• 한국세라믹학회지
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• 제33권12호
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• pp.1387-1393
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• 1996

A study on mesophase pitch as a matrix precursor of carbon fiber reinforced carbon (C/C) composite has been recently presented. This study is concerned with the production of mesophase pitch as matrix precursors for C/C composite from coal tar pitch. A commercial coal tar pitch was heat-treated at 25$0^{\circ}C$ for 2 hours to remove low molecular weight fraction from the pitch then increasing the temperature of the pitch to between 350~45$0^{\circ}C$ to produce mesophase pitch. The pitch was continuously stirred during this time and nitrogen gas was continuously bubbled through the pitch. Spherical and bulk mesophases were formed in the pitch after heat-treatment,. Parent and mesophae pitches were characterized by elemental analysis coke yield solubi-lity in tetrahydrofuran and hexane and an optical microscopy to measure the mesiophase content. It was neces-sary to produce C/C composite that a mesophase pitch with about 30-40 vol% mesophase spherulites can be infiltrated into a fiber preform without a filter effect as a matrix precursor conditions. This condition was satisfied with mesophase pitch heat treated at 40$0^{\circ}C$ for 2 hours. The other heat treatment conditions showed the nuclei of mesophase or bulk mesophae which were not satisfied with the matix precursor condition.

• Composites Research
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• 제33권3호
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• pp.115-124
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• 2020

적층복합재료, 특히 탄소섬유 복합재료는 금속에 비해 가벼우며 상대적으로 비강도 및 비강성이 뛰어나기 때문에 항공 우주 산업 및 자동차 산업 등과같이 광범위한 분야에서 사용되고 있다. 그러나, 적층 복합재료는 섬유의 배열이 모두 면내방향으로 배열되어있기 때문에 박리가 발생한다는 큰 단점이 있으며, 이는 적층복합재료의 응용분야를 제한한다. 본 연구에서는 먼저 π-빔과 평판이 결합된 형태의 적층복합재료 T-빔을 개발하고, 구조해석 및 기계적 물성평가를 통하여 설계변수를 최적화하였다. 이후 적층복합재료 T-빔의 설계변수를 3D 직조 프리폼에 동일하게 적용하여 T-빔을 개발하였으며, 적층구조에 비하여 향상된 기계적 강도를 달성할 수 있었다. 이러한 연구결과는 강도향상을 필요로 하는 기존의 적층복합재료 구조물에 적용 가능할 것으로 기대된다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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• pp.185-188
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• 2007

액체 및 고체추진기관의 내열부품으로 사용하기 위하여 Liquid Silicon Infiltration(액체 실리콘 함침) 공정이 적용된 C/SiC 복합재료를 개발하였다. 탄소섬유 및 탄소직물을 사용하여 필리멘트 와인딩, 테이프 롤링 및 인벌루트 적층 공법이 사용된 다양한 탄소 프리폼이 제작되었다. 내열 부품으로써의 열구조 성능을 극대화시키기 위하여 SiC 함유량, 열처리 조건, 수지 및 기상 함침 조건을 변화시키면서 시편을 제작하고 평가하였다. C/SiC 복합재료를 액체 및 고체추진기관의 내열부품으로 사용하기 위하여 연소시험을 수행하였으며 내열 성능 해석을 위한 수학적 삭마 모델이 개발되었다.

• 한국분말재료학회지
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• 제30권1호
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• pp.35-40
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• 2023

In this study, a graphite block is fabricated using artificial graphite processing byproduct and phenolic resin as raw materials. Mechanical and electrical property changes are confirmed due to the preforming method. After fabricating preforms at 50, 100, and 150 MPa, CIP molding at 150 MPa is followed by heat treatment to prepare a graphite block. 150UP-CIP shows a 12.9% reduction in porosity compared with the 150 MPa preform. As the porosity is decreased, the bulk density, flexural strength, and shore hardness are increased by 14.9%, 102.4%, and 13.7%, respectively; and the deviation of density and electrical resistivity are decreased by 51.9% and 34.1%, respectively. Therefore, as the preforming pressure increases, the porosity decreases, and the electrical and mechanical properties improve.

• 한국염색가공학회지
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• 제28권4호
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• pp.239-245
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• 2016

In this study, carbon/phenol composites were prepared from carbon fiber preform and phenol resin by RTM(resin transfer molding) process. And changes in the properties of the composite according to the pre-treatment of phenol resin was mainly studied. RTM process conditions were deduced from viscosity and thermal analysis of phenol resin which were rheometer and thermogravimetric analyzer(TGA). RTM process was performed under various injection and molding temperature. Characterization of the prepared C/P composites were evaluated by various analysis. Morphology of composites was analyzed by Micro-CT(MCT), Mechanical properties of composites were measured through the flexural properties. As results, volatile impurities of phenol resin were effectively removed at resin pre-treatment temperature of $100^{\circ}C$ and composite was sufficiently cured at molding temperature of $180^{\circ}C$.

• 한국세라믹학회지
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• 제48권4호
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• pp.288-292
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• 2011

In this study, we investigated the mechanical behavior of carbon fiber reinforced silicon carbide composites by indentation stress. Relatively porous and dense fiber reinforced ceramic composites were fabricated by liquid silicon infiltration (LSI) process. Densification of fiber composite was controlled by hardening temperature of preform and consecutive LSI process. Load-displacement curves were obtained during indentation of WC sphere on the carbon fiber reinforced silicon carbide composites. The indentation damages at various loads were observed, and the elastic modulus were predicted from unloading curve of load-displacement curve.

• Carbon letters
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• 제15권1호
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• pp.25-31
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• 2014

A microstructure analysis is carried out to optimize the process parameters of a randomly oriented discrete length hybrid carbon fiber reinforced carbon matrix composite. The composite is fabricated by moulding of a slurry into a preform, followed by hot-pressing and carbonization. Heating rates of 0.1, 0.2, 0.3, 0.5, 1, and $3.3^{\circ}C/min$ and pressures of 5, 10, 15, and 20 MPa are applied during hot-pressing. Matrix precursor to reinforcement weight ratios of 70:30, 50:50, and 30:70 are also considered. A microstructure analysis of the carbon/carbon compacts is performed for each variant. Higher heating rates give bloated compacts whereas low heating rates give bloating-free, fine microstructure compacts. The compacts fabricated at higher pressure have displayed side oozing of molten pitch and discrete length carbon fibers. The microstructure of the compacts fabricated at low pressure shows a lack of densification. The compacts with low matrix precursor to reinforcement weight ratios have insufficient bonding agent to bind the reinforcement whereas the higher matrix precursor to reinforcement weight ratio results in a plaster-like structure. Based on the microstructure analysis, a heating rate of $0.2^{\circ}C/min$, pressure of 15 MPa, and a matrix precursor to reinforcement ratio of 50:50 are found to be optimum w.r.t attaining bloating-free densification and processing time.

• 한국복합재료학회:학술대회논문집
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• 한국복합재료학회 2001년도 춘계학술발표대회 논문집
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• pp.38-41
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• 2001

A new 2-D braided textile metal matrix composite was developed and characterized. The constituent materials consist of PAN type carbon fiber as reinforcements and pure aluminum as matrices. The braided preforms of different braider yarn angles were fabricated. For a fixed bundle size of 12K, three braider yarn angles was selected: $30^{\circ}$, $45^{\circ}$, and $60^{\circ}$. The braided preforms were infiltrated with pure Al by vacuum assisted squeeze casting. Through the investigation of melt pressing methods and the effects of process parameters such as applied pressure, and pouring temperature, the optimal process conditions were identified as follows: applied pressure of 60MPa, pouring temperature of $800^{\circ}C$. Using the measured geometric parameters, 3-D engineering constants of metal matrix composites have been determined from the elastic model, which utilizes the coordinate transformation and the averaging of stiffened and compliance constants based upon the volume of each reinforcement and matrix material.

• Composites Research
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• 제18권5호
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• pp.27-33
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• 2005

본 연구에서는 펄스-CVI (Chemical Vapor Infiltration)에 의해 탄화규소/탄소 복합재료를 제조하는 공정에 대한 수치모사가 행해졌다. 각 펄스가 가스 주입시간, 반응시간, 배출시간으로 구성될 때, 반응시간과 배출시간의 영향이 관찰되었다. 또한 반응가스 농도와 압력의 영향이 연구되었다. 탄소프리폼에의 탄화규소의 균일한 침착과 반응시간 단축을 위한 펄스-CVI공정의 이점이 확인되었다.

• Composites Research
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• 제20권6호
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• pp.1-7
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• 2007

본 연구에서는 팽창흑연/탄소섬유 혼합 보강 전도성 고분자 복합재료를 2단계 성형 공법으로 제조하였으며, 탄소섬유의 첨가가 전도성 고분자 복합재료의 전기적, 기계적 특성에 미치는 영향을 고찰하였다. 전도성 충진재들은 고분자 수지와 기계적으로 혼합되었으며 이를 통하여 복합재료가 전기적 특성을 가지도록 하였다. 팽창흑연은 입자 간 접촉 면적이 넓기 때문에 복합재료 내 전도성 네트워킹의 형성에 매우 유리하지만, 팽창흑연과 고분자 수지만을 사용하여 상기 공정으로 복합재료를 제조할 경우 우수한 기계적 강도를 얻기가 어렵다. 따라서 이를 보완하기 위하여 탄소섬유를 복합재료에 첨가하였으며 전기적 기계적 물성을 바탕으로 탄소섬유의 혼합 비율을 최적화하였다. 굽힘 강도는 탄소섬유의 충친 비율이 증가할수록 섬유에 의한 강화 효과에 의하여 증가 하지만, 32wt.% 이상에서는 오히려 감소하였다. 이는 여분의 탄소섬유들이 공극을 발생시켜 응력집중이 발생하기 때문으로 판단된다. 전기 전도도는 탄소섬유의 비율이 증가할수록 전도성 공백이 발생하고 팽창흑연의 전도성 네트워킹이 저해되기 때문에 계속 감소한다.