• 한국신재생에너지학회:학술대회논문집
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• 2006.06a
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• pp.315-318
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• 2006

포항풍력에너지연구소에서는 에너지 관리공단의 지원으로 2004년부터 풍력터빈 KBP-2000M에 사용될 발전기를 개발해 오고 있다. KBP-2000M에 사용되는 발전기는 기어비가 24인 기어박스를 가진 가변속도형식의 발전기이다. 발전기의 직경은 1.87m 이고 축 방향의 길이는 1.288m 로 영구자석을 사용하여 여자하는 형식으로 설계되었다. 이러한 설계는 풍력발전기에서 요구하는 주요 요구조건인 고효율, 고 신뢰성을 만족시키기 위해서 매우 중요하다 이 보고에서는 발전기의 물리설계에서 얻어진 사양을 기준으로 하여 열 해석에서 얻어진 열 손실을 이용하여 냉각시스템 설계를 하였으며 펌프 및 라디에이터 선정에 관해서 논의한다.

• Transactions of the Korean Society for Noise and Vibration Engineering
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• v.18 no.1
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• pp.80-86
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• 2008

In this study. the noise sources were identified and the noise and vibration were reduced for an industrial forklift. To identify the noise sourses, noise signals were measured by a microphone on a driver seat and these signals were analyzed with a waterfall plot. For this purpose, the gear mesh frequencies from the gear box of a reducer were not only investigated but noise/vibration sourses of an electric motor were also examined. Furthermore, the frequency response functions were obtained to confirm the vibration and noise sourses. It was found that severe vibration and noise were generated in the casing and the connecting part of the reducer. The severe vibration and noise could be reduced by a structure modification.

• Journal of the Korean Vacuum Society
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• v.18 no.2
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• pp.79-84
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• 2009

The electron emission source of triode type has been fabricated using CNT paste. The nano Ag particle and photosensitive polymers were added to the CNT paste. The surface roughness of the CNT emitter was uniform by the back exposure method. The added nano Ag particle improves the adhesion and the electric conductance with small variation in the CNTs and between electrode. After the aging with heat-exhausting, the reliability of the triode CNT electron source was secured in the high voltage and current operation for 12 hours. At this time, the gate leakage current was about 10 % less than.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.2
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• pp.1-7
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• 2016

Although the second driving device of KTX, which consists of the wheel and the axle reduction gears unit, is a mechanically integrated structure, its preventive maintenance (PM) requires two separate intervals due to the different technical requirements. In particular, these subsystems perform attaching and detaching work simultaneously according to the maintenance directive. Therefore, to reduce the unnecessary amount of PM and high logistic availability of the train, it is important to optimize PM with regard to reliability-centered maintenance toward a cost-effective solution. In this study, fault tree analysis and reliability of the subsystems, considering the criticality of the components, were performed using the data derived from field data in maintenance. The cost optimization of the PM was derived from a genetic algorithm considering the target reliability and improvement factor. The cost optimization was derived from a maximum of the fitness function of the individual in generation. The optimal TBO of them using the genetic algorithm was 2.85x106 km, which is reduced to approximately 21% compared to the conventional method.

• Tribology and Lubricants
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• v.31 no.4
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• pp.141-147
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• 2015

Gas foil thrust bearings (GFTBs) have attractive advantages over rolling element bearings and oil film thrust bearings, such as oil-free operation, high speed stability, and high-temperature operation. However, GFTBs have lower load carrying capacity than the other two types of bearings owing to the inherent low gas viscosity. The load carrying capacity of GFTBs depends mainly on the compliance of the foil structure and the formed hydrodynamic wedge, where the gas pressure field is generated between the top foil and the thrust runner. The load carrying capacity of the GFTBs is very important for the suitable design of oil-free turbomachinery with high performance. The aim of the present study is to identify the characteristics of the load carrying performance of GFTBs. A new test rig for the experimental measurements is designed to provide static loads up to 800 N using a pneumatic cylinder. The maximum operating speed of the driving motor is 30,000 rpm. A series of experimental tests—lift-off test, static load performance test, and maximum load capacity test—estimate the performance of a six-pad GFTB, in terms of the static load, driving torque, and temperature. The maximum load capacity is determined by increasing the static load until the driving torque rises suddenly with a sharp peak. The test results show that the torque and temperature increase linearly with the static load. The estimated maximum load capacity per unit area is approximately 80.5 kPa at a rotor speed of 25,000 rpm. The test results can be used as a design guideline for GFTBs for realizing oil-free turbomachinery.

• Proceedings of the Korean Vacuum Society Conference
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• 2013.08a
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• pp.263.1-263.1
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• 2013

탄소나노튜브(CNT)를 이용한 초소형 X선 튜브는 근접 암치료, 비파괴 X선 영상 장치, 휴대용 X선 분광계 등에서 X선 발생소스로 많이 연구되고 있다. 2극형 CNT 에미터의 경우 구조가 단순하여 초소형 X선 튜브에 쉽게 장착할 수 있지만 아노드의 전압과 전류가 연동되기 때문에 튜브의 조작성이 제한적이다. 3극형은 상대적으로 복잡한 구조이고, CNT에서 방출된 전자가 게이트 전극으로 흐르는 누설 전류 그리고 절연체와 충돌하여 차징을 발생시킬 수 있기 때문에 직경이 좁은 초소형 X선 튜브에 구현하기가 쉽지 않다. 하지만 초소형 X선 튜브를 다양한 X선 장치에 응용하기 위해서는 아노드 전압과 전류의 독립된 조작이 가능한 3극형 CNT 에미터가 반드시 구현되어야 한다. 본 발표에서는 전자빔의 아노드 집속을 강화하고 절연체에서의 차징을 줄이는 포커싱 기능의 게이트(FFG) 구조를 제안하였고. 이를 적용하여 초소형 X선 튜브들을 제작하고, 분석하였다. FFG 구조가 성공적으로 적용된 초소형 X선 튜브는 게이트 누설 전류 없이 뛰어난 전류 및 X선 방출 특성을 보였다. 이와는 달리, 몇몇 초소형 X선 튜브들에서는 게이트 누설 전류가 나타났고, 아노드 전압에 의한 게이트 전압 상승이 발생하여 불안정한 구동 특성을 보였다. 초소형 X선 튜브를 밀봉하지 않고 진공 챔버에서 실험한 결과, 유도된 게이트 전압은 상당한 시간이 흐르거나 진공챔버에 공기를 주입하고 다시 진공상태로 만들면 유도전압이 제거되는 것을 볼 수 있었다. 결론적으로 CNT에서 방출된 전자빔이 정상궤도를 벗어나 게이트 누설전류와 차징에 의한 게이트 유도전압을 발생시키면 초소형 X선 튜브가 불안정한 구동을 하고, 결국 튜브의 심각한 결함으로 나타나게 된다. 즉, 게이트 누설 전류와 유도된 게이트 전압은 3극형 CNT 에미터가 장착된 초소형 X선 튜브의 디자인과 제작에 있어서 성공 기준이 될 수 있다.

• Journal of the Korean Society of Propulsion Engineers
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• v.23 no.3
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• pp.28-34
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• 2019

The thrust control calculation according to the operation of plug nozzle for cold air test and the analysis of the flow characteristics of the pintle shape and operation pressure are performed. The numerical computation was verified by comparing the flow structure and the coefficient of thrust with the experimental data. It was confirmed that the nozzle throat was formed at the design position on each pintle shape, and thrust control up to 1:8 was achieved only by the stroke change. Finally, although the aerospike nozzle is autonomous, it is unfavorable in the under_expansion condition, if it is designed for a very low nozzle pressure ratio.

• Proceedings of the Korean Institute of Electrical and Electronic Material Engineers Conference
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• 2000.04a
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• pp.152-154
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• 2000

Electro_optical characteristics in AC-PDP are confined by a lots of parameters. especially driving pulse shape is very important to improve AC-PDP's luminosity and efficiency. In that experiment measure the luminosity, IR(Infra Red) peak value and response time as the increase of 1st, 2rd sustain pulse width. The VDS(Versatile Driving Simulator -developed by kwangwoon university-) was used to make driving pulse shape. It is found that IR response time after displacement current, Luminosity and IR peak value are changed on account of 1st,2rd sustain pulse width.

• 한국신재생에너지학회:학술대회논문집
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• 2005.11a
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• pp.706-710
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• 2005

포항공과대학교의 포항풍력에너지연구센터(PoWER Center)가 개발에 참여했던 750 kW급 직접구동형 국산화 풍력발전 시스템(KBP-750D)은 그 개발이 완료 단계에 이르러 설치를 준비하고 있으며 현재 KBP-750D의 상용화를 추진하기 위한 출력성능 및 하중 측정을 통한 실증연구가 진행되고 있다. IEC 61400-13의 규격을 기준으로 수행되는 하중 측정은 수개월간 지속되는 측정을 통한 방대한 하중 데이터 수집 과정과 데이터 검증, 데이터 분류, 시계열 해석, 하중 통계 해석, 주파수 분석, 하중 스펙트럼 해석과 등가하중 해석의 측정 데이터 처리 과정으로 구성된다. 본 연구에서는 하중 측정 데이터를 처리 해석함에 있어서 성력화를 도모하고 정확하면서도 객관적인 성능평가 자료를 확보하기 위하여, 하중 측정에 대한 전용 해석 프로그램의 개발을 추진하였다. 본 논문에서는 하중 측정 데이터에 대한 처리 및 해석 과정을 소개하고 해석 프로그램의 개발 과정 및 수행 결과를 보고한다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.12 no.6
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• pp.2707-2712
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• 2011

In this paper, a power factor correction (PFC) control circuit using single stage boundary conduction mode(BCM) for the 400V. 120W LED drive application has been designed. The proposed control circuit is aimed for improvement of the power factor correction and reduction of the total harmonic distortion. In this circuit, a new CMOS multiplier structure is used instead of a conventional BJT(bipolar junction transistor) based multiplier where has a relatively large area. The CMOS multiplier can bring 30 % reduced chip area, competitive die cost in comparison with the conventional BJT multiplier.