• 기계와재료
• /
• v.21 no.4
• /
• pp.6-15
• /
• 2010

탄소/탄소 복합재료는 해외에서의 기술/부품 도입 자체부터 엄격히 통제되는 국가의 미래 전략산업의 핵심소재로서 $2,000^{\circ}C$ 이상의 고온에서 지속적으로 내열성 및 내산화성이 요구되는 우주항공 분야, 초고온에서 고순도 및 내 삭마성 등이 요구되는 원자로/핵융합로 분야, 고순도 및 고온 열처리가 요구되는 반도체 제조 및 진공 열처리로 분야에서 기존의 내열합금 또는 세라믹 재료로는 한계에 도달한 성능을 획기적으로 향상시킬 수 있는 재료이다. 본고에서는 탄소/탄소 복합재료의 구성재료, 제조방법, 기본적인 물성치 등에 대한 기술적 내용을 소개하고, 현재 및 미래의 응용분야에 대하여 알아보았다. 또한 국내외 기술동향 분석을 통하여 국가의 전략 소재의 독자적인 개발과 일반산업으로의 상용화에 대하여 탄소/탄소 복합재료가 나아가야 할 방향을 제시하고자 하였다.

• Composites Research
• /
• v.18 no.3
• /
• pp.1-6
• /
• 2005

Carbon nanofiber exhibits superior and of ien unique characteristics of mechanical, electrical, chemical and thermal properties. Despite of the excellent properties of carbon nanofiber, the properties of carbon nanofiber filled polymer composites were not increased largely. The reason is that it is still difficult to ensure the uniform dispersion of carbon nanofiber in a polymer matrix. In this study, for improvement of the mechanical properties of composites, carbon nanofiber reinforced hybrid composites was investigated. For the dispersion of carbon nanofiber. solution blending method using ultrasonic was used. Dispersion of carbon nanoifiber was observed by scanning electron microscope (SEH). Mechanical properties were measured by universal testing machine(UTM).

• Composites Research
• /
• v.20 no.4
• /
• pp.18-24
• /
• 2007

The mechanical and thermal properties of PAN-based/rayon-based carbon fabrics interply hybrid composite materials have been studied. Mechanical properties including tensile and interlaminar shear strengths were improved with increasing amount of continuous PAN-based carbon fabrics. The erosion rate and insulation index were determined through the torch test. Continuous rayon-based carbon fabrics composite indicated relatively low ablation resistant property. The thermal conductivity of hybrid composite of spun PAN-based/continuous rayon-based carbon fabrics is lower than that of the continuous PAN-based carbon fabrics composite.

• Proceedings of the Computational Structural Engineering Institute Conference
• /
• 2010.04a
• /
• pp.554-557
• /
• 2010

본 논문에서는 동일한 체적분율 가지는 탄소나노튜브 나노복합재의 기계적 특성을 규명하였다. 동일한 chirality를 가지는 서로 다른 크기의 탄소나노튜브를 이용하여 탄소나노튜브의 크기가 복합재의 물성에 미치는 영향을 규명하였다. 복합재료의 분자동역학의 결과 탄소나노튜브의 길이방향의 물성은 크게 증가하나, 전단특성의 물성 강화효과를 나타나지 않았다. 이는 통해 탄소나노튜브와 기지재료 사이의 상호작용력이 복합재료의 전단력을 전달하고, 변형을 유지할 만큼 강하지 않다는 것을 확인하였다. 이와 같은 분자동역학 결과를 바탕으로 멀티스케일 모델을 개발하여 복합재료에서 나타나는 현상을 묘사하였다. 제안된 멀티스케일 모델을 이용하여 다양한 조건의 복합재료에 대한 특성 예측이 가능하다.

• Polymer(Korea)
• /
• v.28 no.4
• /
• pp.285-290
• /
• 2004

Nondestructive damage sensitivity of carbon nanotube(CNT) and nanofiber (CNF)/epoxy composites with their adding contents was investigated using electro-micromechanical technique. Carbon black (CB) was used only for the comparison with CNT and CNF. The fracture of carbon fiber was detected by acoustic emission (AE), which was correlated to the change in electrical resistance, ΔR under double-matrix composites (DMC) test. Stress sensing on carbon nanocomposites was performed by electro-pullout test under uniform cyclic loading. At the same volume fraction, the damage sensitivity for fiber fracture, matrix deformation and stress sensing were highest for CNT/epoxy composite, whereas for CB/epoxy composite they were the lowest among three carbon nanomaterials (CNMs). Damage sensitivity was correlated with morphological observation of carbon nanocomposites. Homogeneous dispersion among CNMs could be keying parameters for better damage monitoring. In this study, damage sensing of carbon nanocomposites could be evaluated well nondestructively by the electrical resistance measurement with AE.

• Polymer(Korea)
• /
• v.24 no.2
• /
• pp.237-244
• /
• 2000

Phenolic resin used as a precursor of carbonized matrix for carbon-carbon composites was modified by addition of molybdenum disilicide (MoSi$_2$) in various concentrations of 0, 4, 12 and 20% by weight to improve the anti-oxidation properties of the composites. The green body was manufactured by a prepreg method and was submitted to carbonization up to 110$0^{\circ}C$. In this work, the oxidation behavior of carbon-carbon composites with MoSi$_2$ as an oxidation inhibitor was investigated at the temperature range of 600-100$0^{\circ}C$ in an air environment. The carbon-carbon composites with MoSi$_2$ showed a significantly improved oxidation resistance due to both the reduction of the porosity formation and the formation of mobile diffusion barrier for oxygen when compared to those without MoSi$_2$. Carbon active sites should be blocked, decreasing the oxidation rate of carbon. This is probably due to the effect of the inherent MoSi$_2$ properties, resulted from a formation of the protective layer against oxygen attack in the composites studied.

• Composites Research
• /
• v.26 no.3
• /
• pp.147-154
• /
• 2013

Nanocarbons such as carbon nanotubes (CNT) and graphene are considered to be ideal fillers for polymer composites, because of their outstanding mechanical properties and high length-to-diameter ratio. There has been much effort to realize the implementation of their full potential, but a large number of unsolved problems still must be challenged, for example, effective processing for fabrication. This review deals with the progress that has already been made in the area of nanocarbon polymer composites using CNT and graphene. Mechanical reinforcement of various nanocarbon polymer composites is analyzed and compared, and future perspectives in research and development that need to be done are discussed.

• Proceedings of the Computational Structural Engineering Institute Conference
• /
• 2009.04a
• /
• pp.18-20
• /
• 2009

입자 강화 복합재료 내에서의 다양한 손상 메커니즘은 복합재료의 전체 거동을 예측에 상당한 영향을 미친다. 이에 본 연구에서는 입자 강화 복합재료 내에서의 누적 손상을 고려한 미세역학 기반 탄소성 모델(Kim and Lee, 2009)을 소개하고자 한다. Kim and Lee (2009)에 의해서 입자 강화 복합재료의 탄소성 모델을 위해 입자 강화 복합재료 내 계면에서의 누적 손상 및 기지재의 연성 거동이 고려되었다. 제안된 모델을 이용한 입자 강화 복합재료의 탄소성 거동 예측값은 관련된 실험값 (Llorca et al., 1991)과의 비교를 통해 수치해석을 수행하였다.

• Composites Research
• /
• v.13 no.2
• /
• pp.72-80
• /
• 2000

Effect of graphite powder addition on the mechanical properties of carbon fiber reinforced carbon composites (C/C composites) was investigated. Greenbody (G/B) with 0~30wt.% graphite powder addition to phenol resin was prepared and carbonized at $1000^{\circ}C$ to make C/C composites. Flexural strengths of 20wt.% graphite powder additions showed maximum values in the both case of G/B and C/C composites. But, at the graphite addition over 20wt.%, there was negative effect due to the matrix inhomogeneity. Flexural strength of cured resin without graphite Powder was higher than that with graphite. However, flexural strength of carbonized resin with graphite increased three times as much as that of carbonized resin without graphite. Because the addition of graphite powder effects the restraint of shrinkage after carbonization and the deflection of crack path. In Mode II ENF test, energy release rates($G_{II}$) of G/B and C/C composites with the 20w1.% addition of graphite were both increased. But, the addition of graphite was more effective to the increase of $G_{II}$ in C/C composites than that in G/B.

• Polymer(Korea)
• /
• v.25 no.6
• /
• pp.866-875
• /
• 2001

In this work, thermal decomposition mechanism based on kinetic parameters and thermal stability of carbon fiber-reinforced carbon matrix composites (C/C composites), have been studied under high temperature oxidative conditions with addition of tetra-ethylorthosilicate (TEOS) as an oxidation inhibitor. Thermogravimetric analysis (TGA) was executed to evaluate the thermal decomposition mechanism and thermal stability of C/C composites in the temperature range of 30 ～ $850^{\circ}C$. As a result, the kinetic parameters of the composites impregnated with TEOS, i.e., activation energy for thermal decomposition ($E_d$), order of reaction (n) , and pre-exponential factor (A) were evaluated as 136 kJ/mol, 0, and 2.3$\times$$10^9s^{-1}$, respectively. Especially, the IPDT and $E_d$ of C/C composites impregnated with TEOS were improved largely compared with the composites impregnated without TEOS, due to the formation of $SiO_2$ on composite surfaces, resulting in interrupting the oxygen attack to carbon active site in the composites.