure, initial crack active location, and crack propagation using acoustic emission.

• Composites Research
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• v.36 no.3
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• pp.193-198
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• 2023

Currently, there are many discussions about composite materials and 3D printed composite material to weight reduction of ships. A test was conducted to confirm the applicability of the 3D printed composite material to ships and offshore structures by linking the 3D printing technology with excellent productivity and the composite material with corrosion resistance and lightweight characteristics in salt water environments. In order to apply the 3D printed composite material used in this paper to ships and offshore structures, the temperature environmental effects that can be exposed in the marine environment should be considered. Therefore, the tensile test was conducted with specimen of Carbon + Onyx, Carbon + Nylon, HSHT glass + Onyx, HSHT glass + Nylon material in low temperature (-50℃), room temperature (20℃), and high temperature (50℃) environments that can be exposed to the marine environment. As a result of the tensile test, the carbon + onyx specimen showed the highest tensile strength and the HSHT glass + onyx specimen showed the highest tensile strain. In addition, by analyzing the tested specimens, the failure mode of the 3D printed composite material specimens exposed to various temperature environments was analyzed.

• Composites Research
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• v.29 no.5
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• pp.306-314
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• 2016

In this study, to improve the thermal stabilities of the epoxy composite specimens in addition to the enhanced mechanical properties, those were reinforced with carbon nanotubes and micrometer-sized silica particles. To disperse the filler in matrix relatively simple physical process, specimens were fabricated using shear mixing and sonication. Tensile strength, coefficients of thermal expansion and thermal conductivity of the specimens were measured with varied contents of the two fillers. The mechanical and thermal properties were also discussed, and the experimental results of thermal expansion related to the thermal stability of the specimens were compared with those from several micromechanics models. The hybrid composites specimens incorporating 0.6 wt％ of carbon nanotubes and 50 wt％ of silica particles showed better mechanical properties than the others with increase in tensile strength up to 11％, with respect to those of the baseline specimens. As the silica contents were increased the thermal expansion was reduced down to 36%, and the thermal stability was improved with the decreased thermal deformation. Thermal conductivity of the epoxy composite specimens incorporating 50 wt％ of silica particles was enhanced, which demonstrate improvement of 72%. The mechanical and thermal properties of the hybrid composites specimens incorporating the two fillers were improved simultaneously.

• Composites Research
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• v.22 no.1
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• pp.15-21
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• 2009

In this paper, static compressive test and compression-compression fatigue test of carbon/epoxy composites which have different micro-structures were carried out with respect to the bias angle. In order to find out the effect of the micro-structure of the fabric composite on compressive characteristics the specimens made of UD carbon/epoxy composite comprising the same fiber and matrix system as the fabric composite were also prepared. The compressive strength and modulus were measured and these values were used to develop a semi-empirical formula for predicting compressive strength of the fabric composite with bias angles. The fatigue behavior of the fabric composite with respect to the bias angle variation was also investigated.

• Composites Research
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• v.35 no.6
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• pp.463-468
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• 2022

The high porosity of the infill pattern of carbon chopped fiber-reinforced Nylon composite structures fabricated by the fused filament fabrication (FFF) type 3D printers determines the mechanical performance of the printed structures. This study experimentally evaluated the mechanical performance of Onyx composite specimens fabricated with a rectangular infill structure under the hot-pressing condition to improve the mechanical properties by reducing the porosity of the infill pattern of the printed structure, and evaluated the best mechanical performance. The hot-pressing conditions (145℃, 4 MPa, 12 min) that induce the most appropriate mechanical properties were found. As a result of microscopic observation, it was confirmed that the infill porosity of the composite specimens subjected to post hot-pressing treatment was effectively reduced. In order to confirm the mechanical performance of the post-treated specimen, a tensile test and a three-point bending test were performed with a control specimen without post-treatment and a specimen printed with the same density and dimensions after post-treatment to evaluate the mechanical properties. As a result of comparison, it was confirmed that the mechanical properties were effectively improved when the post-treatment of hot-pressing was performed.

• Proceedings of the Materials Research Society of Korea Conference
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• 2012.05a
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• pp.106.1-106.1
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• 2012

EBSD(Electron BackScattered Diffraction)분석은 주사전자현미경에서 관찰되는 비교적 넓은 영역의 결정 방위를 측정하여 집합조직을 해석하는 동시에 결정 방위의 변화를 기준으로 결정립계를 구분 지어 미세조직의 정량 분석도 가능하기 때문에 많은 연구자들이 사용하고 있다. 그러나 EBSD의 Kikuchi 패턴은 시편 표면으로부터 30~50nm 깊이 범위의 표면층으로부터 방출되기 때문에 EBSD 분석 결과는 시편의 표면 처리 상태에 크게 영향을 받아 적절한 시편준비법이 요구된다. 시편 준비 과정 중에 생기는 변형층, 산화층이나 오염층이 10nm 이내로 제어되지 못하면 명확한 패턴을 얻지 못하여 분석이 어려운 경우가 많으므로, 시료의 절단과 연마 과정 중에 변형층을 되도록 적게 만들고 표면의 산화나 오염을 최대한 방지해야 한다. 또한 EBSD 분석 특성상 시편을 70도로 기울이기 때문에 시편의 요철이 심하면 볼록한 영역에 의해 오목한 영역의 패턴이 가려져 결정방위 정보를 얻기 힘들다. 이런 이유로 시편을 최대한 평평하게 하고 요철이 생기지 않게 시편 준비를 하는 것이 관건이다. 금속재료의 EBSD 시편준비법으로는 일반적으로 기계적 연마법과 전해연마법이 주로 쓰인다. 경한 석출물이나 개재물이 연한 기지에 분산되어 있는 시편이나 이종 소재 접합재의 경우는 전해연마법을 사용하면 특정 상(혹은 합금)이 먼저 연마되어 큰 단차가 생기거나 석출물에 의해 요철이 심해져서 정량적인 EBSD 분석이 어렵게 된다. 이 연구에서는 시편 준비가 어렵다고 알려진 다상 금속재료에서의 EBSD 분석 사례를 소개한다. Ti-6Al-4Fe-0.25Si 시효처리합금, 알루미늄 기지 복합재료, 마찰교반용접한 알루미늄-타이타늄합금의 EBSD 시편준비법과 그 분석 결과를 고찰한다.

• Composites Research
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• v.16 no.4
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• pp.29-35
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• 2003

In this paper. various tow parameters such as equivalent tow thickness, amplitude of longitudinal tow and tow intervals were investigated and compared with each other by using microscopic observation to find out the exact deformation patterns between both directions of the fabric structure(Longitudinal and Transverse Directions). And those observation results were compared with bias extension. biaxial tests results with dry fabric which has the same tow structure as the draped helmet materials and also compared with prepreg specimen which is cured by autoclave moulding without vacuum and pressure condition. Specimens for the observation were taken from draped helmet which is made of fabric composite(Five Harness Satin Weave). From the observation results, it was found that there are different deformation pattern between tow directions and effect of geometric condition on the deformation of the fabric materials during draping process was verified.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1999.04a
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• pp.27-27
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• 1999

본 연구에서는 초음파 Immersion법을 이용하여 복합재 연소관내에 존재하는 결함을 검출하는 방법에 대하여 연구하였으며, 이를 위하여 FRP의 delamination, FRP-EPDM간의 미접착을 모사한 모의 결함 시편을 제작하여 시험하였다. 먼저 복합재료에 대한 초음파 시험방법을 최적화하기 위하여 가장 검출 감도가 좋은 탐촉자의 적용 주파수조건 및 물거리를 구하였으며, 이들 최적 조건으로 모의 결함 시편을 A, B, C-Scan하여 결함을 검출 분석하였다. 그리고 시험 자료를 바탕으로 데이터 값을 분석함으로써 복합재료에서의 음파 속도, 음향 임피던스, 반사율 및 투과율 등 복합재료의 초음파 특성을 산출하였으며, 동 시편에 대한 X-ray 필름을 촬영하여 그 결과를 초음파 시험 결과와 비교 분석하였다.