• 제목/요약/키워드: Laminated

검색결과 2,080건 처리시간 0.03초

실리콘이 라미네이팅된 신축성 소재의 위생 및 안전성과 역학적 성능 (Analysis of Physical Performance, Hygiene and Safety of Silicone-Laminated Stretch Material)

  • 권명숙;정기수
    • 한국의류학회지
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    • 제31권1호
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    • pp.77-84
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    • 2007
  • The purpose of this study was to investigate and to compare the performances of silicone laminated materials sold for swimming cap in market, to get the basic data for product development. We selected 4 specimens and tested their air permeability, waterproofness and breathability. We also tested the physical and mechanical properties of the specimens using KES system. Silicone-laminated material was not bursted on high hydraulic pressure since silicone membrane gave waterproofness while PU/Polyester substrate gave elasticity. It didn't have air permeability and breathability at all. Any toxic materials such as Formaldehyde, Deldrin, PCP, Amin, TDBPP were not detected in silicone-laminated material and other materials. Silicone-laminated material had higher stretchability with the low force but it had lower elastic recovery and shape stability comparing to PU laminated material. It had lower flexibility than PU laminated material. It had lower unrecoverable amount in shearing direction. Friction coefficient was higher in silicone-laminated material than PU laminated material due to its surface stickiness. It was compressed easily and its compression resiliency was higher with compared to PU laminated material.

전단변형을 고려한 이방성 적층판의 좌굴해석 (Buckling Analysis of Anisotropic Laminated Plates with Shear Deformation)

  • 최용희;권택진
    • 한국전산구조공학회:학술대회논문집
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    • 한국전산구조공학회 2001년도 가을 학술발표회 논문집
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    • pp.361-368
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    • 2001
  • This paper deals with the buckling load of antisymmetric angle-ply and cross-ply laminated rectangular plates. Buckling analysis is preformed for a simply supported, shear deformable laminated plate subjected to uniaxial compression and biaxial compression combined with uniform lateral pression. The shear deformation theory is considered to figure out a more exact behavior of laminated plates exactly. The purposes of this study are to formulate anisotropic laminated plates with shear deformation and to investigate the buckling load according to the various variables of laminated plates by using the exact solutions for anisotropic laminated plates having simply supported boundary.

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CF/Epoxy 복합재 적층쉘의 충격특성 (Impact Characteristics on the Laminated Shell for CF/Epoxy Composite)

  • 양현수;정풍기;김영남;이종선
    • 대한안전경영과학회지
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    • 제6권1호
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    • pp.311-323
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    • 2004
  • This paper is to study the energy absorption characteristics of CF/Epoxy(Carbon Fiber/Epoxy Resin) laminated shell with the various curvatures subjected to transverse impact loadings under the low impact velocity in consideration of design of structural members for use of transportation machine, which are consisted of the characteristics of high stiffness, strength and lightweight. The curvature radius are associated with the energy absorption characteristics of CF/Epoxy laminated shell which is brittleness material. In all tests, maximum load of CF/Epoxy laminated plate is higher than that of laminated shell with curvature, but maximum deflection is lower. And then absorbed energy of laminated shell with curvature is higher than laminated plate(curvature radius is unlimited), As curvature radius is increased, the absorbed energy is increased in laminated shell with curvature.

A refined discrete triangular Mindlin element for laminated composite plates

  • Ge, Zengjie;Chen, Wanji
    • Structural Engineering and Mechanics
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    • 제14권5호
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    • pp.575-593
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    • 2002
  • Based on the Mindlin plate theory, a refined discrete 15-DOF triangular laminated composite plate finite element RDTMLC with the re-constitution of the shear strain is proposed. For constituting the element displacement function, the exact displacement function of the Timoshenko's laminated composite beam as the displacement on the element boundary is used to derive the element displacements. The proposed element can be used for the analysis of both moderately thick and thin laminated composite plate, and the convergence for the very thin situation can be ensured theoretically. Numerical examples presented show that the present model indeed possesses the properties of higher accuracy for anisotropic laminated composite plates and is free of locking even for extremely thin laminated plates.

구조용 목질재료의 전단파괴기구 해명을 위한 파면해석적 연구 (Fractography of the Wood Materials Ruptured by Shear Stress)

  • 김남훈;;홍순일;이성재
    • 한국가구학회지
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    • 제10권1호
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    • pp.23-32
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    • 1999
  • The ultrastructural characteristics of shear fracture surfaces of laminated wood prepared from major four Korea wood specimens were examined. Commercial urea and urethan resin were used as adhesives for laminated woods of both homospecies and heterospecies. The morphology of fracture surface was observed using an optical microscopy and scanning electron microscopy. Three anatomical failure types were recognized : intercell failure, intrawall failure and transwall failure. In dry specimen, failure occurred mainly in woods. Laminated woods of softwoods showed mostly intrawall failure and transwall failure of tracheids, and them of hardwoods indicated mainly intrawall failure and interwall failure. Laminated woods prepared with urethan resin showed coarse fracture surface, on the other hand, those prepared with an urea formaldehyde resin had clean surface. In wet specimen, failure occurred dominantly in glue line. Intrawall failure and flags were characterized in laminated wood prepared with urethan resin. In heterospecies laminated woods, failure was occurred mainly in softwood. Consequently, fracture morphology of laminated wood may be influenced by adhesives, moisture content, species and anatomical characteristics.

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비등방성 적층 캔틸레버 박판 및 후판의 해석연구 (Study on the Analysis of Anisotropic Laminated Cantilever Thin Plates and Anisotropic Laminated Cantilever Thick Plates)

  • 박원태
    • 복합신소재구조학회 논문집
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    • 제1권4호
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    • pp.1-5
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    • 2010
  • In this study, it is presented analysis results of bending problems in the anisotropic cantilever thick plates and the anisotropic laminated cantilever thin plates bending problems. Finite element method in this analysis was used. Both Kirchoff's assumptions and Mindlin assumptions are used as the basic governing equations of bending problems in the anisotropic laminated plates. The analysis results are compared between the anisotropic laminated cantilever thick plates and the anisotropic laminated cantilever thin plates for the variations of thickness-width ratios.

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Frequency and thermal buckling information of laminated composite doubly curved open nanoshell

  • Dai, Humin;Safarpour, Hamed
    • Advances in nano research
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    • 제10권1호
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    • pp.1-14
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    • 2021
  • In the present computational approach, thermal buckling and frequency characteristics of a doubly curved laminated nanopanel with the aid of Two-Dimensional Generalized Differential Quadrature Method (2D-GDQM) and Nonlocal Strain Gradient Theory (NSGT) are investigated. Additionally, the temperature changes along the thickness direction nonlinearly. The novelty of the current study is in considering the effects of laminated composite and thermal in addition of size effect on frequency, thermal buckling, and dynamic deflections of the laminated nanopanel. The acquired numerical and analytical results are compared by each other to validate the results. The results demonstrate that some geometrical and physical parameters, have noticeable effects on the frequency and pre-thermal buckling behavior of the doubly curved open cylindrical laminated nanopanel. The favorable suggestion of this survey is that for designing the laminated nano-sized structure should pay special attention to size-dependent parameters because nonlocal and length scale parameters have an important role in the static and dynamic behaviors of the laminated nanopanel.

유리섬유 보강적층재의 파괴인성 특성 (Fracture Toughness of Glass Fiber Reinforced Laminated Timbers)

  • 김선호;홍순일
    • Journal of the Korean Wood Science and Technology
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    • 제43권6호
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    • pp.861-867
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    • 2015
  • 유리섬유 보강적층재의 파괴인성을 평가하기 위하여 Compact tension (CT)형 시험을 실시하였다. 보강재는 직물형 유리섬유와 시트형 유리섬유강화플라스틱을 사용하였으며, 보강적층재는 층재사이에 보강재를 삽입 적층하였다. ASTM D5045에 의거하여 CT형 시험편을 제작하였다. 시험편의 길이는 끝면거리를 고려하여 선정하였으며, 인위적인 노치 끝에 볼트구멍(12 mm, 16 mm, 20 mm)을 선공하였다. 시트형 유리섬유강화플라스틱 보강적층재의 파괴인성하중은 보강하지 않은 적층재보다 최대 33% 증가하였으며, 직물형 유리섬유 보강적층재는 최대 152% 증가하였다. 이중외팔보(Double Cantilever Beam)이론에 의한 응력확대계수는 시트형 유리섬유강화플라스틱 보강적층재의 경우 1.08~1.38이었으며, 직물형 유리섬유 보강적층재는 1.38~1.86이었다. 이는 직물형 유리섬유 보강적층재의 경우 유리섬유와 층재의 섬유배열방향이 직교하여 파괴하중으로 인한 목재의 할렬진행을 억제시켰기 때문이다.

멜라민시트 적층 MDF 마루판재의 가열에 의한 치수변화 (Dimensional Change of Melamine Sheet Laminated MDF Flooring by Heating)

  • 민일홍;김의식;한규성
    • Journal of the Korean Wood Science and Technology
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    • 제24권4호
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    • pp.32-39
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    • 1996
  • The overall purpose of this study was to investigate the dimensional changes of melamine sheet laminated medium density fiberboard(MDF) floorings by sub-heating system(Ondol). This study was also conducted to improve the properties of melamine sheet laminated MDF floorings. The effects of density, resin content, manufacturing speed of MDF and types of melamine sheet on dimensional and weight changes of floorings were investigated. The results were as followings. 1. Dimensional and weight change of melamine sheet laminated MDF flooring by heating decreased with decreasing the density of MDF. 2. Dimensional and weight change of melamine sheet laminated MDF flooring by heating decreased with increasing the resin content of MDF. 3. Dimensional and weight change of melamine sheet laminated MDF flooring by heating decreased with decreasing the manufacturing speed of MDF. 4. Dimensional change of melamine sheet laminated MDF flooring in width direction by heating was doubled than that in machine direction. 5. Dimensional change and curling of high pressure melamine laminate(HPM) laminated MDF flooring by heating was less than those of low pressure melamine laminate(LPL) flooring. 6. Weight loss of melamine sheet laminated MDF flooring by heating has linear relationship with shrinkage.

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Measurement of Dynamic MOE of 3-Ply Laminated Woods by Flexural Vibration and Comparison with Blending Strength and Creep Performances

  • Park, Han-Min;Byeon, Hee-Seop
    • Journal of the Korean Wood Science and Technology
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    • 제34권2호
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    • pp.46-57
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    • 2006
  • To estimate nondestructively strength performances of laminated woods, 3-ply parallel- and cross-laminated wood specimens exposed under atmosphere conditions after bending creep test were prepared for this study. The effects of density of species, arrangement of laminae and lamination types on dynamic MOE obtained by flexural vibration were investigated, and regression analyses were conducted in order to estimate static bending strength and bending creep performances. Dynamic MOE of parallel-laminated woods showed 1.0~1.2 times higher values than static bending MOE, and those of cross-laminated woods showed 1.0~1.4 times higher values than static bending MOE. The degree of anisotropy of dynamic MOE perpendicular to the grain of face laminae versus that parallel to the grain of face laminae was markedly decreased by cross-laminating. There were strong correlations between dynamic MOE by flexural vibration and static bending MOE (correlation coefficient r = 0.919~0.972) or bending MOR (correlation coefficient r = 0.811~0.947) of 3-ply laminated woods, and the correlation coefficient were higher in parallel-laminated woods than in cross-laminated woods. It indicated that static bending strength performances were able to be estimated from dynamic MOE by flexural vibration. Also, close correlations between the reciprocal of dynamic MOE by flexural vibration and initial compliance at 0.008 h of 3-ply laminated woods were found (correlation coefficient r = 0.873~0.991). However, the correlation coefficient between the reciprocal of dynamic MOE and creep compliance at 168 h of 3-ply laminated woods was considerably lower than those between dynamic MOE and initial compliance, and it was hard to estimate creep compliance with a high accuracy from dynamic MOE due to the variation of creep deformation.