• 제목/요약/키워드: Multilayer composite

검색결과 78건 처리시간 0.026초

단층/다층 LB 분자막의 내마멸 성능 평가 (Evaluation of Antiwear Performance of Mono/multilayer LB Molecular Films)

  • 안효석;김두인
    • Tribology and Lubricants
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    • 제19권6호
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    • pp.329-334
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    • 2003
  • The antiwear properties of amphiphilic monolayers and composite multilayer on silicon surface were investigated using micro­tribometer and Auger Electron Spectroscopy. Langmuir­Blodgett (LB) monolayers from behenic acid, 2,4­heneicosanedione(HD) and its lopper complex((HD)$_2$Cu) were fabricated on silicon surface and the composite multilayer of 5­bilayer of (HD)$_2$Cu was fabricated on the surface of octadecyltrichlorosilane (OTS) self­assembled monolayer (SAM). We observed that LB monolayers and the composite multilayer exhibited a steady and excellent friction response when compared with the OTS SAM. These LB mono and multilayer also showed much higher wear­resistance than the OTS SAM.

단층/다층 LB 분자막의 트라이볼로지 특성 (Tribological properties of mono/multilayer LB molecular films)

  • 안효석;김두인
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 2003년도 춘계학술대회 논문집
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    • pp.211-214
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    • 2003
  • The tribological properties of amphiphilic monolayers and composite multilayer on silicon surface were investigated using micro-tribometer and Auger Electron Spectroscopy. Langmuir-Blodgett (LB) monolayers from behenic acid. 2.4-heneicosanedione(HD) and its copper complex((HD)$_2$Cu) were fabricated on silicon surface and the composite multilayer of 5-bilayer of (HD)$_2$Cu was fabricated on the surface of octadecyltrichlorsilane (OTS) self-assembled monolayer(SAM). We observed that LB monolayers and the composite multilayer exhibited a steady and excellent friction response when compared with the OTS SAM. These LB mono and multilayer also showed much higher wear-resistance than the OTS SAM.

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Design of Composite Multilayer Surface Antenna Structure and Its Bending Fatigue Characteristics

  • Moon, Tae-Chul;Hwang, Woon-Bong
    • Advanced Composite Materials
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    • 제17권3호
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    • pp.215-224
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    • 2008
  • The present study aims to design a multilayer microstrip antenna with composite sandwich construction and investigate fatigue behavior of this multilayer SAS (surface antenna structure) that was asymmetric sandwich structure for the next generation of structural surface technology. This term, SAS, indicates that the structural surface becomes an antenna. Constituent materials were selected considering electrical properties, dielectric constant and tangent loss as well as mechanical properties. For the antenna performance, antenna elements inserted into structural layers were designed for satellite communication at a resonant frequency of 12.2 GHz. From electrical measurements, it was shown that antenna performances were in good agreement with design requirements. In cyclic 4-point bending, flexure behavior was investigated by static and fatigue test. Fatigue life curve of the SAS was obtained. The experimental results of bending fatigue were compared with single load level fatigue life prediction equations and in good agreement. The SAS concept is can be extended to give a useful guide for manufacturers of structural body panels as well as antenna designers.

다층코팅을 이용한 C/C 복합재료의 내산화성 및 내마모성 증진 (Improvement of Oxidation Resistance and Erosion Resistance Properties of the C/C Composite with the Multilayer Coating)

  • 김옥희;이승윤;윤병일;박종욱
    • 한국세라믹학회지
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    • 제32권9호
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    • pp.1003-1008
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    • 1995
  • CVD-Si3N4/CVD-SiC/pack-SiC/pyro-carbon/(3-D C/C composite) multilayer coating was performed to improve the oxdiation resistance and erosion resistance properteis of the 3-D carbon/carbon composite, and the plasma test was performed to measure the oxidation resistance and erosion resistance properties. The thicknesses of each film layer were about 10${\mu}{\textrm}{m}$ for pack-SiC, 5${\mu}{\textrm}{m}$ for CVD-SiC and 40${\mu}{\textrm}{m}$ for CVD-Si3N4. When the multilayer coated specimen was exposed to the plasma flame with temperature of 500$0^{\circ}C$ for 20 seconds, it showed the weight loss five times less than that of the only pyro-carbon coated specimen.

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Static analysis of a multilayer piezoelectric actuator with bonding layers and electrodes

  • Xiang, H.J.;Shi, Z.F.
    • Smart Structures and Systems
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    • 제5권5호
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    • pp.547-564
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    • 2009
  • Based on the theory of piezoelasticity, an analytical solution for a typical multilayer piezoelectric composite cantilever is obtained by the Airy function method. The piezoelectric cantilever may consist of any number of layers. Moreover, the material and thickness for different layers may be different. The solution obtained in the present paper is concise and can be easily applied for the bending analysis of multilayer piezoelectric actuators considering the effect of bonding layers and electrodes. At last, a comprehensive parametric study is conducted to show the influence of electromechanical coupling (EMC), the number of piezoelectric layers, the elastic modulus of elastic layer and the thickness ratio on the bending behavior of actuators. Some interesting results for the design of multilayer piezoelectric actuators are presented.

축열조용 복합 다층 단열재의 단열 성능 연구 (A Study on the Insulation Performance of Composite Multilayer Insulation by Applciation of Heat Storage Tank)

  • 최규홍;황승식;신동훈;박우성;박대웅;손승길;정태용
    • 에너지공학
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    • 제23권3호
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    • pp.82-87
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    • 2014
  • 적층 단열재(multi-layer insulation, MLI)는 초전도 마그넷과 초전도 전력 케이블과 같은 초전도 응용기기의 냉각에 사용되는 저온유지장치(cryostat)에 외부 열침입을 차단하여 단열성능을 향상시키기 위해 사용된다. 적층 단열재는 인공위성에 사용되는 단열재로 적층단열재를 구성하는 자재의 종류와 적층층수 등에 따라 단열 성능이 변화한다. 본 연구에서는 적층 단열재의 원리를 이용한 축열조용 복합 다층 단열재(composite multilayer insulation, CMI)의 구성 재질 종류를 변경하고 적층 방식을 바꿈으로서 단열 성능이 바뀌는 것을 확인하였다. 실험은 KS C 9805의 방법을 이용하였으며, 복합 다층 단열재의 단열 성능 확인을 위해 동일한 조건의 축열조에 스티로폼을 적용하여 비교하였다. 또한, 실험 결과를 분석하기 위한 방법으로 기존 단열재에 대한 등가 두께를 비교하고 type별 CMI의 열전도율을 구해 비교하였다. 그 결과 복합 다층 단열재의 등가 두께는 스티로폼 보다 작아 동일 두께인 경우 스티로폼 보다 단열성능이 더 우수함을 확인할 수 있었다. 또한, 복합 다층 단열재의 구성 소재 및 적층 방식에 따라 전도, 대류 및 복사와 관련된 값들의 변화가 총괄 열전달계수에 영향을 미치는 것을 확인할 수 있었다.

Finite element based dynamic analysis of multilayer fibre composite sandwich plates with interlayer delaminations

  • Jayatilake, Indunil N.;Karunasena, Warna;Lokuge, Weena
    • Advances in aircraft and spacecraft science
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    • 제3권1호
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    • pp.15-28
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    • 2016
  • Although the aircraft industry was the first to use fibre composites, now they are increasingly used in a range of structural applications such as flooring, decking, platforms and roofs. Interlayer delamination is a major failure mode which threatens the reliability of composite structures. Delamination can grow in size under increasing loads with time and hence leads to severe loss of structural integrity and stiffness reduction. Delamination reduces the natural frequency and as a consequence may result in resonance. Hence, the study of the effects of delamination on the free vibration behaviour of multilayer composite structures is imperative. The focus of this paper is to develop a 3D FE model and investigate the free vibration behaviour of fibre composite multilayer sandwich panels with interlayer delaminations. A series of parametric studies are conducted to assess the influence of various parameters of concern, using a commercially available finite element package. Additionally, selected points in the delaminated region are connected appropriately to simulate bolting as a remedial measure to fasten the delamination region in the aim of reducing the effects of delamination. First order shear deformation theory based plate elements have been used to model each sandwich layer. The findings suggest that the delamination size and the end fixity of the plate are the most important factors responsible for stiffness reduction due to delamination damage in composite laminates. It is also revealed that bolting the delaminated region can significantly reduce the natural frequency variation due to delamination thereby improving the dynamic performance.

적층형 압전 세라믹 액추에이터에 대한 Ag-세라믹 복합소재 전극의 응용 (Application of Ag-Ceramic Composite Electrodes to Piezoelectric Multilayer Ceramic Actuators)

  • 김성훈;이용희;조성열;최문석;이재신;김일원;정순종;송재성
    • 한국전기전자재료학회:학술대회논문집
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    • 한국전기전자재료학회 2006년도 하계학술대회 논문집 Vol.7
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    • pp.331-332
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    • 2006
  • Ag-ceramic composite materials were investigated as internal electrodes for multilayer ceramic actuators (MLCA). Ag-ceramic pastes were prepared by adding PZT-based ceramic powders to a Ag patse in a range of 0 to 50 wt.%. PZT/Ag-PZT multilayered laminates were fabricated by tape casting and fired at low temperatures below $950^{\circ}C$. The addition of ceramic into the Ag electrode resulted in a decrease in the thermal expansion mismatch between the electrode and the ceramic sheet. The maximum strain of PZT/Ag-PZT multilayered actuators were $9{\times}10^{-4}$ under an electric field of 2.5MV/m. In conclusion, Ag-PZT composite materials are efficient for low cost piezoelectric MLCAs.

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Fabrication and characterization of PCL/TCP-coated PHBV composite multilayer as a bone plate

  • Kim, Yang-Hee;Song, Ho-Yeon;Lee, Byong-Taek
    • 한국재료학회:학술대회논문집
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    • 한국재료학회 2009년도 추계학술발표대회
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    • pp.39.2-39.2
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    • 2009
  • In this work, Poly($\varepsilon$-Caprolactone)(PCL) andpoly(3-hydroxybutyrate-co-3-hydroxyvalerate)(PHBV) mats were fabricated usingelectrospinning process. The electrospinning process is a simple and efficient method to fabricate the nanofibrous mats. PCL and PHBV is a kind of biodegradable polymer but their mechanical properties aren't good. For improving mechanical properties, PHBV mats were coated by TCP. Using PCL mats and TCP-coated PHBV composite mats, a bio-resorbablebone plate were made by pressing. Detailed micro-structural characterization was done by SEM techniques. Tensile strength and bending strength were also evaluated for mechanical properties. The cytotoxicity evaluation ofPCL/TCP-coated PHBV composite multilayer was done by MTT assay. The evidence obtained in this work implies the potential for use as a biodegradable boneplate.

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접착필름의 영향을 고려한 다층 복합재료 안테나 구조 설계 (Design of Multilayer Composite-Antenna-Structures Considering Adhesive)

  • 김동섭;박현철;백위상;황운봉
    • Composites Research
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    • 제20권2호
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    • pp.27-31
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    • 2007
  • 미래의 환경에서는 위성을 이용한 통신서비스의 운송체 내에서의 사용이 기하급수적으로 확대될 전망이다. 이를 위해서는 안테나의 성능 향상 및 역학적 에너지의 고효율성에 기하고, 구조적인 안정을 보장하기 위한 복합 안테나 구조의 설계, 제조 및 해석 기술이 필요하다. 복합 안테나 구조가 안테나의 역할 및 구조체로의 역할을 하기 위해서는 접착필름의 사용이 필수적이다. 하지만 접착필름은 얇은 두께로 인하여 설계시 고려되지 못하고 유전체로 작용하여 전자기적 영향을 끼치게 되어 설계자가 기대하는 성능을 얻지 못한다. 따라서, 이러한 접착필름의 전자기적 특성을 실험적으로 알아본다.