• Journal of the Korean Society of Propulsion Engineers
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• v.20 no.4
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• pp.94-103
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• 2016

A regeneratively-cooled channel in a liquid rocket engine is used to effectively cool a combustion chamber inner wall from hot combustion gas, and the heat transfer/pressure loss characteristics should be predicted in advance to design cooling channels. In the present research, five cooling channels with different geometric dimensions were designed and the channels were respectively manufactured using cutter and endmill. By changing coolant velocity and downstream pressure, the effects of manufacturing method, channel shape, and flow condition on pressure losses were experimentally investigated and the results were compared with the analytical results. At same channel shape and flow condition, the pressure loss in the channel machined by the cutter was lower than that by the endmill. It was also found that the pressure loss ratio between the experimental result and the analytical data changed with the channel shape and flow condition.

• Korean Journal of Materials Research
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• v.6 no.1
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• pp.40-48
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• 1996

고주파 저손실 재질로 사용되고 있는 Mn-Zn 페라이트의 제조공정 중 소결조건과 Ta2O5첨가가 Mn-Zn 페라이트의전력손실에 미치는 영향에 대해서 연구하였다. 등조성선을 따라 냉각하기 위하여 컴퓨터를 사용해서 정확하게 산소분압을 조절하였으며 적절한 등조성선을 선택함으로써 보다 좋은 손실특성을 얻을 수 있었다. CaO-SiO2 첨가계에 Ta2O5를 0ppm에서 400ppm으로 변화시켜 가며 첨가하였으며, Ta2O5 가 400ppm 첨가되었을 경우 균일한 grain 성장과 더불어 낮은 전력손실을 나타내었다. 온도에 상응하는 상평형 산소분압을 정확히 맞춰 냉각할 경우 전력손실 최소값이 질소 분위기에서 냉각시킨 시편보다 높은 온도쪽으로 이동됨도 확인할 수 있었다.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2014.10a
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• pp.973-974
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• 2014

대형 전동기의 주요 소음원은 전자기 소음과 냉각/통풍 시스템 소음이며, 이 중 냉각/통풍 시스템이 전체 소음에 큰 영향을 미친다. 본 논문에서는 대형 전동기의 저소음 냉각/통풍 시스템 개발을 위해 저소음 냉각 팬을 개발하고 팬 커버 내부의 유로를 개선하였다. 유동해석은 상용 CFD 소프트웨어를 이용하였으며 팬 커버 내의 scroll 형상 및 air guide, baffle 의 유무에 따라 팬 커버의 압력손실을 계산하였다. 해석을 통해 팬 커버 내부의 난류 유동과 압력손실이 가장 작은 팬 커버 형상을 도출하였으며 개선된 냉각/통풍 시스템이 기존 냉각/통풍 시스템보다 6.5dB 감소된 것을 확인하였다.

• JOURNAL OF ELECTRICAL WORLD
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• s.309
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• pp.83-87
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• 2002

전력계통에서의 발전, 송변전, 배전의 각각에 대한 에너지절약 및 이용 합리화를 미쓰비시(삼릉)전기는 여러 방면에서 노력하고 있으며, 여기서는 전력기기에 대한 그간의 노력에 대하여 기술한다. 발전에 관해서는 공기냉각과 수소냉각 터빈발전기의 효율 향상으로 성(省)에너지화를 지향하고 있다. 동사에서는 세계 최대급의 공기냉각 터빈발전기를 제작하여 수소냉각기와 거의 동등한 높은 효율을 얻고 있다. 송변전에 대해서는 전력용 대형 변압기의 본체 체적 축소, 신(新)절연구조의 채용으로 대형변압기의 설치면적을 반감시키고 손실저감도 실현시킬 수 있었다. 성숙기종으로 생각되는 분야에 대해서도 새로운 발상으로 더욱 개선해 나갈 계획이다. 배전분야에 대해서는 전력의 합리적 사용이나 고효율 변압기의 채용에 의한 전력삭감 등 필요성이 재검토되고 있다. 동사에서는 배전설비 구성의 일익을 담당하는 손실이 극히 적은 수퍼 고효율 유입변압기를 개발, 배전분야에서 활용되고 있다. 성(省)에너지를 위한 발전기의 응용 예의 하나로 자연에너지를 이용하는 풍력발전을 들 수 있다. 동사가 개발하여 실용화되고 있는 풍력발전기는 회전자 자극(磁極)에 영구자석을 사용한 동기발전기를 사용하고 있어, 여자장치나 기어기구가 불필요하여 전기적, 기계적인 손실을 경감시키고 있다.

• Journal of the Korean Society of Propulsion Engineers
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• v.22 no.2
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• pp.87-95
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• 2018

The pressure loss in a cooling channel was investigated by conducting a numerical analysis, which was performed with a different channel angle in the axial direction, velocity of flow, and diameter of channels. The pressure loss did not change much with respect to the different channel angle. However, the pressure loss tended to decrease if the diameter of the channel increased and the velocity of the flow decreased. The results were quantified by a nondimensional method and compared to an existing experimental equation to validate them. The data obtained by this study would be helpful in the design process of a cooling channel considering the pressure loss.

• Journal of the Korean Society of Propulsion Engineers
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• v.26 no.2
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• pp.72-78
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• 2022

A vacuum brazed cooling passage for an aircraft engine controller was designed. In order to predict the total pressure loss, which is the main design factor of the cooling passage, theoretical and numerical methods for the major loss and the minor loss considering the overall shape of the cooling passage are presented. This design and evaluation method can predict the pressure loss of the complex cooling passage shape for various flow conditions at the initial design step.

• Nuclear Engineering and Technology
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• v.26 no.2
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• pp.179-189
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• 1994

A performance of reactor coolant pump in two-phase flow is examined using the pump geometric conditions and the performance of the pump in single-phase flow. Wall friction loss of the reactor coolant pump in single-phase flow is prdicted using the Truckenbrodt boundary layer theory, and the head loss in two-phase flow is predicted with calculated well friction loss and separation loss coefficients. The analysis results are compared with the Combustion Engineering pump test data. The effect of two-phase multiplier on the peak clad temperature in Loss-of-Coolant Accident is also examined using the RELAP5 and the results indicate the importance of its accuracy.

• Journal of the Korean Magnetics Society
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• v.11 no.4
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• pp.173-178
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• 2001

The effects of heat-treatment with magnetic or non-magnetic field on magnetic properties of gas-atomized MPP dust cores subjected to various cooling processes after annealing were investigated. Upon magnetic-field annealing, ac permeability and core loss decreased with the increase of cooling rate, which were attributed to the generation of inhomogeneous internal stress and anomalous eddy current loss, respectively. It was not observed the formation of ordered phase and the related change in magnetic properties at the cooling stage for MPP dust cores. In MPP alloys, magnetic anisotropy was easily induced through the directional order, and permeability and core loss were changed under the conditions of low cooling rate and magnetic annealing.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.44 no.12
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• pp.1062-1070
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• 2016

The heat transfer and flow characteristics of gas turbine blade tip were investigated in this paper by using the conjugate heat transfer analysis. The rotor inlet boundary condition profile which was taken from the first stage nozzle outlet was used to analyse. The profile contained the velocity and temperature information. This study presents the influence of tip clearance about aerodynamic loss, heat transfer coefficient and film cooling effectiveness with the squealer tip designed blade model which tip clearance variation range from 1% to 2.5% of span. Results showed that the aerodynamic loss and the heat transfer coefficient were increased when the tip clearance was increased. Especially when the tip clearance was 2% of the span, the average heat transfer coefficient on the tip region was increased obviously. The film cooling effectiveness of tip region was increasing with decreasing of the tip clearance. There was high film cooling effectiveness at cavity and near tip hole region.

• The Journal of the Korea institute of electronic communication sciences
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• v.9 no.7
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• pp.799-804
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• 2014

To combine to the power transmission, photovoltaic inverter is demanded, because the photovoltaic system is generated direct current power. However, photovoltaic inverter is sensitive to high temperature. In the temperature rising such as at noon and on summer, efficiency of machine is decreased due to the loss increment. Because this problem causes national energy loss according to the expanding the photovoltaic industry, countermeasure is demanded. There, in this paper, we installed a cooling system using a thermoelement regardless of the temperature. Also, we analyze the cooling effect according to the position of two fans which improve the effect maximize.