• 한국신재생에너지학회:학술대회논문집
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• 2010.06a
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• pp.63.1-63.1
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• 2010

실리콘 박막 태양전지의 효율을 향상시키기 위해 밴드갭이 다른 흡수층을 적용한 tandem형 적층 태양전지를 이용하고 있다. 일반적으로 1.7eV이상의 밴드갭이 큰 비정질 실리콘을 이용하여 단파장의 빛을 흡수하고, 상대적으로 낮은 1.1eV 정도의 밴드갭을 갖는 미세결정 실리콘 층으로 장파장을 흡수하게 된다. 이렇게 연결된 tandem형 태양전지의 효율을 극대화하기 위해서는 각 태양전지에서 발생하는 전류 밀도를 일치시키는 것이 필요하다. 이를 위해 비정질 실리콘의 두께가 증가되는 경우가 있는데 이러한 경우 비정질 실리콘의 광열화 특성(Lihgt-induced degradation)으로 안정화 효율이 감소하게 된다. 따라서 비정질 실리콘 태양전지의 전류 밀도를 향상 시켜 두께를 최소화하는 것이 매우 중요하다. Tandem형 태양전지에서 비정질 실리콘 태양전지의 전류 밀도를 향상시키기 위해 두 개의 전지사이에 광 반사층을 적용하여 태양전지를 제조하게 된다. 이러한 경우 비정질 실리콘의 전류 밀도는 증가하지만, 광 반사 층의 장파장 흡수로 인하여 하부 태양전지의 전류 밀도 감소가 더 커지게 되어 전체 발생 전류 밀도는 오히려 감소하게 된다. 본 논문에서는 비정질 실리콘의 밴드갭을 제어하여 광 흡수 파장 영역 확대로 전류 밀도를 향상시키는 연구를 진행하였다. PECVD의 RF power 조건을 제어하여 1.75eV에서 1.67eV까지 밴드갭을 변화시켰다. 이와 같은 조건의 박막을 광 흡수층으로 갖는 p-i-n 구조의 비정질 실리콘 태양전지를 제작하였다. i층의 밴드갭이 감소됨에 따라 장파장 영역의 흡수가 확대되어 전류 밀도가 증가 하였지만, Voc의 감소가 컸다. 이는 i층의 밴드갭이 좁아짐에 따라 p층과의 불연속성이 커졌기 때문이다. 이러한 악영향을 줄이기 위해 p층과 i층 사이에 buffer층을 삽입하여 태양전지를 제작하였다. 이와 같은 최적의 buffer층 삽입을 통하여 불연속성을 줄임으로써 Voc의 상승효과를 확인하였다. 본 연구의 결과로 좁은 밴드갭을 갖는 광 흡수 층을 적용하여 전류 밀도를 향상시키고, 최적화된 buffer층 삽입으로 Voc를 향상시킴으로써 고효율의 비정질 실리콘 태양전지를 제작하였다. 이를 tandem형 태양전지에 적용할 경우 초기 효율뿐만 아니라 얇은 두께에서 제조할 수 있기 때문에 광열화 특성이 향상되어 안정화 효율의 증가를 가져올 수 있다.

• Review of Korean Society for Internet Information
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• v.16 no.2
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• pp.65-69
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• 2015

• Journal of the Korean Society of Manufacturing Process Engineers
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• v.21 no.3
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• pp.63-69
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• 2022

Compressor efficiency must be improved to reduce refrigerator power consumption. In this study, the heat dissipation rate through the compressor housing is increased via gap flow passages between the compressor body and housing. Four types of gap flow passages are considered for achieving the maximum heat-dissipation rate. In addition, thermal analysis is performed to examine the effect of increased heat dissipation rate on the energy efficiency ratio (EER). The results show that the heat dissipation rate, compressor superheat, and compressor EER increased by up to approximately 52%, 3 ℃, and approximately 1%, respectively.

• Journal of the Korean Society of Propulsion Engineers
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• v.24 no.1
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• pp.34-46
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• 2020

Computational assessment of gas-dynamic characteristics is explored for a three-dimensional counter-flow thrust vector control system in a rectangular supersonic nozzle. This convergent-divergent nozzle is designed by Method of Characteristics and its design Mach number is specially set as 2.5. Performance variations of the counter-flow vector system are illustrated by varying the gap height of the secondary flow duct. Key parameters are quantitatively analyzed, such as static pressure distribution along the centerline of the upper suction collar, deflection angle, secondary mass flow ratio, and resultant thrust coefficient. Additionally, the streamline on the symmetry plane, three-dimensional iso-Mach number surface contour, and three-dimensional turbulent kinetic energy contour are presented to reveal overall flow-field characteristics in detail.

• Korean Chemical Engineering Research
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• v.56 no.4
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• pp.585-591
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• 2018

Characteristics of nano-structured $SiO_2:Zn$ hollow powders prepared in the micro drop fluidized reactor process were investigated with respect to bandgap energy and surface activity. The $SiO_2:Zn$ hollow powders were successfully prepared continuously in the one step process with reasonable production efficiency, with varying the amount of THAM (tris(hydroxymethyl)-aminomethane) additive and concentration of $Zn^{2+}$ ions. The doping of $Zn^{2+}$ ions into $SiO_2$ lattice led to the reduction of bandgap energy by forming the acceptor level of $Zn^{2+}$ below the conduction band of $Si^{4+}$ ions. The hollow shape also contributed to reduce the bandgap energy of $SiO_2:Zn$ powders. The doping of $Zn^{2+}$ ions into $SiO_2$ hollow powders could enhance the surface activity by forming SiO-H stretching and oxygen vacancies at the surface of $SiO_2:Zn$ powders.

• Nuclear Engineering and Technology
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• v.22 no.2
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• pp.116-127
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• 1990

The fission gas release model used In the SPEAR-BETA fuel performance code was modified by use of effective thermal conductivity for cracked fuel and by laking Into account axial fission-gas mixing between the fuel-clad gap and the plenum. With use of this modified model the fission gas release was analyzed under various power ramping conditions of P$_{max}$ and $\Delta$.fP. Effective fuel thermal conductivity that accounts for the effect of fuel tracking was used in calculation of the fuel temperature distribution and the Internal gas pressure under power ramping conditions. Mixing and dilution effects due to axial gas flow were also considered in computing the width and the thermal conductivity of the gap. The effect of axial gas flow w3s solved by the Crank-Nicholson method. The finite difference method was used to save running time in the calculation. The present modified fission-gas release model was validated by comparing its predicted results with experimental data from various lamping tests In the literature and calculated results with use of the models used In the SPEAR-BETA and FEMAXI-IV codes. Results obtained with use of the present modified model showed better agreement with experimental data reported in the literature than those results with use of the latter codes. The fuel centerline temperature calculated with introduction of effective thermal conductivity for centerline temperature calculated with Introduction of effective thermal conductivity for cracked fuel was 200 higher fission gas release predicted with use of the modified model was nearly 6% larger on the average than that calculated by use of the unmodified model used in the SPEAR-BETA code.e SPEAR-BETA code.e.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.24 no.5
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• pp.513-520
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• 2011

In this paper, the advanced explicit algorithm is proposed to simulate the stress-erection process analysis of Strarch system. The Strarch(Stressed-Arch) system is a unique and innovative structural system and member prestress comprising prefabricated plane truss frames which are erected by a post-tensioning stress-erection procedure. The flexible bottom chord which have sleeve and gap detail are closed by the reaction force of prestressing tendon. The prestress imposing to the tendon will make the Strarch system to be erected. This post tensioning process is called as "stress-erection process". During the stress-erection process, the plastic rigid body rotation is occurred to the flexible top chord by the excessive amount of plastic strain, and the structural characteristic becomes to be unstable. In this study, the large deformational beam-column element with plastic hinge is used to model the flexible top chord, and the advanced Dynamic Relaxation method(DRM) are applied to the unstable problem of stress-erection process of Strarch system. Finally, the verification of proposed explicit algorithm is evaluated by analysing the stress-erection of real project of Strarch system.

• Journal of Korean Society of Steel Construction
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• v.23 no.4
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• pp.429-438
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• 2011

In this study, the explicit numerical algorithm was proposed to simulate the stress erection process and ultimate-load analysis of the strarch (stressed arch) system. The strarch system is a unique and innovative structural system and member prestress comprising prefabricated plane truss frames erected through a post-tensioning stress erection procedure. The flexible bottom chord, which has sleeve and gap details, is closed by the reaction force of the prestressing tendon. The prestress imposed on the tendon will enable the strarch system to be erected. This post-tensioning process is called "stress erection process." During this process, plastic rigid-body rotation occurs to the flexible top chord due to the excessive amount of plastic strain, and the structural characteristic is unstable. In this study, the dynamic relaxation method (DRM) was adopted to calculate the nonlinear equilibrium equation of the system, and a displacement-based finite-element-formulated filament beam element was used to simulate the nonlinear behavior of the top chord sections of the strarch system. The section of the filament beam element was composed by the amount of filaments, which can be modeled by various material models. The Ramberg-Osgood and bilinear kinematic elastic plastic material models were formulated for the nonlinear material behaviors of the filaments. The numerical results that were obtained in the present study were compared with the experiment results of the stress erection and with the results of the ultimate-load analysis of the strarch unit frame. The results of the present studies are in good agreement with the previous experiment results, and the explicit DRM enabled the analysis of the post-buckling behaviors of the strarch unit frame.

• Proceedings of the Materials Research Society of Korea Conference
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• 1994.11a
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• pp.97-97
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• 1994

Wide gap 반도체 중 하나인 GaN 에너지갭이 실온에서 3.4eV 이고 직접천이형 에너지대 구조를 가지므로 청색 및 자외영역의 파장을 발광하는 발광다이오드와 바도체 레이저 다이오드의 제작에유용한 재료이다. GaN계 III족 질화물반도체가 다파장용 광원으로서 유망함을 보인 것은 1970년대 초방의기초적 연구이다. 이로부터 약 25년이 경고한 현재 청색발광다이오드가 실용화당계에 이르게 되었지만 아직까지 전류주입에 의한 레이저발진은 보고되고있지 않다. 이 논문에서는 ALGaN/GaN이중이종접합(DH) 구조의 광여기에 의한 유도방출과 광학적 이득을 측정하므로서 전류주입에의한 레이저발진의 가능성을 조사하였다. 유기금속기상에피텍셜(MOVPE)법으로 성장한 ALGaN/GaN DH구조의 표면에 수직으로 펄스발진 질소레이저(파장:337.1nm, 주기:10Hz, 폭: 8nsec) 빔의 공출력밀도를 변화시키어 조사하고 시료의단면 혹은 표면으로부터 방출되는 광 스펙트럼을 측정하였다. 입상광밀도가 증가함에 따라 자연방출에 의한 발광피크보다 낮은 에너지에서 발광강도가 큰 유도방출에 의한 피크가 370nm의 파장에서 현저하게 나타났으며 실온에서 유동방출에 필요한 입사공밀도의 임계치는 약 89㎾/$\textrm{cm}^2$이었다. 이는 GaN 단독층에 대한 유동방출의 임계치 700㎾/$\textrm{cm}^2$ 에 비하여 약 1/8정도 낮은 것이며, 이를 전류밀도로 환산하면 약 27㎄/$\textrm{cm}^2$ 정도로서 전류주입에 의하여서도 레이저발진을 실현할 수 있는 현실적인 값이다. 한편 광여기 방법으로 측정한 광학적 이득은 입사광의 밀도가 각각 100㎾/$\textrm{cm}^2$과 200㎾/$\textrm{cm}^2$일 때 34$cm^{-1}$ / 과 160 $cm^{-1}$ / 이었다. 이와 같은 결과는 GaN의밴드단 부근의 파장영역에서 AIGaN 흔정의 굴절율이 GaN의 굴절율보다 작으므로 DH구조의 채택의 의한 광의 몰입이 가능하여 임계치가 저하된 것으로 여겨진다. 또한 광학적 이득의 존재는 이 구조에 의한 극단파장 반도체 레이저다이오드의 실현 가능성을 나타내는 것이다.