• 설비공학논문집
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• 제23권11호
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• pp.733-740
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• 2011

To analyze the cooling performance in the refrigerator truck according to frost growth, the analytical model of refrigeration system was developed under frost and non-frost condition using EES. The system performance was analyzed with outdoor temperature, storage temperature, outdoor front air velocity and compressor speed in order to investigate the system performance characteristics with operating conditions. Besides, the system performance under frost condition was compared with that under non-frost condition. As a result, the frost thickness was 0.9 mm when the refrigerating capacity of frost condition was decreased by 30%. The maximum of the system COP was shown at compressor speed of 1500 rpm for non-frost and frost condition, simultaneously. The performance under frost condition was more sensitive to the operating condition compared to that under non-frost condition.

• 한국전기전자재료학회:학술대회논문집
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• 한국전기전자재료학회 2000년도 제2회 학술대회 논문집 일렉트렛트 및 응용기술전문연구회
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• pp.36-39
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• 2000

This paper presents the technology of condition diagnosis & life estimation on insulation system of the traction motor. In the non-destructive methods for diagnosis of coil insulation state, residual dielectric strength is estimated by the D-map which consist of the partial discharge quantity Q and average degradation degree $\Delta$. In the operating history of machine, the N-Y life estimation method is based on the stop-starting numbers and operating times with considering each degradation factor by the thermal, electrical and heat-cycle stress. With the on-line conditioning monitoring on the currents of traction motors, detecting the abnormal operating state due to bearing faults, stator or armature faults, eccentricity related faults and broken rotor bars can be performed.

• 항공우주시스템공학회지
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• 제2권2호
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• pp.42-45
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• 2008

Under the non-operating exposure condition in the hot area, the T-50 cockpit temperature is expected over the requirement according to T-50 environmental criteria. So it is necessary to protect the cockpit from the high temperature condition during the non-operating exposure because the high temperature of the cockpit may result in the cockpit equipment malfunction. In this study, the transparency coating is selected as the method for protecting the cockpit from the high temperature exposure and analyzed the effect on the cockpit heat load attenuation. Some kinds of cockpit coating were reviewed and selected and the analysis was performed about the effect before and after coating application under 1% hot day condition based on the T-50 FSD hot soaking test data. The result of analysis show transparency coating is so effective to attenuate the heat load of T-50 cockpit.

• 수산해양기술연구
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• 제49권2호
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• pp.136-143
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• 2013

The analysis of the written verdicts in recent five years was conducted to obtain preventive measures of collision between fishing vessel and non fishing vessel. As a result, a collision much happened in offshore trap for fishing vessel and below 5,000 tons of small and medium class for non fishing vessel. A person involved in a marine accident occupied 68% in sixth class deck officer and small boat operator for fishing vessel and 29% in third class deck officer for non fishing vessel. 90% of the collision happened in a underway by operating state and 84% in sight of one another by visibility state. The systemic radar training was required since 47% of the collisions was occurred on the condition of radar operation in fishing vessel. The main cause of poor lookout was a intensive fishing and poor lookout on movement by radar for fishing vessel and one man watch system and no recognition of one another by radar for non fishing vessel. This result is expected to contribute for the decrease of collision.

• Nuclear Engineering and Technology
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• 제45권2호
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• pp.203-210
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• 2013

The objective of this conducted research is to study the iodine removal efficiency in a self-priming venturi scrubber for submerged and non-submerged operating conditions experimentally and theoretically. The alkaline solution is used as an absorbent, which is prepared by dissolving sodium hydroxide (NaOH) and sodium thiosulphate ($Na2S_2O_3$) in water to remove the gaseous iodine ($I_2$) from the gas. Iodine removal efficiency is examined at various gas flow rates and inlet concentrations of iodine for submerged and non-submerged operating conditions. In the non-submerged venturi scrubber, only the droplets take part in iodine removal efficiency. However, in a submerged venturi scrubber condition, the iodine gas is absorbed from gas to droplets inside the venturi scrubber and from bubbles to surrounding liquid at the outlet of a venturi scrubber. Experimentally, it is observed that the iodine removal efficiency is greater in the submerged venturi scrubber as compare to a non-submerged venturi scrubber condition. The highest iodine removal efficiency of $0.99{\pm}0.001$ has been achieved in a submerged self-priming venturi scrubber condition. A mathematical correlation is used to predict the theoretical iodine removal efficiency in submerged and non-submerged conditions, and it is compared against the experimental results. The Wilkinson et al. correlation is used to predict the bubble diameter theoretically whereas the Nukiyama and Tanasawa correlation is used for droplet diameter. The mass transfer coefficient for the gas phase is calculated from the Steinberger and Treybal correlation. The calculated results for a submerged venturi scrubber agree well with experimental results but underpredicts in the case of the non-submerged venturi scrubber.

• 청정기술
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• 제20권3호
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• pp.298-305
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• 2014

석탄에 포함되어 있는 회분은 환경오염을 유발시킬 수 있으며, 고온에서 운전되는 발전 설비에 융착되어 열전달 효율을 저하시키는 문제점을 가지고 있다. 이러한 문제를 해결하기 위해서 알칼리나 산, 또는 유기 용매를 이용하여 석탄 내의 회분을 제거하기 위한 연구와 함께 무회분 석탄을 이용한 석탄화력 발전 및 석탄가스화 복합발전에 대한 타당성 연구가 활발히 진행 중이다. 따라서 본 연구에서는 200 ppm급 무회분 석탄을 석탄가스화 발전에 이용하기 위해서 필요한 가스화기 운전조건을 ASPEN $Plus^{(R)}$ 공정모사의 민감도 해석을 바탕으로 도출하였다. 특히 석탄가스화 공정은 열분해, 휘발분 연소, 촤 가스화 공정으로 나누어 해석을 진행하였으며, 1.5 톤일급 비용융(non-slagging) 가스화기의 크기 및 운전 조건을 반영하여 모델링 하였다.

• 유기물자원화
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• 제20권4호
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• pp.106-117
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• 2012

건조과정에서 시료의 순환과 낙하이동에 따른 건조효과를 평가하기 위하여 음식물류폐기물 8,000kg을 간접건조방식의 건조기에 투입하고 회전스크류 가동시와 미가동시에 대하여 수분함량, 건조율, 평균입자크기 및 입도분포, 증발수분량 및 건조효율을 비교하였다. 음식물류폐기물의 초기 수분함량은 77.1%로서, 회전스크류 가동시에는 가동 후 5시간 만에 수분함량이 14.4%로 낮아진 반면에 미가동시에는 16시간을 가동시켜도 수분함량 35.6%에 머물고 있어 시료의 순환과 낙하이동이 건조효과 상승에 영향을 미치고 있음을 알 수 있다. 건조시작 후 점성구간 도달 이전에는 입자크기가 증가하면서 수분증발률은 최대치를 보인다. 점성구간에서는 입자크기가 최대치를 나타내나 수분증발률은 급감하기 시작하며, 점성구간 이후에는 입자크기와 수분증발률이 동시에 감소하는 것으로 나타났다. 이는 자유수 증발량과 각 구간에서의 점성차이에 기인한 것으로 여겨진다. 평균 입자크기는 가동 후 지속적으로 증가하여 점성구간인 수분함량 70%-60% 범위에서 최대치를 보인 후 감소하는 경향을 나타내었으나 평균 입자크기의 변화정도는 회전스크류 가동방식에 따라 다르게 나타났다. 또한 회전스크류 가동시 입도분포는 25.0mm에서 0.25mm까지 폭넓게 분포하는 반면에 미가동시에는 25.0mm에서 3.56mm까지 의 좁은 입도분포와 25.0mm이상의 입자크기에 집중되고 있다. 회전스크류 가동으로 건조효율에 미치는 효과를 회전스크류 미가동시와 비교하면 시간당 증발수분량은 364%, DS(Dry Solid)당 증발수분량은 356%나 증가한 것으로 평가되었다.

• 에너지공학
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• 제12권1호
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• pp.11-16
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• 2003

지상 정적 상태에 있는 항공기내 연료온도의 변화가 유한차분식에 의하여 해석되었다. 수정 Dufort-Frankel 기법의 explicit 방법에 의해 수치계산이 수행되었다. 항공기는 지상 정적상태에서 1% hot day 대기조건에 따른 태양의 복사 및 바람의 속도와 함께 반복되는 일일주기의 공기온도에 노출되어 있다고 가정되었다. 항공기는 난류유동장내에 있는 것으로 가정되었다. 항공기 표면과 외부대기사이의 열전달을 계산하기 위하여 Eckert에 의해 제안된 평판위의 난류 열전달계수가 사용되었다. 본 해석에 사용된 지배방정식은 연료에 대한 에너지방정식이다. 본 해석으로부터, 주익탱크의 연료온도가 다른 탱크들 가운데 가장 높게 나타났으며 온도변화율 또한 가장 크게 나타났다. 본 온도해석에 대한 결과는 여러 비행임무에 있어서 항공기내의 연료온도 변화 해석을 위한 초기치로서 사용될 수 있다. 또한, 본 해석방법은 항공기 열에너지 관리시스템의 해석 및 설계에 사용될 수 있다.

• Korean Chemical Engineering Research
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• 제58권3호
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• pp.493-497
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• 2020

Hazardous area classification is designed to prevent chemical plant explosions in advance. Generally, the duration of the explosive atmosphere is used for zone type classification. Herein, IEC code, a quantitative zone type classification methodology, was used to achieve Zone 2 NE, which indicates a practical non-explosion condition. This study analyzed the operating pressure of a vessel handling propane to achieve Zone 2 NE by applying the IEC code via MATLAB. The resulting zone type and hazardous area grades were compared with the results from other design standards, namely API and EI codes. According to the IEC code, the operating pressure of vessels handling propane should be between 101325-116560.59 Pa. In contrast, the zone type classification criteria used by API and EI codes are abstract. Therefore, since these codes could interpret excessively explosive atmospheres, care is required while using them for hazardous area classification design.

• International Journal of Fluid Machinery and Systems
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• 제4권2호
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• pp.243-254
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• 2011

In the present paper, we focus on the flow computation of a low head Propeller turbine at a wide range of design and off-design operating conditions. First, we will present the results on the efficiency hill chart prediction of the Propeller turbine and discuss the consequences of using non-homologous blade geometries for the CFD simulation. The flow characteristics of the entire turbine will be also investigated and compared with experimental data at different measurement planes. Two operating conditions are selected, the first one at the best efficiency point and the second one at part load condition. At the same time, for the same selected operating points, the numerical results for the entire turbine simulation will be compared with flow simulation with our standard stage calculation approach which includes only guide vane, runner and draft tube geometries.