• Proceedings of the Korean Society of Precision Engineering Conference
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• 2008.06a
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• pp.811-812
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• 2008

• 한국신재생에너지학회:학술대회논문집
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• 2010.06a
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• pp.62.2-62.2
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• 2010

박막 실리콘 태양 전지는 저가격화 및 대량생산, 대면적화에 유리하다는 장점을 가지고 있다. 단점으로 지적되는 낮은 효율을 극복하기 위해 광흡수층의 밴드갭이 서로 다른 두 개 이상의 박막을 적층하여, 넓은 파장 대역의 빛을 효과적으로 흡수함으로써 광변환 효율을 올리기 위한 많은 연구가 이루어지고 있다. 서로 다른 밴드갭의 광흡수층을 가진 p-i-n 구조를 다중 적층하여 고효율의 태양 전지를 제작하기 위해서는 n-도핑층과, p-도핑층 간에 전자와 정공이 빠르게 재결합할 수 있는 터널 접합(Tunnel Recombination Junction)의 형성이 필수적이며, 이때 광손실이 최소화되도록 해야한다. 만약 터널 접합이 적절하게 형성되지 않으면 결합되지 않은 전자와 정공이 도핑층 사이에 쌓이게 되고, 도핑층 사이의 저항 증가로 태양 전지의 광변환 효율은 크게 하락한다. 이번 연구에서는 터널 접합이 잘 이루어지게 하기 위한 n-도핑층 및 p-도핑층 박막의 특성과, 터널 접합의 특성에 따른 적층형 태양 전지의 광효율 변화를 확인하였다. 광흡수층 및 도핑층은 TCO($SnO_2:F$, Asahi) 유리 기판 위에 PECVD를 사용하여 p-i-n 구조로 RF Power 조건에서 증착되었고, ${\mu}c$-Si 광흡수층의 경우에는 VHF Power 조건에서 증착되었다. 광흡수층이 a-Si/${\mu}c$-Si의 구조를 가지는 이중 접합 태양 전지에서 ${\mu}c$-Si n-도핑층/${\mu}c$-Si p-도핑층 사이의 터널 접합 실험 결과 n-도핑층 및 p-도핑층의 결정화도와 도핑 농도를 조절하여 터널 접합의 저항을 최소화했고, 터널 접합 특성이 이중 접합 셀의 광효율 특성과 유사한 경향을 보임을 확인하였다. 광흡수층이 a-Si/a-SiGe/${\mu}c$-Si의 구조를 가지는 삼중 접합 태양 전지 실험의 경우 a-Si과 a-SiGe 광흡수층 사이에 ${\mu}c$-Si n-도핑층/${\mu}c$-Si p-도핑층/a-SiC p-도핑층의 구조를 적용하여 터널 접합을 형성하였으며, ${\mu}c$-Si p-도핑층의 두께 및 박막 특성을 개선하여 광손실이 최소화된 터널 접합을 구현하였고, 삼중 접합 태양 전지에 적용되었다.

• Composites Research
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• v.32 no.4
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• pp.185-190
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• 2019

This work investigates the elastic buckling characteristics of laminated composite trapezoidal corrugated plates with simply supported edges using the analytical method. In the analysis, three types of in-plane loading conditions: uniaxial, biaxial and shear loads are considered. Because it is very difficult to determine the mechanical behavior of 3-dimensional corrugated structures analytically, the equivalent homogenization model is adapted to investigate the overall mechanical behavior of corrugated plates. The corrugated element is homogenized as an orthotropic material. The previous formulae for bending rigidities of corrugated plate are adapted in this paper. The comparisons of the proposed analytical results with those of FEA based on the shell element are made to verify the proposed analytical method. In the comparison study both the critical buckling loads and the buckling mode shapes are presented. Some numerical results are presented to check the effect of the geometric properties.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.12 no.4
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• pp.563-571
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• 1999

변단 면과 다양한 경계조건을 갖는 보와 타워구조물의 제1모드에서의 고유진동수를 구하는 정확한 해는 1974년에 Kim에 의해 발표되었다. 최근 이 방법은 복합재료 적층 판을 포함하는 2차원 문제의 제 1모드 진동해석에 확장되었으며, 다양한 경계조건과 불규칙 단면을 갖는 판에 매우 효과적이다. 이 논문에서는 변단 면과 경계조건에 따른 특별직교 이방성 판에 대한, Kim에 의해 개발된 간편한 진동해석 방법의 응용결과가 주어진다. 또한 집중하중들에 대한 영향이 연구되었다.

• Computational Structural Engineering
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• v.10 no.4
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• pp.267-280
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• 1997

This paper deals with the development of simplified methods to predict the creep deformation of reinforced concrete beams. The layer approach based on a degenerate kernel of compliance function in form of Dirichlet series is mentioned and a simplified analytical method derived from the equilibrium equations and compatibility conditions is proposed to overcome the sophisticated calculation procedures in the classical creep analysis. Correlation studies between analytical and experimental results and design codes are conducted with the objective to establish the validity of the proposed methods. Besides, various parameter studies are conducted with the objective to identify the effects of cracking, steel ratio and sectional shape in the creep deformation and the obtained results are discussed.

• Composites Research
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• v.20 no.4
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• pp.25-30
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• 2007

The advanced fiber-reinforced laminated composites are widely used in a variety of engineering applications such as aerospace, marine, mechanical and civil engineering for weight savings because of their high specific strength and stiffness. The material properties of ply is known to have larger variations than that of conventional materials and very sensitive to the loading direction. Therefore, it is important to consider the variations on designing the laminated composite. This paper demonstrates the importance of considering uncertainties through examining the effect of material properties variations on various design requirements such as tip deflection, natural frequency and buckling stress using COMSOL-MATLAB interface.

• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.6
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• pp.1391-1407
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• 1990

In this paper, optimization procedures are presented considering the static and dynamic constraints for laminated composite plate and hybrid laminated composite plate subject to concentrated load on center of the plates. Design variables for this problem are ply angle or ply thickness. Deflection, natural frequency and specific damping capacity are considered as constraints. Using a recursive linear programming method, the nonlinear optimization problems are solved. By introducing the design scaling factor, the number of iterations is reduced significantly. Composite plates could be designed optimally combined with FEM analysis under various conditions. In the optimization procedure, verification for both analysis and design of the laminated composite plates are compared with the results of the others. Various design results are presented for the laminated composite plates and hybrid laminated composite plates.

• Transactions of the Korean Society of Mechanical Engineers
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• v.14 no.6
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• pp.1365-1381
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• 1990

A $C^{0}$ continuous displacement finite element method based on a higher-order shear deformation theory is employed in the prediction of the transient response of laminated composite plates subjected to low-velocity impact. A modified contact law was applied to calculate the contact force during impact. The discrete element chosen is a nine-noded quadrilateral with 5 degree-of-freedom per node. The Wilson-.theta. time integration algorithm is used for solving the time dependent equations of the impactor and the central difference method was adopted to perform time integration of the plate. Numerical results, including the contact force history, deflection, and velocity history, are presented. Comparisons of numerical results using a higher order theory and a first-order theory show that using a higher order theory provides more accurate results. Effects of boundary condition, impact velocity, and mass of the impactors are also discussed.d.

• Journal of the Korean Society of Manufacturing Technology Engineers
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• v.19 no.2
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• pp.235-240
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• 2010

The recent trend of vehicle design aims at crash safety and environmentally-friendly aspect. For the crash safety aspect, energy absorbing members should be absorbed with collision energy sufficiently. But vehicle structure must be light weight for the environmentally-friendly aspect, in order to improve fuel efficiency and to reduce tail gas emission. Therefore, the light weight of vehicle must be achieved in a status of securing safety of crash. An aluminum or CFRP (Carbon Fiber Reinforced Plastics) is representative one among the light-weight materials. In this study, impact collapse behavior of circular hybrid thin-walled member is evaluated. The hybrid members are manufactured by wrapping CFRP prepreg sheets outside the aluminum circular members in the autoclave. Because the CFRP is an anisotropic material whose mechanical properties change with its stacking condition, special attention is given to the effects of the stacking condition on the collapse behavior evaluation of the hybrid thin-walled member. Collapse mode and energy absorption capability of the hybrid thin-walled member are analyzed with change of the fiber orientation angle and interface number.

• Transactions of the Korean Society of Mechanical Engineers
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• v.10 no.6
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• pp.929-936
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• 1986

Free vibration characteristics of laminated orthotropic circular cylindrical shells with clamped free boundary condition are investigated. The solution is obtained through a direct solution procedure with axial mode displacements represented as simple Fourier series expressions. On the basis of the thin shell theories of Sanders, Love, Loo, Morley and Donnell, the 4*$ frequency determinant is derived and is expressed in a unified form. Various numerical examples determining the natural frequencies of circular cylindrical shells with isotropic material and also with layers of orthotropic elastic material arbitraily laminated either symmetrically or anti-symmetrically about the shell middle surface. The results obtained compared very well with some available experimental and numerical results.