• 제목/요약/키워드: Carbon-aramid

검색결과 61건 처리시간 0.022초

온도 및 수분이 탄소/아라미드 섬유 복합재의 파손거동에 미치는 영향 (The Effects of Temperature and Water Absorption on Failure Behaviors of Carbon / Aramid Fiber Composites)

  • 권우덕;권오헌;박우림
    • 한국안전학회지
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    • 제37권4호
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    • pp.11-19
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    • 2022
  • This paper presents the effects of high temperature and water absorption on the mechanical behaviors of carbon-aramid fiber composites, specifically their strength, elastic modulus, and fracture. These composites are used in industrial structures because of their high specific strength and toughness. Carbon fiber composites are vulnerable to the impact force of external objects despite their excellent properties. Aramid fibers have high elongation and impact absorption capabilities. Accordingly, a hybrid composite with the complementary properties and capabilities of carbon and aramid fibers is fabricated. However, the exposure of aramid fiber to water or heat typically deteriorates its mechanical properties. In view of this, tensile and flexural tests were conducted on a twill woven carbon-aramid fiber hybrid composite to investigate the effects of high temperature and water absorption. Moreover, a multiscale analysis of the stress behavior of the composite's microstructure was implemented. The results show that the elastic modulus of composites subjected to high temperature and water absorption treatments decreased by approximately 22% and 34%, respectively, compared with that of the composite under normal conditions. The crack behavior of the composites was well identified under the specimen conditions.

A Novel Manufacturing Method for Carbon Nanotube/Aramid Fiber Filled Hybrid Multi-component Composites

  • Song, Young-Seok;Oh, Hwa-Jin;Jeong, Tai-Kyeong T.;Youn, Jae-Ryoun
    • Advanced Composite Materials
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    • 제17권4호
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    • pp.333-341
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    • 2008
  • A novel manufacturing method for hybrid composites filled with carbon nanotubes (CNTs) and aramid fibers is proposed. To disperse the CNTs in the epoxy matrix with the presence of aramid fibers, CNT/polyethyleneoxide (PEO) composites are prepared and utilized because PEO is miscible in the epoxy resin. After thin films are made of the CNT/PEO composite and placed together with the aramid fibers, the epoxy resin is infused to them. The PEO is dissolved in the epoxy and then the CNTs are dispersed in the PEO/epoxy matrix between aramid fibers before the pre-heated matrix is cured. It is found that the PEO is completely miscible with the epoxy resin and CNTs are dispersed well in the space between the aramid fibers.

Mode-I fracture toughness of carbon fiber/epoxy composites interleaved by aramid nonwoven veils

  • Beylergil, Bertan;Tanoglu, Metin;Aktas, Engin
    • Steel and Composite Structures
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    • 제31권2호
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    • pp.113-123
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    • 2019
  • In this study, carbon fiber/epoxy (CF/EP) composites were interleaved with aramid nonwoven veils with an areal weight density of $8.5g/m^2$ to improve their Mode-I fracture toughness. The control and aramid interleaved CF/EP composite laminates were manufactured by VARTM in a [0]4 configuration. Tensile, three-point bending, compression, interlaminar shear, Charpy impact and Mode-I (DCB) fracture toughness values were determined to evaluate the effects of aramid nonwoven fabrics on the mechanical performance of the CF/EP composites. Thermomechanical behavior of the specimens was investigated by Dynamic Mechanical Analysis (DMA). The results showed that the propagation Mode-I fracture toughness values of CF/EP composites can be significantly improved (by about 72%) using aramid nonwoven fabrics. It was found that the main extrinsic toughening mechanism is aramid microfiber bridging acting behind the crack-tip. The incorporation of these nonwovens also increased interlaminar shear and Charpy impact strength by 10 and 16.5%, respectively. Moreover, it was revealed that the damping ability of the composites increased with the incorporation of aramid nonwoven fabrics in the interlaminar region of composites. On the other hand, they caused a reduction in in-plane mechanical properties due to the reduced carbon fiber volume fraction, increased thickness and void formation in the composites.

해수 열화 및 원공 손상 CF/Aramid 복합재의 패치 부착이 굽힘거동에 미치는 영향 (The Patch Attachment Effect for Bending Behavior on the CF/Aramid Composites with Seawater Aging and Hole Damage)

  • 권우덕;권오헌;윤유성
    • 한국안전학회지
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    • 제38권3호
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    • pp.20-26
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    • 2023
  • Fiber-reinforced composite materials with carbon, glass, and aramid fibers are widely applied to industrial field structures due to their excellent properties. However, carbon fibers are vulnerable to external impacts, whereas aramid fibers degrade when exposed to water. This study evaluated carbon/aramid fiber composites degraded and damaged by high-temperature saline environments using acoustic emission (AE). The test specimen was molded using an autoclave and immersed in seawater at 70 ℃ for 224 days. In order to imitate the damage, a 3-mm-diameter hole was drilled using a diamond drill. Additionally, the specimen with the perforation was repaired by patch attachment processing. Three-point bending was used to conduct the flexural experiment, and an AE sensor with a 150-kHz resonance frequency was attached to evaluate the damage and the effect of patch attachment. AE accumulative counts obtained at the maximum load were 69.2, 67.1, and 91.2 for a high-temperature seawater deteriorated condition, a hole specimen, and a repaired patch specimen, respectively. Furthermore, the maximum amplitude of AE was detected at low values of 28 dB, 31.3 dB, and 30.3 dB.

하이브리드 능직 탄소-아라미드 섬유 복합재의 모드 I 파괴인성에 대한 실험적 연구 (Experimental Investigations of Mode I Fracture Toughness of a Hybrid Twill Woven Carbon and Aramid Fabric Composite)

  • 권우덕;권오헌
    • 한국안전학회지
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    • 제34권6호
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    • pp.1-6
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    • 2019
  • Carbon fiber has excellent specific strength, corrosion resistance and heat resistance. And p-Aramid fiber has high toughness and heat resistance and high elasticity, and is used in various fields such as industrial protective materials, bulletproof helmets and vests, as well as industrial fields. However, carbon fiber is relatively expensive, and is susceptible to brittle fracture behavior due to its low fracture strain. On the other hand, the aramid fiber tends to decrease in elastic modulus and strength when applied to the epoxy matrix, but it is inexpensive and has higher elongation and fracture toughness than carbon fiber. Thus the twill hybrid carbonaramid fiber reinforced composite laminate composite was investigated for a delamination fracture toughness under Mode I loading by 2 kinds of MBT and MCC deduction. The specimen was fabricated with 20 hybrid fabric plies. The initial crack was made by inserting the teflon tape in the center plane with a0/W=0.5 length. The results show that SERR(Strain Energy Release Rate) as the critical and stable delamination fracture toughness were 0.09 kJ/㎡, 0.386 kJ/㎡ by MBT deduction, and 0.192 kJ/㎡, 0.67 kJ/㎡ by MCC deduction, respectively.

탄소 및 아라미드섬유를 이용한 철근콘크리트 깊은 보의 전단보강에 관한 실험적 연구 (An Experimental Study on Shear Strengthening of the R/C Deep Beams Using Carbon and Aramid Fibers)

  • 조병완;김영진
    • 한국해양공학회지
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    • 제13권3B호
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    • pp.56-64
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    • 1999
  • An experimental study was carried out to examine the structural behavior of reinforced concrete deep beams strengthened with aramid fiber sheets, carbon fiber sheets and plates, and to propose the reasonable strengthening method for the deteriorated R.C. deep beams. Results show that the most significant differences in behavior of reinforced concrete deep beams strengthened with fiber sheet and plate were mainly due to various fiber orientations and anchorage. Deep beams diagonally strengthened with carbon fibers show better performance compared with those of vertically, horizontally strengthened specimens and produce the increase in the shear resistance through the redistribution of internal forces after the initial cracks occur. However, strengthened deep beams without anchorages might show unreasonable, brittle peeling-off failure of fiber reinforcements.

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복합재료의 고체 로켓 모터 케이스 적용 리뷰 (Review of the Composite Materials Application to the Solid Rocket Motor Cases)

  • 이태호
    • Composites Research
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    • 제25권3호
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    • pp.82-89
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    • 2012
  • 본 논문은 고체 추진기관 로켓 모터 케이스에 사용된 복합재료에 대하여 사례와 발전 추세를 조사하였다. 기본적으로 모터케이스는 강인하고 고압에 견뎌야 하며, 가벼워야 한다. 이에 부응하는 소재로 복합재료가 효율적인 재료로서 대두되어 유리섬유, 아라미드 그리고 탄소 섬유가 순차적으로 적용되었다. 모터 케이스 효율을 탄소섬유, 아라미드, D6AC강 등을 비교한 결과 탄소섬유가 가장 우수하고 고강도 탄소섬유를 사용하면 탑재용량이 20% 이상 증가시킬 수 있는 것으로 조사되었다.

탄소섬유/아라미드섬유 하이브리드 복합재료의 적층 순서의 영향 평가 (Influence of Stacking Sequence on Carbon Fiber/Aramid Fiber Hybrid Composite)

  • 이현호;배서연;이성비;이명규;나원진
    • Composites Research
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    • 제36권6호
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    • pp.383-387
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    • 2023
  • 탄소섬유 복합재료는 우수한 물성을 바탕으로 산업 전반에 활용되고 있으나 취성이 강하다는 단점이 있다. 연신율이 높은 소재와의 하이브리드화를 통해 강도는 다소 감소되더라도 파괴인성을 향상시킬 수 있다. 이 연구에서는 탄소섬유와 아라미드섬유를 하이브리드한 적층 판재의 물성을 평가하되, 적층 순서를 다르게 하여 이종 재료와의 계면 형성 정도를 조절하였다. 그 결과 25%의 아라미드 섬유 포함 시 순수 탄소섬유 대비 최대 63%의 Izod 충격강도의 향상을 확인할 수 있었으며, 중간 정도의 복잡도를 가진 적층순서 [CF/CAF2/CF]s 에서 가장 우수하였다. 그러나 전체적인 복합화 효과는 부정적인 것으로 분석되었다.

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

  • 윤한기;정해용;허정원
    • 대한기계학회논문집
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    • 제19권4호
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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.

고온에서 비석면 마찰재의 마찰$cdot$마모특성 (Frictional and Wear Characteristics of Non-Asbestos Materials at Elevated Temperature)

  • 안병길;최웅수;권오관
    • Tribology and Lubricants
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    • 제7권2호
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    • pp.61-66
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    • 1991
  • The frictional and wear characteristics of non-asbestos friction materials made of four different fibers (carbon, aramid, ceramic and glass) have been investigated at elevated temperature using High Frequency Friction Tester. On the basis of the experimental results, friction and wear phenomena of four different non-asbestos fibers were caused by lattice layer film of carbon, polymeric transfer film of aramid, abrasion of ceramic and adhesion of glass fiber under each contact junction. The surface analysis of the worn specimens and counter parts after tests were observed using Scanning Electron Microscope and Optical Microscope.