• 제목/요약/키워드: Advanced composite materials

검색결과 1,142건 처리시간 0.031초

유리섬유-폴리프로필렌 복합재료의 압축 공정 중 뒤틀림 예측에 관한 연구 (A Study on the Prediction of Warpage During the Compression Molding of Glass Fiber-polypropylene Composites)

  • 김규형;조동혁;이주원;김상덕;신철민;윤정환
    • 소성∙가공
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    • 제32권6호
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    • pp.367-375
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    • 2023
  • Composite materials, known for their excellent mechanical properties and lightweight characteristics, are applied in various engineering fields. Recently, efforts have been made to develop an automotive battery protection panel using a plain-woven composite composed of glass fiber and polypropylene to reduce the weight of automobiles. However, excessive warpage occurs during the GF/PP compression molding process, which makes car assembly challenging. This study aims to develop a model that predicts the warpage during the compression molding process. Obtaining out-of-plane properties such as elastic or shear modulus, essential for predicting warpages, is tricky. Existing mechanical methods also have limitations in calculating these properties for woven composite materials. To address this issue, finite element analysis is conducted using representative volume elements (RVE) for woven composite materials. A warpage prediction model is developed based on the estimated physical properties of GF/PP composite materials obtained through representative volume elements. This model is expected to be used for reducing warpages in the compression molding process.

FRP 패널로 보강한 강골조의 가이드 시스템에 따른 성능평가 (Performance Evaluation of Steel Frame with FRP Composite Panel according to Guide System)

  • 임정희;권민호;서현수;김진섭
    • 복합신소재구조학회 논문집
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    • 제6권2호
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    • pp.46-51
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    • 2015
  • Since it is impossible to predict earthquakes, they involve more casualties and property damage compared to meteorological disasters such as heavy snow and heat waves, which can be predicted through weather forecasts. This has highlighted the need for seismic design and reinforcement. Recently, the use of composite materials as reinforcement has surged because steel plate reinforcement and section enlargement are likely to result in increased weight and physical damage to structures. This study evaluates the seismic performance of panels created from composite materials, and their guide systems. The specimens were miniature versions of actual steel structures, and displacement loads were applied in the transverse direction. Seismic performance was found to improve when structures were reinforced with seismic panels.

알루미늄탄소나노튜브 복합재의 가공 방법과 탄소나노튜브 함량에 따른 트라이볼로지 특성 (Tribological Characteristics of Carbon Nanotube Aluminum Composites According to Fabrication Method and Content of Carbon Nanotube)

  • 이영제;이중희;김일영;이규선;백승현;윤정일;김영직
    • Tribology and Lubricants
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    • 제24권5호
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    • pp.269-274
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    • 2008
  • Carbon nanotube composite is considered to be a good candidate material for composite material because of its excellent mechanical property and low density under high temperature as well as good wear and frictional properties. In this study, tribological characteristics of carbon nanotube aluminum composite were evaluated using pin-on-disk wear tester. Spark Plasma Sintering method is more effective than Hot Pressing method in terms of wear and friction. The composite with 1% CNT has the lowest friction and wear characteristic.

Rapid Synthesis and Consolidation of Nanostructured Ti-TiC Composites from TiH2 and CNT by Pulsed Current Activated Heating

  • Park, Na-Ra;Shon, In-Jin
    • 한국재료학회지
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    • 제25권1호
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    • pp.48-53
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    • 2015
  • $TiH_2$ nanopowder was made by high energy ball milling. The milled $TiH_2$ and CNT powders were then simultaneously synthesized and consolidated using pulsed current activated sintering (PCAS) within one minute under an applied pressure of 80 MPa. The milling did not induce any reaction between the constituent powders. Meanwhile, PCAS of the $TiH_2$-CNT mixture produced a Ti-TiC composite according to the reaction ($0.92TiH_2+0.08CNT{\rightarrow}0.84Ti+0.08TiC+0.92H_2$, $0.84TiH_2+0.16CNT{\rightarrow}0.68Ti+0.16TiC+0.84H_2$). Highly dense nanocrystalline Ti-TiC composites with a relative density of up to 99.7% were obtained. The hardness and fracture toughness of the dense Ti-8 mole% TiC and Ti-16 mole% TiC produced by PCAS were also investigated. The hardness of the Ti-8 mole% TiC and Ti-16 mole% TiC composites was higher than that of Ti. The hardness value of the Ti-16 mole% TiC composite was higher than that of the Ti-8 mole% TiC composite without a decrease in fracture toughness.

철계 복합 분말로 제조된 오버레이 용접층의 미세조직 및 특성 (Microstructure and Characterization of Overlay Welding Layer using Fe-based Composite Powders)

  • 민홍;이종재;이진규
    • 한국분말재료학회지
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    • 제26권3호
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    • pp.214-219
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    • 2019
  • In this study, the microstructure and characterization of an overlay welding layer using Fe-based composite powders are reported. The effects of the number of passes and composition of powders on the microstructure and mechanical properties are investigated in detail. The welding wire and powders are deposited twice on a stainless-steel rod using a laser overlay welding process. The microstructure and structural characterization are performed by scanning electron microscopy and X-ray diffraction. The mechanical properties of the first and second overlay layers are analyzed through the micro-Vickers-hardness tester and abrasion wear tester. In the second overlay layer, the hardness and specific wear are approximately 840 Hv and $2.0{\times}10^{-5}mm^3/Nm$, respectively. It is suggested that the increase of the volume fractions of $(Cr,Fe)_7C_3$ and NbC phases in the second welding layer enhances the hardness and wear resistance.

나노구조 (W,Ti)C-Graphene 복합재료 급속소결 (Rapid Sintering of Nanocrystalline (W,Ti)C-Graphene Composites)

  • 김성은;손인진
    • 대한금속재료학회지
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    • 제56권12호
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    • pp.854-860
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    • 2018
  • In spite of the many attractive properties of (W,Ti)C, its low fracture toughness limits its wide application. To improve the fracture toughness generally a second phase is added to fabricate a nanostructured composite. In this regard, graphene was considered as the reinforcing agent of (W,Ti)C. (W,Ti)C-graphene composites that were sintered within 2 min using pulsed current activated heating under a pressure of 80 MPa. The rapid consolidation method allowed retention of the nano-scale microstructure by blocking the grain growth. The effect of graphene on the hardness and microstructure of the (W,Ti)C-graphene composite was studied using a Vickers hardness tester and FE-SEM. The grain size of (W,Ti)C was reduced remarkably by the addition of graphene. Furthermore, the hardness decreased and the fracture toughness improved with the addition of graphene.

Nano-sized TiCxNy를 함유한 STS 복합체의 특성 (Characteristics of Stainless Steel Composites with Nano-sized TiCxNy)

  • 반태호;박성범;조수정;이동원;;박용일;김성진
    • 한국분말재료학회지
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    • 제18권3호
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    • pp.290-296
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    • 2011
  • Titanium carbonitride is more perspective materials compared to titanium carbide. It can be used in tool industry and special products because of its higher strength, abrasive wear-resistance and especially its strong chemical stability at high temperatures. We produced STS+TiCxNy composite by the spark plasma sintering for higher strength and studied the characteristics. The planar and cross-sectional microstructures of the specimens were observed by scanning electron microscopy. Characterizations of the carbon and nitride phases on the surface of composite were carried out using an X-ray diffractometer. During annealing TiCxNy particles diffusion into STS 430 was observed. After annealing, sintering isolations between particles were formed. It causes decreasing of mechanical strength. In addition when annealing temperature was increased hardness increased. Heterogeneous distribution of alloying elements particles was observed. After annealing composites, highest value of hardness was 738.1 MHV.

Thermoelastic Behaviors of Fabric Membrane Structures

  • Roh, Jin-Ho;Lee, Han-Geol;Lee, In
    • Advanced Composite Materials
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    • 제17권4호
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    • pp.319-332
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    • 2008
  • The thermoelastic behaviors of an inflatable fabric membrane structure for use in a stratospheric airship envelope are experimentally and numerically investigated. Mechanical tensile properties of the membrane material at room, high, and low temperatures are measured using an $Instron^{(R)}$ universal testing machine and an $Instron^{(R)}$ thermal chamber. To characterize the nonlinear behavior of the inflated membrane structure due to wrinkling, the bending behavior of an inflated cylindrical boom made of a fabric membrane is observed at various pressure levels. Moreover, the envelope of a stratospheric airship is numerically modeled based on the thermoelastic properties of the fabric membrane obtained from experimental data, and the wrinkled deformed shape induced by a thermal load is analyzed.

RE Magnetron Sputtering에 의해 제조된 HAp와 HAp-Ag복합코팅층의 미세조직 (Microstructures of HAp and HAp-Ag Composite Coating Layer Prepared by RS Magnetron Sputtering)

  • Lee, Hee-Jung;Oh, Ik-Hyun;Park, Sang-Shik;Lee, Byong-Taek
    • 한국세라믹학회지
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    • 제41권4호
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    • pp.328-333
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    • 2004
  • RF magnetron sputtering법에 의해 단상의 하이드록시아파타이트와 하이드록시아파타이트은 복합코팅층을 ZrO$_2$와 Si 웨이퍼 기판에 코팅하였다. 이들 코팅층들의 두께 0.7∼1.0$\mu\textrm{m}$ 범위였으며 또한 거칠기(roughness)는 3∼4nm였다. 열처리된 HAp 코팅층은 나노크기의 결정들로 구성되어 있었으며, 반면 Ag가 함유된 복합코팅층의 경우 결정질과 비결정질이 혼재되어 있었다. 열처리 전 HAp 코팅층의 Ca/P비는 1.9였고, Ag의 함량이 증가함에 따라 비는 감소하는 경향을 나타내었다. 또한 Ag 함량이 증가함에 따라 HAp코팅층의 미소 경도는 감소하였다.