• Title/Summary/Keyword: 에폭시 섬유

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Fiber Surfaces and Interlaminar Shear Strengths of Electrolytic Ni-plated Carbon Fiber/Epoxy Resin Composites (전해 니켈도금 처리에 따른 탄소섬유/에폭시 수지 복합재료의 섬유표면 및 기계적 계면전단 강도)

  • 박수진;장유신;이재락;김진석
    • Polymer(Korea)
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    • v.24 no.5
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    • pp.721-727
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    • 2000
  • The electrolytic plating of a metallic nickel on carbon fiber surfaces was carried out to improve mechanical interfacial properties of carbon fiber/epoxy resin composites. The surface characteristics of carbon fibers and the mechanical interfacial properties of final composites were characterized by X-ray photoelectron spectroscopy (XPS) and interlaminar shear strength (ILSS), respectively. It was found that the electrolytic Ni-plating conditions significantly affected the degree of adhesion at interfaces between carbon fibers and epoxy resin matrix in a composite system. Especially, the increase of O,$_{1s}$/$C_{1s}$ ratio, production of NiO groups, and formation of metallic nickel on the nickel-plated carbon fiber surfaces led to an increase of the ILSS of the composites. Also, the ILSS of the composites was greatly correlated with the $O_{1s}$/$C_{1s}$ ratio of the carbon fibers treated in this work.is work.

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Structural Behavior Evaluation of Mg-GFRP Composite Single-Lap Bonded Joints With Different End Shapes (한 끝단 형상에 따른 마그네슘 합금과 유리섬유 복합소재 단일겹치기 본드 조인트 거동 분석)

  • Kim, Jung-Seok;Im, Jae-Young;Lee, Woo-Geun
    • Journal of the Korean Society for Railway
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    • v.17 no.6
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    • pp.391-396
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    • 2014
  • In this study, the strength of magnesium-GFRP/epoxy single-lap bonded joints are experimentally evaluated with different end shapes. In order to achieve this, four different single-lap joints with different end shapes are fabricated and the failure load is measured under tensile loading tests. From the test results, the single-lap joint with a square end exhibits the lowest failure load while the single-lap joint with reverse tapering and a spew fillet has the highest stress values. It has 11.1% higher failure strength than the single-lap joint with a square end.

Flexural Behavior of Hybrid Fiber Reinforcement Strengthened RC Beams (하이브리드 섬유보강재로 보강된 철근콘크리트 보의 휨거동)

  • Yi, Seong-Tae;Lee, Chin-Yong
    • Journal of the Korea institute for structural maintenance and inspection
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    • v.14 no.5
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    • pp.79-86
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    • 2010
  • This study was performed to evaluate the flexural behavior of Hybrid fiber sheet (HFC) and Hybrid fiber bar (HFB) strengthened reinforced concrete (RC) beams. According to test results, Hybrid fiber reinforcement strengthened RC beams showed approximately 60 to 200% higher reinforcing effects than that of un-reinforced specimens. In addition, the reinforced beams showed the ideal failure pattern, which is failed presenting the ductile behavior after yielding of the reinforcing bar. More specifically, in the case of HFB reinforced RC beams, the difference with puttying method was not apparent since HFB beams reinforced using the injection of epoxy and bonding of putty showed the similar failure patterns.

Optimization of the Coupling and the Reflector Material in the DOI PET Detector Module using the WLS Fiber (파장변이섬유를 사용하는 반응 위치 측정 양전자방출 단층촬영기기 검출기 모듈의 연결물질과 반사체 물질의 최적화)

  • Lee, Seung-Jae
    • Journal of the Korean Society of Radiology
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    • v.13 no.1
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    • pp.15-20
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    • 2019
  • We developed a novel depth-of-interaction positron emission tomography (PET) detector using wavelength shifting (WLS) fibers and optimized it. The optimization module was designed by using two scintillators and three WLS fibers and attaching a sensor to the end of the WLS fiber. Optimum combinations were obtained through the light collection efficiency and the light collection ratio between sensors depending on coupling materials and reflectors of scintillators, WLS fibers and sensors. The highest light collection efficiency and the light collection ratio between sensors were obtained in the combination of the epoxy (coupling materials)-diffuse reflector (scintillators)-specular reflector (WLS fibers).

Effect of Surface-Modified Carbon Fiber on the Mechanical Properties of Carbon/Epoxy Composite for Bipolar Plate of PEMFC (표면처리 탄소섬유가 PEMFC용 탄소/에폭시 복합재료 분리판의 기계적 강도에 미치는 영향)

  • LEE, HONGKI;HAN, KYEONGSIK
    • Transactions of the Korean hydrogen and new energy society
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    • v.31 no.1
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    • pp.49-56
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    • 2020
  • Epoxy/carbon composite was used to prepare a bipolar plate for polymer electrolyte membrane fuel cell (PEMFC). Phenol novolac-type epoxy and diglycidyl ether of bisphenol A (DGEBA)-type epoxy mixture was used as a matrix and graphite powder, carbon fiber (CF) and graphite fiber (GF) were used as carbon materials. In order to improve the mechanical properties of the bipolar plate, surface-modified CF was incorporated into the epoxy/carbon composite. To determine the cure temperature of the epoxy mixture, differential scanning calorimetry (DSC) analysis was performed and the data were introduced to Kissinger equation in order to get reaction activation energy and pre-exponential factor. Tensile and flexural strength was obtained by using universal testing machine (UTM). The surface morphology of the fractured specimen and the interfacial morphology between epoxy matrix and CF or GF were observed by a scanning electron microscopy (SEM).

Design of High Speed Composite Air Spindle System (초고속 복합재료 공기정압 주축의 설계)

  • 장승환;이대길;한흥삼
    • Composites Research
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    • v.14 no.1
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    • pp.47-56
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    • 2001
  • In order to enhance high speed stability the composite air spindle system composed of a high modulus carbon fiber composite shaft, powder contained epoxy composite squirrel cage rotor and aluminum tool holder was designed and manufactured. For the optimal design of the composite air spindle system, the stacking sequence and thickness of the composite shaft were selected by considering the fundamental natural frequency and deformation of the system. The analysis gave results that the composite air spindle system had 36% higher natural frequency relative to a conventional air spindle system. The dynamic characteristics of the composite spindle system were compared with those of a conventional steel air spindle system. From the calculated and test results, it was concluded that the composite shaft and the power contained composite rotor were able to enhance the dynamic characteristics of the spindle system effectively due to the low inertia and high speific stiffness of the composite materials.

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Cut-off Grinding Characteristics of the Carbon Fiber Epoxy Composite Materials (탄소 섬유 에폭시 복합재료의 절단 연삭 특성)

  • Kim, Po-Jin;Choe, Jin-Gyeong;Lee, Dae-Gil
    • Transactions of the Korean Society of Mechanical Engineers A
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    • v.24 no.2 s.173
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    • pp.338-346
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    • 2000
  • Although the net-shape molding of composites is generally recommended, molded composites are frequently required cutting or grinding due to the dimensional inaccuracy for precision machine elements . During the composite machining operations such as cutting and grinding, the temperature at the cutting point may increase beyond the allowed limit due to the low thermal conductivity of composites, which might degrade the matrix of composite. Therefore, in this work, the temperature at the cutting point during cut-off grinding of carbon fiber epoxy composites was measured. The cutting force and surface roughness were also measured to investigate the cut-off grinding characteristics of the composites. The experiments were performed both under dry and wet grinding conditions with respect to cutting speed and feed rate. From the experimental investigation, the optimal conditions for the composite cut-off grinding were suggested.

A Study on the Impact Fracture Behavior of Carbon Fiber Reinforced Plastics (CFRP 복합재료의 충격파괴거동에 관한 연구)

  • 고성위;김학돌;엄윤성;최영근;김형진;김재동;김엄기
    • Journal of the Korean Society of Fisheries and Ocean Technology
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    • v.38 no.4
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    • pp.300-306
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    • 2002
  • In this paper the failure mechanisms and Charpy impact tests of carbon fiber polypropylene composites have been studied in the temperature range -5$0^{\circ}C$ to 6$0^{\circ}C$ and 3 different supported length of specimen (span length). There are significant effects of temperature and span length on impact fracture toughness, which shows a peak at ambient temperature and decrease as temperature is reduced. Fracture toughness shows a maximum at span length s=20mm. Failure mechanisms are characterized based on SEM examination, which is correlated the measured fracture toughness. Mafor mechansms of this composites can be classified as fiber matrix debonding, delamination, fiber pull-out and matrix deformation.

Impact Behaviors of Ni-plated Carbon Fibers-reinforced Epoxy Matrix Composites (니켈도금된 탄소섬유 강화 에폭시 수지 복합재료의 충격 특성)

  • 박수진;김병주;이종문
    • Polymer(Korea)
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    • v.27 no.1
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    • pp.52-60
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    • 2003
  • In this work, two types of Ni-plating, namely electrolytical and electroless Ni-platings on carbon fiber surfaces, were carried out to enhance the impact resistance of composites. And the comparison between electrolytical and electroless methods on their impact properties of composite system was studied. The surface properties of carbon fibers were characterized using XRD, SEM, and contact angle measurements. The impact behaviors were investigated using an Izod type impact tester. As experimental results, it was observed that electrolessly plated Ni layers had Ni-P alloys on carbon fiber surfaces as revealed by XRD, and electrolytically Ni-plated carbon fibers showed higher surface free energies than those of the electrolessly Ni-plated carbon fibers. In particular, the impact strengths of electrolessly Ni-plated carbon fibers-reinforced plastics were strongly increased. These results were probably due to the difference of wettabilities according to the different types of Ni-plating methods.

Evaluation of Adhesion Property of Epoxy Adhesive with Different Surface Roughness of GFRC (유리섬유강화 복합재료의 표면거칠기에 따른 에폭시 접착제의 접착강도 평가)

  • Kim, Jong-Hyun;Shin, Pyeong-Su;Lee, Sang-Il;Park, Joung-Man
    • Journal of Adhesion and Interface
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    • v.21 no.1
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    • pp.27-33
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    • 2020
  • Adhesion property of epoxy adhesive was evaluated with different surface roughness of glass fiber reinforced composite (GFRC) and optimized condition of surface roughness was confirmed. Different sizes of alumina (Al2O3) particles were blasted to GFRC to control surface roughness of GFRC using sand blasting method. The surface roughness was measured and quantified via surface roughness tester. Contact angle was measured using four types of different solvents. Surface energies and work of adhesion between epoxy adhesive and GFRCs were calculated with different surface roughness of GFRC. Adhesion property between epoxy adhesive and GFRCs was evaluated using single lap shear test and adhesion property increased with surface roughness of GFRC. The fracture surface of GFRCs was observed to evaluate adhesion property. Finally, the optimized roughness condition of GFRCs was confirmed.