• 제목/요약/키워드: 샌드위치 평판

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이방성판을 사용한 샌드위치판의 차음특성 (Characteristics of Sound Insulation in Sandwich Plates with Orthotropic Skin Plate)

  • 강현주;김봉기;김재승
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2004년도 추계학술대회논문집
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    • pp.853-856
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    • 2004
  • 조립식 건축용 외장재로 사용되는 샌드위치판은 충분한 구조강도가 필요하기 때문에 표면재가 굴곡판 (Corrugated plate)으로 구성되는 경우가 많다. 샌드위치판의 부재로서 굴곡판을 이방성판으로 고려하면 이론 해석상 많은 어려움이 있다. 그러나 이방성판이 샌드위치판의 부재로서 다중판으로 되었을 때에는 단판에서 보인 여러 가지 현상들이 다중판 효과에 비해서 크지않음이 실험결과에서 보이고 있다. 이러한 사실에 착안하여 이방성판을 등가의 평판으로 모델링한 후 샌드위치 모델을 적용하여 이론 예측을 수행하였다. 계측결과와 비교로부터 본 연구에서 사용된 방법은 좋은 일치를 보이고 있다.

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가변 샌드위치 구조물의 형상최적설계 (Shape Optimal Design of Variable Sandwich Structure)

  • 박철민;박경진;이완익
    • 대한기계학회논문집
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    • 제17권9호
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    • pp.2162-2171
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    • 1993
  • Geneal Structure optimization is utilized to minimize the weight of structures while satisfying constraints imposed on stress, displacements and natural frequencies, etc. Sandwich structures consist of inside core and outside face sheets. The selected sandwich structures are isotropic sandwich beams and isotropic sandwich plate. The face sheets are treated as membrane and assumed to carry only tensions, while the core is assumed to carry only transverse shear. The characteristic of the varying area are considered by adding the projected component of the tension to the transverse shear. The bending theory and energy method are adopted for analyzing sandwich beams and plates, respectively. In the optimization process, the cost function is the weight of a structure, and a deflection and stress constraints are considered. Design variable are thickness and tapering coefficients which determine the shape of a structure. An existing optimization code is used for solving the formulated problems.

샌드위치 평판의 모드 감쇠 최대화를 위한 점탄성층 두께 결정법 (A Method to Determine Optimum Viscoelastic Layer Thickness of Sandwich Plate for Maximum Modal Damping)

  • 남대호;신윤호;김광준
    • 한국소음진동공학회논문집
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    • 제16권7호
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    • pp.690-696
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    • 2006
  • Thickness of damping layer in sandwich plate needs to be optimized in order to make modal loss factor of the sandwich plate maximum. Since previous studies were interested in noise reductions over high frequency range, the modal properties were derived based on simply supported boundaries. This conventional formula is approximately applicable to other boundary conditions over high frequency range only. The purpose of this study is to propose a method to determine optimum damping layer thickness of sandwich plate for maximum modal damping in low frequency range when the boundary condition is not a simple support. The conventional RKU equation based on simply supported boundary is modified to reflect other boundary conditions and the modified RKU equation is subsequently applied to determine the optimum damping layer thickness for arbitrary conditions. In order to reflect frequency-dependent characteristics of elastic modulus of the damping layer, an iteration method is proposed in determining the modal properties. Test results on sandwich plates for optimum damping layer thickness are compared with predictions by the proposed method and conventional method.

스펙트럴유한요소법을 적용한 점탄성층 샌드위치평판의 진동해석 (Applications of Spectral Finite Element Method for Vibration Analysis of Sandwich Plate with Viscoelastic Core)

  • 이성주;송지훈;홍석윤
    • 대한조선학회논문집
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    • 제46권2호
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    • pp.155-164
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    • 2009
  • In this paper, a spectral finite element method for a rectangular sandwich plate with viscoelastic core having the Levy-type boundary conditions has been plated. The sandwich plate consists of two isotropic and elastic face plates with a surfaced-bonded viscoelastic core. For the analysis, the in-plane and transverse energy in the face plates and only shear energy in the core are considered, respectively. To account for the frequency dependent complex shear modulus of the viscoelastic core, the Golla-Hughes-McTavish model is adopted. To evaluate the validity and accuracy of the proposed method, the frequency response function and dynamic responses of the sandwich plate with all edges simply supported subject to an impact load are calculated and compared with those calculated by a finite element method. Though these calculations, it is confirmed that the proposed method is very reliable and efficient one for vibration analysis of a rectangular sandwich plate with viscoelastic core having the Levy-type boundary conditions.

공작기계를 위한 보와 평판의 샌드위치 구조 설계에 관한 파라메트릭 연구 (Parametric Study on the Design of Sandwich Beams and Plates for Machine Tool Structures)

  • 김대일;장승환
    • 한국공작기계학회논문집
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    • 제15권1호
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    • pp.39-48
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    • 2006
  • In this paper, polymer composites based sandwich structures like beams and plates are optimised by using parametric study. The structures are composed of fibre reinforced composites for facial material and resin concrete and PVC foam for core materials. The stacking sequences and thickness of the composites are controlled as major parameters to find out the optimal condition for machine tool components. For the plate structure of machine tool bed composites-skined sandwich structure which has several ribs are proposed to enhance bending stiffnesses in two major directions at the same time. Dynamic robustness of a machine tool structure is investigated using modal analysis. From the results optimal configuration and materials for high precesion machine tools are proposed. And the plate was made of fiber reforced composite material and PVC foam.

좌굴을 고려한 샌드위치형 판 구조물의 모드해석 (Modal Analysis of Sandwich Plate Structure Considering Buckling)

  • 한근조;안찬우;안성찬;홍도관;한동섭
    • 한국정밀공학회지
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    • 제19권6호
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    • pp.104-108
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    • 2002
  • Sandwich plate structure is widely used in various fields of industry due to its excellent strength and stiffness compared with weight. In this paper, the mechanical behavior of sandwich plate structure with honeycomb core considering buckling is investigated in detail. The focus of the analysis is to evaluate strength and stiffness of the plate structure with critical stress, natural frequency, and mode shapes. The results of this investigation are obtained from detailed finite element analysis for various parameters, such as length, height ratio, and thickness ratio of honeycomb core.

좌굴을 고려한 샌드위치형 판 구조물의 모드해석 (Modal Analysis of Sandwich Plate Structure Considering Bucking)

  • 한근조;안찬우;안성찬;홍도관;한동섭
    • 한국정밀공학회:학술대회논문집
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    • 한국정밀공학회 1997년도 추계학술대회 논문집
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    • pp.702-705
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    • 1997
  • Sandwich plate structure is widely used in various fields of industry due to its excellent strength and stiffness compared with weight. In this paper, the mechanical behavior of sandwich plate structure with honeycomb core considering buckling is investigated in detail. The focus of the analysis is to evaluate strength and stiffness of the plate structure with critical stress, natural frequency, and mode shapes. The results of this investigation are obtained from detailed finite element analysis for various parameters, such as length, height ratio, and thickness ratio of honeycomb core

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두껍고 비대칭인 FRP면재를 갖는 Sandwich 평판의 구조해석 (A Structural Analysis of Sandwich Plate with Unsymmetrical FRP Thick Faces)

  • 김익태;김기성
    • 대한조선학회논문집
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    • 제32권1호
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    • pp.132-140
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    • 1995
  • 선체의 중량을 감소시키기 위한 구조적인 형식중의 하나가 샌드위치 type이고 고속선의 면재는 F.R.P.와 Kevlar/Epoxy를, 심재로는 P.V.C.foam을 많이 사용한다. 본 연구에서는 면재의 두께가 두껍고 윗면재와 아랫면재의 두께가 다른 비대칭인 경우에 대하여 Rayleigh-Ritz의 에너지방법으로 해석하였다. 그리고 얇은 면재와의 비교를 위하여 등방성이고 중립축에 대칭인 평판을 기준하여 굽힘응력, 전단응력, 국부적인 굽힘응력, 막응력효과를 고려한 응력들을 면재2종류와 심재3종류에 대해서 비교하고 해석하였다.

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개선된 일차전단변형이론을 이용한 복합재료 적층평판의 고정밀 해석 (An Accurate and Efficient Analysis of Composite Plates Based on Enhanced First-order Shear Deformation Theory)

  • 김준식;조맹효
    • 한국전산구조공학회논문집
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    • 제19권4호
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    • pp.407-418
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    • 2006
  • 본 논문에서는 일차전단변형이론(FSDT)을 이용한 복합재료 적층평판의 고정밀 해석기법을 소개한다. 전단수정계수가 자동적으로 포함되도록 횡방향 전단 변형에너지를 혼합변분이론(mixed variational theorem)을 이용하여 개선하였다. 혼합변분이론에서는 변분을 횡방향 응력들에 대해서만 취하였다. 가정된 횡방향 전단응력은 효율적인 고차이론(Cho and Parmerter, 1993)으로부터 구하였다 횡방향 수직응력은 3차 다항식으로 가정하였고, 무전단 응력조건과 평판의 윗면과 아랫면에서의 응력을 만족하는 조건을 부과함으로써 얻었다. 한편, 변위들에 대해서는 일차전단변형이론의 변위장을 사용하였다. 이렇게 해서 얻어진 변형 에너지를 본 논문에서는 EFSDTM3D이라고 명명 하였다. 본 논문에서 개발된 EFSDTM3D는 변위와 응력의 계산에서 고전적인 FSDT와 같은 정도의 계산 효율을 가지면서, 동시에 변위와 응력의 두께방향의 정확도를 면내 방향 응력들에 대한 최소오차자승법에 기초하여 응력 회복 과정을 적용함으로써 개선하였다. 계산된 결과는 고전적인 FSDT, 3차원 탄성해, 그리고 참고문헌 중에서 이용 가능한 결과들과 비교하여 검증하였다.