• 제목/요약/키워드: composite sheets

검색결과 312건 처리시간 0.024초

가지 달린 구조의 폴리실라잔을 전구체로 이용해 제조한 카본 나노튜브/실리콘 카보나이트라이드 복합체 시트의 발열특성에 관한 연구 (A Study on Heating Element Properties of Carbon Nanotube/Silicon Carbonitride Composite Sheet using Branched Structured Polysilazane as Precursor)

  • 허태환;송현준;정영진;곽영제
    • Composites Research
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    • 제33권6호
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    • pp.395-400
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    • 2020
  • 본 연구에서는 카본나노튜브(CNT) 면상발열체에 preceramic polymer 중 하나인 실세스퀴아잔을 코팅하여 고온에서 안정적인 발열이 가능한 CNT/SiCN 복합체 시트를 제조하였다. 제조된 복합체 필름은 FE-SEM을 통해 실세스퀴아잔이 CNT 면상발열체의 표면을 모두 코팅한 것을 확인하였다. 또한 800℃의 열처리를 통해 실세 스퀴아잔이 SiCN 세라믹으로 전환되어도 표면의 결함이 발견되지 않고 온전한 구조를 유지하는 것을 확인하였다. CNT/SiCN 복합체 시트는 질소와 공기 분위기 모두에서 기존의 CNT 시트보다도 높은 열적 안정성을 확보할 수 있었다. 마지막으로 제조된 CNT/SiCN 복합체 필름은 대기 중에서 700℃ 이상의 온도로 발열이 가능하였고 발열 후 온도를 식히고 재발열 또한 성공적으로 이루어졌다.

Numerical investigation of SHS steel beam-columns strengthened using CFRP composite

  • Keykha, Amir Hamzeh
    • Steel and Composite Structures
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    • 제25권5호
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    • pp.593-601
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    • 2017
  • Carbon Fiber Reinforced Polymer (CFRP) is one of the materials used to strengthen steel structures. Most studies on strengthening steel structures have been done on steel beams and steel columns. No independent study, to the researcher's knowledge, has studied the effect of CFRP strengthening on steel beam-columns, and it seems that there is a lack of understanding on behavior of CFRP strengthening on steel beam-columns. However, this study explored the use of adhesively bonded CFRP flexible sheets on retrofitting square hollow section (SHS) steel beam-columns, using numerical investigations. Finite Element Method (FEM) was employed for modeling. To determine the ultimate load of SHS steel beam-columns, ten specimens, eight of which were strengthened with the different coverage length and with one and two CFRP layers, with two types of section (Type A and B) were analyzed. ANSYS was used to analyze the SHS steel beam-columns. The results showed that the CFRP composite had no similar effect on the slender and stocky SHS steel beam-columns. The results also showed that the coverage length, the number of layers, and the location of CFRP composites were effective in increasing the ultimate load of the SHS steel beam-columns.

항공기 적용 샌드위치 복합재 구조의 충격 손상 거동 연구 (Study on Impact Damage Behavior of Sandwich Composite Structure for aircraft)

  • 박현범;공창덕
    • Composites Research
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    • 제26권1호
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    • pp.36-41
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    • 2013
  • 본 연구에서는 복합재 샌드위치 적층판의 저속 충격 해석을 수행하였다. 샌드위치 구조 형상의 스킨은 탄소/에폭시(Carbon-Epoxy) 재질이 채택되었고 코어(Core)의 재질은 폼(Foam)이 적용되었다. 연구의 타당성을 입증하기 위해 관련 문헌에서의 연구 결과에서 제시한 실험 결과와 유한 요소 해석 결과의 비교가 선행되었다. 타당성 검증을 바탕으로 본 연구에서 손상이 시작되는 충격체의 속도를 평가하고, 예측된 충격 속도에서 충격 거동을 분석하기위해 유한요소법을 이용하여 충격 해석을 수행하였다. 샌드위치 복합재 적층판의 충격 해석 결과 예측된 충격 속도에서 손상이 발생함을 확인하였다. 최종 시편 시험 결과와 수치 해석 결과의 비교 값이 잘 일치함을 확인하였다.

터보팬 엔진 나셀용 샌드위치 복합재 구조물의 손상 거동 연구 (Study on Impact Damage Behavior of Turbo Fan Engine Nacelle Sandwich Composite Structure)

  • 공창덕;박현범;이승현
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.75-78
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    • 2007
  • 본 연구에서는 터보 팬 엔진 나셀 복합재 구조의 충격 손상에 관한 연구를 수행하였다. 연구 결과의 신뢰성 검증을 위해 선행 연구된 결과와 비교 분석하였다. 샌드위치 구조의 형상은 카본/에폭시 면재와 폼 코어로 형성되어있다. 샌드위치 패널의 유한 요소 해석 결과 해석 결과의 타당성을 확인하였다. 초기 손상이 발생하는 속도가 평가되었고 예측된 속도에서 충격 해석이 수행되었다. 충격 해석 결과 예측된 충격 손상에서 손상이 발생하는 것으로 확인되었다.

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Flattening simulations of 3D thick sheets made of fiber composite materials

  • Morioka, Kotaro;Ohtake, Yutaka;Suzuki, Hiromasa;Nagai, Yukie;Hishida, Hiroyuki;Inagaki, Koichi;Nakamura, Takeshi;Watanabe, Fumiaki
    • Journal of Computational Design and Engineering
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    • 제2권2호
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    • pp.88-95
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    • 2015
  • Recently, fiber composite materials have been attracting attention from industry because of their remarkable material characteristics, including light weight and high stiffness. However, the costs of products composed of fiber materials remain high because of the lack of effective manufacturing and designing technologies. To improve the relevant design technology, this paper proposes a novel simulation method for deforming fiber materials. Specifically, given a 3D model with constant thickness and known fiber orientation, the proposed method simulates the deformation of a model made of thick fiber-material. The method separates a 3D sheet model into two surfaces and then flattens these surfaces into two dimensional planes by a parameterization method with involves cross vector fields. The cross vector fields are generated by propagating the given fiber orientations specified at several important points on the 3D model. Integration of the cross vector fields gives parameterization with low-stretch and low-distortion.

방수재료 및 공법의 내구성 평가를 위한 복합열화분석용 3차원 거동대응 시험결과 (A Study on the Analysis of 3 Dimensional Substrate Behaviour of Complex Environmental Deterioration and the Analysis of Results)

  • 송제영;서현재;최은규;이정훈;김병일;오상근
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2018년도 추계 학술논문 발표대회
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    • pp.189-190
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    • 2018
  • KS standards mostly relate to single component material evaluation, so in cases of underground structure environments, most cannot predict the existing composite forms of deterioration, resulting in the applied waterproofing materials becoming unable to respond to these damaging factors. Current domestic waterproofing market in Korea mainly uses single-ply waterproofing materials comprised of coatings or waterproof sheets and two or more-ply composite waterproofing methods. In order to evaluate these types of composite waterproofing systems, a new test equipment and method that incorporates various deterioration conditions (joint displacement, chemical exposure, water pressure etc) was developed. In a comparison testing, the results showed that flexible type materials have higher response performance towards joint displacement than the hardened material.

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Effect of tapered-end shape of FRP sheets on stress concentration in strengthened beams

  • Belakhdar, Khalil;Tounsi, Abdelouahed;Adda Bedia, El Abbes;Redha, Yeghnem
    • Steel and Composite Structures
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    • 제11권6호
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    • pp.435-454
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    • 2011
  • Bonding composite materials to structural members for strengthening purpose has received a considerable attention in recent years. The major problem when using bonded FRP or steel plates to strengthen existing structures is the high interfacial stresses that may be built up near the plate ends which lead to premature failure of the structure. As a result, many researchers have developed several analytical methods to predict the interface performance of bonded repairs. In this paper, a numerical solution using finite - difference method is used to calculate the interfacial stress distribution in beams strengthened with FRP plate having a tapered ends with different thinning profiles. These latter, can significantly reduce the stress concentration. In the present theoretical analysis, the adherend shear deformations are taken into account by assuming a parabolic shear stress through the thickness of both beam and bonded plate. Numerical results from the present analysis are presented to demonstrate the advantages of use the tapers in design of strengthened beams.

탄소분말을 함유한 도전성 고분자 PTCR의 전기적 특성 (Electrical properties of conducting polymer PTCR containing carbon powders)

  • 김경종;이재원;김영혁;김성훈;최문석;이재신
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2006년도 하계학술대회 논문집 Vol.7
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    • pp.220-221
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    • 2006
  • We investigated the electrical properties of polymer-carbon composite materials for temperature sensitive resistor applications. Cu/polymer/Cu sheets were fabricated by laminating low density polyethylene(LDPE) containing carbon powders. Weight ratio of carbon powder to LDPE was varied in a range of 0.9~2. With increasing the carbon concentration, the electrical resistance of the composite material was decreased from 0.75 to $0.08\;{\Omega}cm$. The composite layer showed a abrupt increase in the electrical resistance at $115^{\circ}C$ because of the softening of the polymer.

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Vibration analysis of double-bonded micro sandwich cylindrical shells under multi-physical loadings

  • Yazdani, Raziye;Mohammadimehr, Mehdi;Zenkour, Ashraf M.
    • Steel and Composite Structures
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    • 제33권1호
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    • pp.93-109
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    • 2019
  • In the present study, vibration analysis of double bonded micro sandwich cylindrical shells with saturated porous core and carbon/boron nitride nanotubes (CNT/BNNT) reinforced composite face sheets under multi-physical loadings based on Cooper-Naghdi theory is investigated. The material properties of the micro structure are assumed to be temperature dependent, and each of the micro-tubes is placed on the Pasternak elastic foundations, and mechanical, moisture, thermal, electrical, and magnetic forces are effective on the structural behavior. The distributions of porous materials in three distributions such as non-linear non-symmetric, nonlinear-symmetric, and uniform are considered. The relationship including electro-magneto-hydro-thermo-mechanical loadings based on modified couple stress theory is obtained and moreover the governing equations of motion using the energy method and the Hamilton's principle are derived. Also, Navier's type solution is also used to solve the governing equations of motion. The effects of various parameters such as material length scale parameter, temperature change, various distributions of nanotube, volume fraction of nanotubes, porosity and Skempton coefficients, and geometric parameters on the natural frequency of double bonded micro sandwich cylindrical shells are investigated. Increasing the porosity and the Skempton coefficients of the core in micro sandwich cylindrical shell lead to increase the natural frequency of the structure. Cylindrical shells and porous materials in the industry of filters and separators, heat exchangers and coolers are widely used and are generally accepted today.

Axial buckling response of fiber metal laminate circular cylindrical shells

  • Bidgoli, Ali M. Moniri;Heidari-Rarani, Mohammad
    • Structural Engineering and Mechanics
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    • 제57권1호
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    • pp.45-63
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    • 2016
  • Fiber metal laminates (FMLs) represent a high-performance family of hybrid materials which consist of thin metal sheets bonded together with alternating unidirectional fiber layers. In this study, the buckling behavior of a FML circular cylindrical shell under axial compression is investigated via both analytical and finite element approaches. The governing equations are derived based on the first-order shear deformation theory and solved by the Navier solution method. Also, the buckling load of a FML cylindrical shell is calculated using linear eigenvalue analysis in commercial finite element software, ABAQUS. Due to lack of experimental and analytical data for buckling behavior of FML cylindrical shells in the literature, the proposed model is simplified to the full-composite and full-metal cylindrical shells and buckling loads are compared with the available results. Afterwards, the effects of FML parameters such as metal volume fraction (MVF), composite fiber orientation, stacking sequence of layers and geometric parameters are studied on the buckling loads. Results show that the FML layup has the significant effect on the buckling loads of FML cylindrical shells in comparison to the full-composite and full-metal shells. Results of this paper hopefully provide a useful guideline for engineers to design an efficient and economical structure.