• Title/Summary/Keyword: 카본-카본 복합재료

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Cross-link Density Measurement and Thermal Oxidative Degradation Analysis of a Carbon Black Compounded EPDM Rubber Hose (카본블랙을 충전한 EPDM 고무호스의 가교밀도 측정과 열가속 및 산소 노화거동)

  • Kwak, Seung-Bum;Choi, Nak-Sam;Kim, Jin-Kuk
    • Composites Research
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    • v.22 no.3
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    • pp.35-43
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    • 2009
  • In this study, for a radiator hose made of carbon black filled EPDM(ethylene-propylene diene monomer) rubber, a measuring method of crosslink density was established to analyze the aging behaviors under thermo-oxidative stresses. At $125^{\circ}C$, the crosslink density of the rubber specimens decreased slightly in the initial stage, but increased with increasing the aging time. Such variation in crosslink density was similar to that of tensile strength. This might be due to the formation of sulphoxide crosslinks as well as to additional crosslinks made by the reaction of unvalcunized sulfurs. A high temperature aging of rubber specimens at $180^{\circ}C$ caused a slight increase in crosslink density while it did a large decrease in tensile strength and elongation. With aging at high temperature, the formation of carbonyl groups in EPDM molecule chain and formation of sulphoxide crosslink, rather than the crosslink density variation itself, had a large influence on such changes in mechanical property.

Gas Permeable Properties of Elastomer-Clay Nanocomposite Membrane (유기탄성체-Clay 나노복합재료 막의 기체투과 특성)

  • Nam Sang-Yong;Park Ji-Soon;Rhim Ji-Won;Chung Youn-Suk;Lee Young-Moo
    • Membrane Journal
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    • v.16 no.2
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    • pp.144-152
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    • 2006
  • Elastomer-clay nanocomposite membranes were prepared by melt intercalation mothod with internal mixer. We are used NMR, Ionomer, SEBS (Styrene Ethylene Butadien styrene Copolymer) as elastomer, and modified clay. Gas barrier property of the elastomer-clay nanocomposites membranes were investigated by a gas permeability of $CO_2,\;O_2,\;N_2$ at room temperature. Gas permeability through the elastomer-clay nanocomposite membranes increased due to increased tortuosity made by intercalation of clay in elastomer.

Study on the Preparation of the Phosphoric Flame retardent for the EMC (EMC용 반응형 인계 난연 수지 개발)

  • Ahn, Tae-Kwang;Kim, Han-Byung;Ryu, Kum-Sook
    • Proceedings of the KAIS Fall Conference
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    • 2009.05a
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    • pp.372-375
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    • 2009
  • 반도체 봉지재란 실리콘 칩, 골드와이어, 리드프레임 등의 반도체 소지를 열, 수분, 충격으로부터 보호하기 위해 밀봉하는 재료로서 EMC(Epoxy Moding Compound)가 가장 많이 쓰인다. EMC는 기계적, 전기적 성능향상을 위한 무기재료로 실리카(Silica), 열에 의해 경화되어 3차원 경화구조를 형성하는 에폭시수지, 빠른 경화특성을 부여하기 위한 경화제로서의 페놀수지, 유기재료와 무기재료 사이의 결합력을 높이기 위해 커플링제, 카본블랙, 이형성 확보를 위한 왁스(Wax), 착색제(Colorant), 난연제(Flame Retardant)등의 첨가제로 구성되는 복합소재로써 본 연구에서는 에폭시의 유형에 따른 용융 실리카를 주충진재로 하여 각각의 봉지재의 첨가제를 기준으로 할 때 다양한 형태의 친환경 비할로겐계 반응형 난연제를 합성하는 기술을 개발하고 비 할로겐계 및 Sb 계 첨가형 난연제의 혼용 배합을 통해 친환경 EMC용 난연제의 제조기술을 개발하였다. 이들 EMC의 요구특성은 요구특성은 외부환경으로부터 칩 보호, 칩을 전기적으로 절연특성 유지, 칩의 작동시 발생되는 열의 효과적인 방출 특성 유지, 실장(Board Mounting)의 간편성 특성을 확보해야 하는 특성을 지니고 있어 이들 요구특성에 적합한 특성조사가 함께 이루어졌다.

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The Behavior of Crack Growth Rate for APAL and CPAL Patched with FRP Laminate in Aluminum Alloy Plate (알루미늄 합금판재에 FRP 라미네이터를 보강한 APAL 및 CPAL 재의 균열전파속도 거동)

  • 윤한기;정해용;허정원
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.19 no.4
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    • pp.1013-1022
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    • 1995
  • A hybrid composite (APAL;Aramid Patched ALuminum alloy, CPAL;Carbon Patched ALluminum alloy), consisting of a Al 2024-T3 aluminum alloy plate sandwiched between two aramid/epoxy and carbon/epoxy laminate, was developed. Fatigue crack growth behavior was examined at stress ratios of R=0.2, 0.5. The APAL and CPAL showed superior fatigue crack growth resistance, which may be attributed to the crack bridging effect imposed by the intact fibers in the crack wake.

Research Trend in Solid Lubricant Layered Materials for the High Performance Li-ion Batteries (층상구조 재료의 고체윤활작용을 이용한 고성능 리튬이온 전지 응용 연구동향)

  • Hur, Jaehyun
    • Prospectives of Industrial Chemistry
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    • v.23 no.5
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    • pp.12-20
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    • 2020
  • 최근 층상구조를 가진 전이금속 칼코겐 화합물이 새로운 고성능 리튬이온전지 음극소재로서 주목받고 있다. 층상구조 물질들의 고성능 전극 소재 활용에 있어 박리를 이용한 정확한 층의 개수 조절은 전기화학 반응성을 증가시키고, 전극 필름 내에서의 균일한 거동을 위해서 매우 중요하다. 볼 밀링 공정은 이차전지 전극 소재 제조에 있어서 주로 물질의 분쇄나 고상 화학반응을 유도하여 합금 형태의 전극 소재 개발에 보편적으로 사용되는 공정이나, 층상구조를 가진 전이금속 칼코겐 화합물에 적용하면 층상구조 물질에 고체윤활작용을 일으켜 박리가 촉진된다. 이러한 성질을 이용하여 다양한 종류의 전이금속 칼코겐 화합물(예: MoS2, MoSe2, NbSe2)에 적절한 카본 매트릭스 물질과 복합화를 통해 새로운 전극 소재를 합성하고, 이를 통해 고성능 리튬이온전지 음극 소재를 제조하는 연구 동향에 대해 보고하고자 한다.

Structural behavior on the steel beam with strengthening bonded carbon plate (카본판을 접착보강한 강재의 거동분석)

  • Sung, Ikhyun
    • Journal of the Society of Disaster Information
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    • v.12 no.1
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    • pp.54-61
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    • 2016
  • The use of advanced composite materials in strengthening and repair of existing structures is increasing rapidly. This paper describes an effectiveness of a bonding of carbon fiber reinforced sheets to corroded steel members for the repair. Three types of surface treatment, what we call cleaning, of corroded plate are chosen as parameters. They are "without cleaning","removal of painting by brushing" and "complete removal of painting". From the experimental study, the following findings are obtained. 1) When the steel plate is subjected to tensile force, carbon fiber sheets adhered to the painted steel gives a higher strength against peeling compared to that of the plate without painting, 2) The grade of surface treatment, or cleaning of the corroded steel plate affects the strengthening effect.

Size effect on tensile strength of filament wound CFRP composites (필라멘트 와인딩 탄소섬유 복합재의 인장강도 크기 효과)

  • Hwang, T.K.;Doh, Y.D.;Kim, H.G.
    • Composites Research
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    • v.24 no.5
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    • pp.1-8
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    • 2011
  • This paper presents the results of theoretical analysis and experimental test to show the size effect on the fiber strength of filament would pressure vessel. First, a series of fully scaled hoop ring tests with filament would carbon-epoxy were conducted, which exhibited a remarkable size effect on the fiber strength. Next, the failure analyses using WWLM(Weibull Weakest Link Model) and the SMFM(Sequential Multi-step Failure Model) were performed and compared to the hoop ring test data, as well as to unidirectional specimens test data from the literature. It was found that the analysis results significantly underestimated the fiber strengths compared to the test data. In this study, a modified SMFM was proposed through the modification of the length size effect. The fiber strengths from modified SMFM analysis showed good agreement with the test data.

The Impact fracture Behaviors of Low Density LD Carbon/Carbon Composites by Drop Weight Impact Test (낙하 충격 시험에 의한 저밀도 2-D탄소/탄소 복합재의 충격파괴거동)

  • 주혁종;손종석
    • Polymer(Korea)
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    • v.26 no.2
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    • pp.270-278
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    • 2002
  • In this study, the fracture behavior by low velocity impact damage and the tendencies of impact energy absorption were investigated. Low velocity impact tests were performed using a mini tower drop weight impact tester, and graphite powder, carbon black and milled carton fiber were chosen as additives. Addition of graphite powder increased the maximum load and maintained the stress long until the total penetration happened. At the content of 9 vol%, they showed the maximum of 42% improvement in impact strength compared composites containing no additives. At the test with low impact energy of 0.4 J, impact energy was consumed by delamination in the composite containing no additives, however, as graphite contents increased, the tendency of failure changed to the penetration of the specimen.

A Study on Residual Strength of Carbon/Epoxy Face Sheet and Honeycomb Core Sandwich Composite Structure after Quasi Static Indentation Damage (탄소섬유/에폭시 면재, 알루미늄 허니컴 코어 샌드위치 복합재 구조의 압입 손상에 의한 잔류강도 연구)

  • Kong, Chang-Duk;Park, Hyun-Bum;Lee, Seoung-Hyun
    • Composites Research
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    • v.22 no.2
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    • pp.24-29
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    • 2009
  • This study aims to investigate the residual strength of sandwich composites with Al honeycomb core and carbon fiber face sheets after the quasi-static indentation damage by the experimental investigation. The 3-point bending test and the edge-wise compressive strength test were used to find the mechanical properties, and the quasi-static point load was applied to introduce the simulated damage on the specimen. The damaged specimens were finally assessed by the 3-point bending test and the compressive strength test. The investigation results revealed the residual strength of the damaged specimens due to the quasi-static indentation. The both test results showed that the residual strength of the damaged specimen was decreased according to increases of the damaged depth.

Design of an Aircraft Composite Window frame Using VaRTM Process (수지 충전 공정을 이용한 항공기 윈도우 프레임 설계)

  • Kim, Wie-Dae;Hong, Dae-Jin
    • Composites Research
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    • v.19 no.6
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    • pp.1-7
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    • 2006
  • This is the preliminary study to develop composite window frame of commercial aircraft using VaRTM process. For two candidate carbon fabrics(triaxial overbraid, sleeving braider), specimens were fabricated using VaRTM process, and the physical & mechanical property tests were performed to obtain the material properties according to ASTM. FEM analysis for each candidate carbon fabric was performed to find the minimum number of plies and weight for composite window frame to satisfy the design requirements. In this study, Tsai-Wu strength failure criterion was used to evaluate the safety of structure.