• Tribology and Lubricants
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• 제24권3호
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• pp.140-146
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• 2008

The floating ring seal which is used in the high pressure turbo pump is frequently used in the oxidizer pump and the fuel pump of the turbo pump of the liquid propulsion rocket, because it is able to minimize clearance to decrease the leakage flow rate. But, the floating ring seal has a tendency to increase instability in decreasing eccentricity ratio. To complement this weakness, it is devised bump floating ring seal which is inserted bump in the outer surface. It has various experiment results. But the theoretical study of the bump floating ring seal didn't investigated yet. In this paper, we analyse about static characteristics of bump floating ring seal, compared previous experimental results. To analyze the characteristic of bump floating ring seal, we coupled perturbation method of floating ring seal and FEM of bump foil.

• Tribology and Lubricants
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• 제22권2호
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• pp.105-111
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• 2006

The floating ring seal which is used in the high pressure turbo pump is frequently used in the oxidizer pump and the fuel pump of the turbo pump of the liquid propulsion rocket, because it is able to minimize clearance to decrease the leakage flow rate. Compared with contact seal, the floating ring seal has advantage of minimizing clearance without rubbing phenomenon. But, the floating ring seal has a tendency to increase instability in operating condition in the high speed region. In this research, we devised floating ring seal which is inserted bump in the outer surface in order to improve the stability in the high speed region. Through this work, we expect to improve stability of floating ring seal with increasing the direct damping coefficient of seal and decreasing the eccentricity ratio.

• 한국가스학회지
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• 제18권4호
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• pp.13-20
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• 2014

상업용 천연가스 배급 시스템에서 천연가스의 공급압력은 압력조절밸브를 사용하여 제어하며 이때 막대한 압력에너지가 낭비된다. 이러한 폐압에너지는 터보 팽창기와 같은 터보기계를 사용하여 회수할 수 있으나 팽창과정에서 발생하는 Joule-Thompson 효과에 따라서 큰 온도강하가 발생한다. 터보 팽창기 전단 또는 후단에 보일러를 설치하여 영하의 온도를 방지할 수 있으며 또한 보일러를 대체하여 연료전지나 가스엔진의 폐열을 이용하여 천연가스를 예열할 수도 있으나 하이브리드 시스템의 구동을 위해 운영규모에 따라 일정량을 소모해야 한다. 이 연구에서는 천연가스가 가지고 있는 압력에너지를 활용하여 천연가스의 소모 없이 터보 팽창기와 연결된 히트펌프를 구동하여 천연가스를 예열하는 시스템을 제안하고 증발온도, 응축온도 및 작동유체의 변화에 따른 시스템의 열역학적 특성을 분석하였다. R717 냉매가 예상 작동범위 내에서 가장 높은 COP와 가장 낮은 압축일을 나타내 제안된 하이브리드 시스템에 적합함을 확인하였다. 보일러시스템과의 경제성 분석을 통해 천연가스를 LNG 형태로 수입하고 있는 국내의 경우 히트펌프 하이브리드 시스템이 경쟁력 있음을 확인하였다.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2004년도 제22회 춘계학술대회논문집
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• pp.234-239
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• 2004

In the development of rocket turbo-pump, cavitation at the inducer is one of the major problems. Cryogenic fluids are commonly used for rocket propellant, therefore, thermodynamic effect becomes noticeable compared to conventional water cavitation. In the present study, a numerical simulation method for cryogenic cavitation is proposed, which reveals the difference between cryogenic and water cavitation.

• Journal of Advanced Marine Engineering and Technology
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• 제32권3호
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• pp.421-429
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• 2008

Various kinds of ship are operated to transport cargo or passengers at sea in the world. Most of the important auxiliary machineries installed in those ships are fluid machineries such as pumps, compressors, and fans. A large percentage of fluid machinery is pumps which are classified turbo and positive displacement pumps. This paper analyzes only positive displacement pumps. This thesis has two aims: (a) to analyze the present status of pumps installed in merchant and training ships and (b) to find the correlation among sea going pump kW, port pump kW, total pump kW, GE kW, ME MCR, number of pumps, ME kgf, pump kgf. Based on ship's type, this paper seeks to find special characteristics as a result of analyzing head, flow rate, and kW. Moreover this paper analyzes and compares number of pumps, pump kW/ME MCR, pump kW/GE kW under the conditions of seagoing and berthing according to ship's type.

• 한국정보처리학회:학술대회논문집
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• 한국정보처리학회 2006년도 춘계학술발표대회
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• pp.399-402
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• 2006

한국 원자력 연구소는 PEFP(Proton Enginnering Frontier Poject)라고 하는 프로젝트를 수행 중이며, PEFP는 고에너지 양성자 가속기에 대한 프로젝트이다. 양성자 가속기에 대한 제어 시스템은 안정적인 운전 제어를 위해서 장치의 상태를 주기적으로 모니터링 할 뿐만 아니라 장치상태를 저장하여 일정시간 후에 확인이 요구되면 저장된 데이터를 이용하여 이전 정보를 추적할 수 있어야한다. 따라서 양성자 가속기 제어시스템에서는 실시간으로 들어오는 진공 데이터 정보를 저장 및 저장된 데이터를 열람이 가능한 저장 시스템으로 구성하였다. 저장된 데이터들은 RFQ(Radio Frequency Quadrupole) Cryopump, Turbo Pump, Press Gauge, Gate Valve, Compressor와 DTL(Drift Tube Linac) Multi-Gauge, Turbo Pump등의 진공도 및 제어변수 등이 있다. 이들 각각의 진공장치로부터 전달되는 진공 데이터들을 저장하기 위해 EPICS Extension toolset중에서 저장하는 기능을 가진 Channel Archiver를 양성자 가속기 제어 시스템에 추가하였다

• 항공우주기술
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• 제9권2호
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• pp.204-209
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• 2010

초기 엔진 시동을 위해 터빈을 구동하기 위한 고압가스를 제공함으로써, 발사체 액체추진기관의 터보펌프 시동기 역할을 수행하는 파이로스타터의 개발 현황에 대해 간단히 소개하기로 한다. 우선 개발 이력을 간단히 정리하였으며, 파이로스타터 개발에 있어서 핵심 부분이라고 할 수 있는 고체추진제, 내탄도, 럽쳐디스크, 점화기 부분에서의 현재 기술 현황을 정리하였다. 현재의 기술개발 수준을 고려해 볼 때, 향후 파이로스타터 개발요구조건을 충분히 만족시킬 수 있을 것으로 기대된다.

• 대한기계학회:학술대회논문집
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• 대한기계학회 2004년도 추계학술대회
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• pp.760-765
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• 2004

One of the obstacles for a magnetic bearing to be used in the wide range of industrial applications is the failure modes associated with magnetic bearings, which we don't expect for conventional passive bearings. These failure modes include electric power outage, power amplifier faults, position sensor faults, and the malfunction of controllers. Fault-tolerant magnetic bearing systems have been proposed so that the system can operate in spite of some faults in the system. In this paper, we designed and implemented a fault-tolerant magnetic bearing system for a turbo-molecular vacuum pump. The system can cope with the actuator/amplifier faults as well as the faults in position sensors, which are the two major fault modes in a magnetic bearing system.

• 한국마린엔지니어링학회:학술대회논문집
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• 한국마린엔지니어링학회 2006년도 전기학술대회논문집
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• pp.57-58
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• 2006

Pumps have been widely used for transporting fluid in most of the merchant ships. However, the present status of using pumps for marine vessels has not been studied. This paper is to classify and analyze pumps installed in many ships(LNGC, Oil Tanker, Bulk, Container, Training ship). Finally, Pumps installed in the training ships are compared with merchant ships about the present status of using pumps.

• Tribology and Lubricants
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• 제21권3호
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• pp.122-129
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• 2005

The floating ring seal has the ability of minimizing clearance without rubbing phenomenon. However, the seal ring can be unstable due to extremely high lock-up eccentricity ratio arisen from the poor design of height and surface finish of the ring. The exact prediction of the lock-up position of the floating ring is necessary to design the floating ring properly. The governing equations are developed and solved numerically. The test facility for the measurement of the boundary-lubrication-friction coefficient of the ring‘s surface has been established. Based on the results of analysis, the geometric conditions of the floating ring seal are suggested for operating at a low lock-up eccentricity ratio.