• Composites Research
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• v.26 no.4
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• pp.207-212
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• 2013

In this study, the thickness optimization for uni-directional (UD) glass fiber reinforced polymer (GFRP) laminates of the spar cap of composite tidal blades was performed under the tip deflection constrains. The spar cap was composed of GFRP composites and carbon fiber reinforced polymer (CFRP) composites. The stress distributions in the blade as well as its material costs for the optimized results were additionally investigated. The optimized thickness was obtained by interacting a sequential quadratic programming (SQP) algorithm and an ABAQUS software to calculate an objective function. It was confirmed that the thickness of UD GFRP increased with a decrease of the restrained tip deflection when a thickness of UD CFRP laminates was constrained to 9 mm. The weight of the optimized spar-cap increased up to 96.2% while the maximum longitudinal tensile stress decreased up to 24.6%. The thickness of UD GFRP laminates increased with a decrease of the thickness of UD CFRP laminates when the tip deflection was constrained to 126.83 mm. The weight increased up to 40.1%, but the material cost decreased up to 16.97%. Finally, the relationships among the weight, internal tensile stress, and material costs were presented based on the optimized thicknesses of the spar cap.

• Journal of Aerospace System Engineering
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• v.12 no.2
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• pp.66-75
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• 2018

In this paper, a lightweight design of the spar cap of 2MW wind turbine blade was carried out using the ply reduction ratio (PRR) and CFRP with a trade-off study. The spar cap is one of the most critical factor in determining the mechanical performance of the blade. Tsai-Wu and Puck fracture theory were used to determine the fracture. As a result, the CFRP composite material could be lighter in terms of weight by about 30% than GFRP composite material under the same conditions. Based on the analytical results, we derive the optimal value of the laminate thickness of the composite material and present the structural performance improvement and the lightweight design result.

• Korean Journal of Air-Conditioning and Refrigeration Engineering
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• v.29 no.10
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• pp.504-514
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• 2017

The insulation performance of aircaps has been recognized and various studies regarding the aircap as a solution to increased building energy consumption are being carried out. However, the aircap is not durable and therefore it cannot play the role of an independent finishing material. Accordingly, the purpose of this study is to suggest an aircap wall module with improved durability through the lamination of the aircap and verify its effectiveness by evaluating its energy saving performance for lighting and air conditioning through a full-scale testbed. The conclusions of this study are as follows. 1) The aircap wall module featuring a laminated aircap that is being proposed in this study can save lighting energy due to the permeability of the aircap in comparison to previous insulating materials. 2) The aircap wall module with a laminated aircap is effective in improving heating and air-conditioning energy saving when it is more than 15 cm-thick during summer and winter in comparison to a 5 cm-thick prefabricated panel. 3) The aircap wall module featuring a laminated aircap is effective in improving lighting and heating and air-conditioning energy saving when it is 10 cm- and 5 cm-thick during summer and winter, respectively, in comparison to a 5 cm-thick prefabricated panel.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.24 no.8
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• pp.78-83
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• 2010

This paper describes the characteristic of tracking progress happened at the end of the polyvinyl chloride insulated cabtyre oval cord(VCTFK) that is widely used for distribution cord. Tracking is occurred owing to the drop of electrolyte at the end of the VCTFK. The tracking progress and its characteristic happened at the end of the VCTFK are as follow; Carbonization and electrical erosion are happened at the end of the VCTFK. Electrical erosion is begun at the insulation layer near conductors. After that, it is also happened at the sheath layer. Accumulation of carbonized insulation and sheath materials at the end of the VCTFK is begun after progress of electrical erosion. When the accumulation is progressed arc discharge is appeared and finally it goes to tracking breakdown.

• Journal of Wind Energy
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• v.5 no.1
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• pp.50-55
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• 2014

Surface Permanent-Magnetic-Synchronous-Generator (SPMSG) discussed in the present study has operational characteristics such as high rotational speed over 1,000 rpm and centrifugal force of 12 kN·m for each magnet. Structure-development analysis for the minimization of rotor-core weights and the maximization of thermal emission is performed by applying the aluminum-laminated cap which combines the advantages of IPM and SPM in order to overcome the difficulty that attaching the magnet to rotor-core only with an adhesive. In this study, the simulations in terms of structure and electromagnetic were performed with the variable parameters such as shape and thickness of laminated-cap and division method of magnet. As a result, condition for minimized centrifugal force with minimum loss is derived.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2009.06a
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• pp.73-73
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• 2009

트렌지스터의 채널 길이가 줄어듦에 따라 절연층으로 쓰이는 $SiO_2$의 두께는 얇아져야 한다. 이에 따라 얇아진 절연층에서 터널링이 발생하여 누설전류가 증가하게 되어 소자의 오동작을 유발한다. 절연층에서의 터널링을 줄여주기 위해서는 High-K와 같은 유전율이 높은 물질을 이용하여 절연층의 두께를 높여주어야 한다. 최근에 각광 받고 있는 High-K의 대표적인 물질은 $HfO_2$, $ZrO_2$와 $Al_2O_3$등이 있다. $HfO_2$, $ZrO_2$와 $Al_2O_3$는 $SiO_2$보다 유전상 수는 높지만 밴드갭 에너지, 열역학적 안정성, 재결정 온도와 같은 특성 면에서 $SiO_2$를 완전히 대체하기는 어려운 실정이다. 최근 연구에 따르면 기존의 High-K물질에 금속을 첨가한 금속산화물의 경우 밴드갭 에너지, 열역학적 안정성, 재결정 온도의 특성이 향상되었다는 결과가 있다. 이 금속 산화물 중 $HfAlO_3$가 대표적이다. $HfAlO_3$는 유전상수 18.2, 밴드캡 에너지 6.5 eV, 재결정 온도 $900\;^{\circ}C$이고 열역학적 안전성이 개선되었다. 게이트 절연층으로 사용될 수 있는 $HfAlO_3$는 전극과 기판사이에 적층구조를 이루고 있어, 이방성 식각인 건식 식각에 대한 연구가 필요하다. 본 연구는 $BCl_3$/Ar 유도결합 플라즈마를 이용하여 $HfAlO_3$ 박막의 식각 특성을 알아보았다. RF Power 700 W, DC-bias -150 V, 공정압력 15 mTorr, 기판온도 $40\;^{\circ}C$를 기본 조건으로 하여, $BCl_3$/Ar 가스비율, RF Power, DC-bias 전압, 공정압력에 의한 식각율 조건과 마스크물질과의 선택비를 알아보았다. 플라즈마 분석은 Optical 이용하여 진행하였고, 식각 후 표면의 화학적 구조는 X-ray Photoelectron Spectroscoopy(XPS) 분석을 통하여 알아보았다.