• 한국신재생에너지학회:학술대회논문집
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• 한국신재생에너지학회 2010년도 추계학술대회 초록집
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• pp.129.2-129.2
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• 2010

As a part of the government renewable energy policy, KOWEPO is constructing 300MW IGCC plant in Taean. IGCC plant consists of gasification block, air separation unit and power block, which performance test is separately conducted. Overall performance test for IGCC plant is peformed to comply with ASME PTC 46. Major factors affected on the overall efficiency for IGCC plant are external conditions, each block performance(gasification, ASU, power block), water/steam integration and air integration. Performance parameters of IGCC plant are cold gas efficiency, oxygen consumption, sensible heat recovery of syngas cooler for gasification block and purity of oxygen, flow amount of oxygen and nitrogen, power consumption for air separation unit and steam/water integration among the each block. The gas turbine capacity applied to the IGCC plant is 20 percent higher than NGCC gas turbine due to the low caloric heating value of syngas, therefor it is possible to utilize air integration between gas turbine and air separation unit to improve overall efficiency of the IGCC plant and there is a little impact on the ambient condition. It is very important to optimize the air integration design with consideration to the optimized integration ratio and the reliable operation. Optimized steam/water integration between power block and gasification block can improve overall efficiency of IGCC plant where the optimized heat recovery from gasification block should be considered. Finally, It is possibile to achieve the target efficiency above 42 percent(HHV, Net) for 300MW Taean IGCC plant by optimized design and integration.

• 한국초전도ㆍ저온공학회논문지
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• 제14권3호
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• pp.43-47
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• 2012

A linear compressor generates pulsating pressure and oscillating flow in a cryocooler such as Stirling cryocooler and pulse tube refrigerator. It is driven by AC power source and designed to operate at resonance of piston motion. The driving voltage level is determined by electric parameters of resistance, inductance and thrust constant of linear motor. From voltage equation on linear motor, the power factor of driving power is inherently less than 1. The phase difference between voltage and current of supplied power can be zero using capacitor and this can minimize a supply voltage level. Especially, the linear compressor of kW class requires high voltage and thus can cause a difficulty in selecting power supply unit due to limitation of voltage level. The capacitor in driving electric circuit is useful to settle this problem. In this study, the electric circuit of linear compressor is analytically investigated with assumption of mechanical resonance. The electric parameters of commercial linear motor are used in the analysis. The effects of capacitor on driving voltage level and power factor are investigated. From analytic results, it is shown that the voltage level can be mimized with using capacitor in driving electric circuit.

• 대한전기학회:학술대회논문집
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• 대한전기학회 1994년도 하계학술대회 논문집 A
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• pp.419-421
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• 1994

A CRU (Customer Remote Unit) for KODAS(Korea Distribution Automatic System) is presented in the paper. This equipment works as a terminal unit for the Load Control and the AMR(Automatic Meter Reading). It is composed of control, drive, input, display, and communication parts. A CRU calculates and memorizes the active power, time-of-use, and demand by the pulse from watthour meter for AMR. It also transfers the data to Center Control System. It can measure current, voltage, and power factor by adding the simple circuit. For load control, It receives the necessary informations such as the load control periods, modes, and time intervals. It controls the load until the stopping commad comes. The system reliability has been proved using a prototype.

• 한국항행학회논문지
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• 제26권2호
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• pp.99-104
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• 2022

최근 국내에서도 항공기 플랫폼을 기반으로 한 무기체계 수요는 점진적으로 증가 추세이다. 특히 지상 요격 용도로 항공기에 장착되어 발사 후 수백 킬로미터를 순항한 뒤 표적에 침투하는 유도탄의 수요가 높지만 개발 초기단계이며 그에 따른 연구와 자료 역시 제한적이다. 본 논문은 항공기 플랫폼에 장착 할 공대지 유도탄의 전력변환장치(PCU)에 대한 연구이며 항공기와 유도탄 간 인터페이스인 MIL-STD-1760 기반, 배꼽 연결기의 특성과 구조 그리고 항공기와 전기적 연동 체계에 대해 확인한다. 또한 주요 기능인 유도탄 구성품에 전원을 공급해주는 전력변환장치 설계 사양을 언급하였고, 항공기 장착 상태에서 유도탄 전원 입력 조건이 되는 3상 교류 입력을 모의하여 PFC를 이용한 정류 방식과 브릿지 정류회로를 이용한 정류 방식 결과를 비교 하였다. 이는 추후 개발 될 항공기 장착 무기 체계의 전력변환장치 설계 기초 자료로 사용 될 수 있을 것이다.

• 전력전자학회논문지
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• 제6권2호
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• pp.217-221
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• 2001

본 논문에서는 통신기기와 같은 저용량 부하를 위한 APLC를 설계하였다. APLC는 부하와 병렬로 위치하여 부하에 필요한 무효전력 성분만을 공급함으로 운전 효율을 향상시켰으며 히스테리스 제어기를 마이크로 프로세서와 아날로그 회로를 이용하여 구현하여 저가형 제어기를 구현하였다. 컴퓨터 시뮬레이션을 통해서 보상 시스템의 특성을 해석하였으며 또한 실험에 의해 제안된 APLC제어기가 고조파 저감 및 역률 개선을 수행하고 있음을 확인하였다.

• 한국정보통신학회:학술대회논문집
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• 한국해양정보통신학회 2006년도 춘계종합학술대회
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• pp.685-688
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• 2006

본 논문에서는 초전도에너지저장 시스템에 적합한 간략한 회로 구성과 높은 신뢰성을 가지는 단상 무정전 전원공급장치를 제안한다. 제안된 시스템은 공통암 방식을 적용하여 스위칭 소자수를 저감한다. Normal, Stored-energy, Bypass의 세 가지 동작 모드에 대하여 상세히 설명한다. 사용되는 스위칭 소자수를 저감시키거나 수동소자로 대체시킬 경우 제어가 복잡해지고 자유도를 감소키는 문제점이 있지만 고성능의 디지털 제어기를 통해 추가적인 부담 없이 해결할 수 있다. 제안된 시스템의 타당성 검증을 위해 시뮬레이션 결과를 제시한다.

• Nuclear Engineering and Technology
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• 제8권2호
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• pp.101-116
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• 1976

고리 1호기 및 2호기 원자로의 발전단가에 대한 해석을 시도했다. 해석의 편의상 발전단가를 우선 건설, 운전 및 관리, 운전자금 및 핵연로 등에 관련된 비용성분으로 나누고, 이 중 첫 세성분에 대한 cost는 POWERCO-50 계산코오드를, 그리고 핵연료 비는 MITCOST-II를 써서 계산했다. 중요한 계산결과로서는 다른 세가지 핵연료 주기에 대한 고리 2획의 핵연료 주기비, 고리 1호 및 2호기의 발전단가 및 발전단가계산에 사용된 코스트 자료의 변화에 따른 발전단가의 민감도 등이다. 제래식 화력발전단가와 비교함으로써 원자력발전이 보다 경제적으로 유리하다는 사실을 알아내었지만 고리 2 호기의 건설비가 다른 PWR 발전에 비해 다소 고가임을 지적했다. 때문에 원자력발전을 유리하게 하기 위해서는 장차 도입될 원자력발전로의 경우 고리 2호기와 같은 turnkey 계약이 지양되어야 함을 지적했다. 또한 발전단가가 발전소 가동율의 변화에 따라 민감하게 변동한다는 사실로부터 발전소를 최대한 가동시킬 수 있도록 노력이 경주되어야 한다고 결론을 내렸다.

• 한국신뢰성학회지:신뢰성응용연구
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• 제15권3호
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• pp.139-144
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• 2015

Track drive unit adopted in the small sized excavator generally have been used in the construction equipment under the 10 tons as the driving device with forwarding and reversing of excavator. It is required to study the accelerated life test applied by over torque and speed to test the durability life test reflected the many driving modes of small sized excavator and also need to equip the comprehensive performance and life test equipments to do the various performance tests. This study had analyzed the failure modes of the components, and calculated the equivalent loads investigated the used loads in the real field conditions and elicits the acceleration factor adopted in the inverse power model. Also, this study have considered the changes of the acceleration factor and the durability test time in the case of the rotary group and the bearing through analyzing the main failure modes. It was calculated the no failure test time about 2 samples and confidence level 90% and elicited the accelerated life time 720 hours.

• 유공압시스템학회논문집
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• 제2권2호
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• pp.1-7
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• 2005

For the reliability evaluation of the track drive unit(TDU), firstly, we analyzed the major failure modes through FMEA(failure mode & effects analysis), FTA(failure tree analysis), and 2-stage QFD(quality function deployment), and then quantitatively determined the priority order of test items. The Minitab analysis was also performed for prediction of life distribution and parameters of TDU by use of field failure data collected from 430 excavators for two years. In addition, we converted the fluctuation load in field conditions into the equivalent load, and for evaluation of the accelerated lift by the cumulative fatigues, the equivalent load is again divided into the fluctuation load by reference of test time. And then, by use of the test method in this paper, the acceleration factor(AF) of needle bearing inside planetary gear which is the most weakly designed part of TDU is achieved as 5.3. This paper presents the quantitative selection method of test items for reliability evaluation, the determination method of the accelerated life test time, and the method of non-failure test time based on a few of samples. And, we proved the propriety of the proposed methods by experiments using a TDU for a 30 ton excavator.

• 제어로봇시스템학회논문지
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• 제13권2호
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• pp.154-162
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• 2007

In this paper, we propose a new AC-DC converter control method to comply with harmonics regulation(IEC 61000-3) effective for the inverter system of an air conditioner whose power consumption is less than 2,500W. There are many different ways of AC-DC converter control, but this paper focuses on the converter control method that is adopting an input reactor with low cost silicon steel core to strengthen cost competitiveness of the manufacturer. The proposed control method controls input current every half cycle of the line frequency to get unit power factor and at the same time to reduce switching loss of devices and acoustic noise from reactor. This kind of converter is known as a Partial Switching Converter(PSC). In this study, theoretical analysis of the PSC has been performed using Matlab/Simulink while a 16-bit micro-processor based converter has been used to perform the experimental analysis. In the theoretical analysis, electrical circuit models and equations of the PSC are derived and simulated. In the experiments, micro-processor controls input current to keep the power factor above 0.95 by reducing the phase difference between input voltage and current and at the same time to maintain a reference DC-link voltage against voltage drop which depends on DC-link load. Therefore it becomes possible to comply with harmonic regulations while the power factor is maximized by optimizing the time of current flow through the input reactor for every half cycle of line frequency.