• Proceedings of the Korean Nuclear Society Conference
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• 1996.05b
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• pp.160-165
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• 1996

중수로형 원전에서 일차측 냉각수를 순환시키는 주연수송펌프가 정상운전중 갑자기 정지하는 사고를 강제순환 상실사고라 한다. 강제순환 상실사고는 주열수송계통을 과도압력상태로 만들며, 일반적으로 펌프에 공급되는 IV등급전원 상실사고와 기계적 손상에 의한 주열수송펌프 고착사고로 분류할 수 있다. 본 논문에서는 강제순환 상실사고에 대하여 중수로계통설계의 열수력 해석코드인 SOPHT를 이용하여 주열수송계통의 과도압력상태를 해석하였다. 카나다 원자력 규제위원회(AECB)의 과압 방지조건인 R-77 요구조건에 적절한 유효트립변수를 결정하기 위한 해석이 수행되었으며, 증기발생기 오염상태와 액체방출밸브 작동여부가 고도압력상태에 미치는 영향을 고찰하여 보수적 조건을 제시하였다. 또한 위와같이 결정된 보수적 조건을 근거로 ASME 코드에 명시된 과압 한계치에 대한 만족여부와 과도압력상태에 따른 주열수송계통의 열수력학적 거동을 고찰하여 보았다. 해석결과, 강제순환상실사고시 주열수송계통은 R-77 요구조건에 적합한 원자로트립변수에 따라 안정화되었으며, 계통의 최대압력은 ASME 코드가 규정한 한계치내에 있음을 알 수 있었다.

• The Bulletin of The Korean Astronomical Society
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• v.37 no.2
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• pp.153.2-153.2
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• 2012

발사체 추진기관은 추진제 및 각종 고압가스류를 엔진으로 공급하는 기능, 지상에서 추진제를 발사체로 충전/배출하는 기능, 저온 산화제를 냉각하기 위한 순환 기능, 추진제 탱크를 가압하는 기능, 지상에서 온보드 밸브를 구동하는 기능, 내부 공간 및 라인 퍼지 기능 등을 수행한다. 이와 같은 기능을 수행하기 위해 발사체에는 타 시스템과는 별도로 추진기관 원격제어 시스템을 구성한다. 제어 시스템은 크게 온보드 시퀀스 및 추진제 탱크 압력 제어, 추진제 및 고압가스 충전/배출 제어, 발사체 기능 확인, 내부 기밀 확인 및 발사 직전까지의 상태 모니터링을 위해 구성한 지상측정시스템(GMS), 비행 중 추진기관 상태를 모니터링하기 위한 텔레메트리시스템(TMS)으로 분류한다. 본 논문에서는 일반적인 발사체 추진기관 운용 및 제어 개념을 제어 기능, 시스템 구성, 작동 원리의 단계로 사례와 함께 제시하였다.

• Proceedings of the KAIS Fall Conference
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• 2000.10a
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• pp.113-113
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• 2000

LPG 및 석유류는 온도에 따라서 유량의 변화가 LPG의 경우는 ±0.23%/℃, 무연은 ±0.11%/℃, 등유는 ±0.10%/℃, 경유의 경우는 ±0.09%/℃로 특히 LPG의 경우가 그 변화가 심하므로 정확한 충전량을 계량하는 것이 중요하다. 이는 공정거래 확립의 차원에서 공급자와 소비자 입장에서 반드시 요구되는 사항이다. 이를 위해 본 논문에서는 LPG 충전기의 충전제어 및 자동 온도 보정의 알고리즘을 개발하고 이를 프로그래밍한 후 온도센서와 16-bit 마이크로프로세서(intel 80C196)로 자동 온도 보정이 가능한 LPG 충전기의 충전제어 시스템을 설계 및 제작하였다. 설계 제작된 시스템은 프로세서부, I/O 입ㆍ출력부, VFD(vacuum fluorescent display) 디스플레이 구동부로 구성된다. 충전제어 동작은 LPG 유량계의 encoder로부터의 유량(유속)신호와 기차 보정값 및 15℃를 기준으로 한 온도 센서부의 온도 보정값을 입력받아 솔레노이드 밸브를 제어하여 충전을 제어하게 된다. 온도 보정은 80C196 프로세서의 내부 10-bit A/D 변환기를 사용하여 0.5℃ 분해능으로 온도제어를 할 수 있다. VFD 디스플레이는 유량, 금액, 단가가 표시되며 그 값을 누적시켜 일계, 월계를 알 수 있게 하였다. 그 외에 시스템 진단기능 및 컴퓨터통신, POS 통신이 가능하도록 하였다. 제작된 시스템을 LPG 충전기에 실장하여 시험한 결과 목표한 정확도로 유량이 제어됨을 알 수 있었다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2004.10a
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• pp.68-76
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• 2004

It is essential to develop a transient engine system analysis model for turbopump fed type liquid rocket engine development, especially for deriving engine system test number and conditions. In this study, we proposed a mathematical model of turbopump fed type liquid rocket engine, and inspected transient mode changes around the nominal thrust level of a rocket engine according to variations of trust control valve's opening ratio. To verify the results, we solved the same problem with AnaSyn software from Russia, and concluded that the transient code showed the similar results within $2\%$ with AnaSyn.

• The Magazine of the Society of Air-Conditioning and Refrigerating Engineers of Korea
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• v.17 no.4
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• pp.395-407
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• 1988

Transient flow in a cold-water supply system for cooling the inside of a coal mining pit was numerically simulated. Properly designed and presetted pressure reducing valves control the level of pressures of the piping system at normal or emergent conditions Quasi-steady relations to simulate the valve motion are obtained and the transient performance of the valve is investigated in the present paper. The present method reasonably simulate transient phenomena in the system including the pressure reducing valve. Excessive valve motion and column separation are simulated when the flow is abruptly reduced. A calculated example of the real system is also presented. The simulation can be used for the safety-check and the guidance for design and operation in emergent cases of the system.

• Journal of the Korean Society for Geothermal and Hydrothermal Energy
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• v.17 no.3
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• pp.1-12
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• 2021

In this study, the effects of various operational conditions for floor radiant heating system were researched by experiments. Hot water supply set temperature, indoor air set temperature and supply water flowrate were considered as operational conditions. The control method for this system is On-Off control of automatic thermostatic valve. The purpose of this study is to evaluate indoor thermal control characteristics and energy performance, respectively. As a result, if lower supply water temperature is applied, the supply and return temperature difference is reduced and energy consumption of heat supply is also reduced.

• Spatial Information Research
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• v.12 no.1
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• pp.89-100
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• 2004

Nowadays, the gas utilities have been increasing constantly due to the expansion of the urban areas. Using computerized information database, the gas companies have developed a gas management system in order to maintain the current status. However, this system can only give basic functions of the maintenance and management of the gas facilities and it has no proper utilities to provide information against accidents from gas leaks. Therefore, a gas accident management system has been developed in this study. Through primary and secondary pipe searching algorithm realtime based management system was devised against gas leaks to propose proper actions. In addition, supporting decision making has been enabled providing estimated maximum amount of gas leaks. Furthermore, all the residential units could be identified thereby minimizing damages through early warning. This system can be expected to contribute to enhance the efficiency of the gas management not to mention of protecting human lives and properties of the nation.

• Journal of Astronomy and Space Sciences
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• v.19 no.3
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• pp.207-214
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• 2002

One of the way to derive design parameters of the fuel feeding system in satellite propulsion system is to analyze unsteady flow of liquid propellant (hydrazine). During steady thruster firing the flow rate is constant: if a thruster valve is abruptly shut down among a set of thrusters, pressure spikes much higher than the initial tank pressure occur. This renders the fuel flow unsteady, and the fluid pressure and flow rate to oscillate. If the pressure spikes are high enough, there are possibilities that propellant explosively decomposes, thruster valves we damaged, and adiabatic detonation of the hydrazine propellant is potentially incurred. Reflected shockwaves could also affect the calibration and operation of the pressure transducers. These necessitate the analysis of unsteady flow in the propulsion system design, and pressure behavior inside the propellant line obtained through some governing parameter variation is presented in this work.

• Transactions of the Korean Society of Automotive Engineers
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• v.21 no.5
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• pp.67-73
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• 2013

This experimental work described the effect of flow control valve type on the performance of wobble plate type fuel pump for the stable DME fuel supply. In order to study this, different four types of flow control valves (ITV, SCV, IMV and MPROP) were installed on the wobble plate fuel pump, and fuel flow rate, torque, and temperature variation of pump were investigated under various operating conditions by using pump performance test system. It was revealed that wobble plate type fuel pump worked well with ITV and SCV control valve, and the flow rate and torque of fuel pump was in proportion to the value of valve open duty. The maximum flow rate and torque of fuel pump were achieved around the 50% duty of control valve. Temperature variation at all pump measuring points were under $60^{\circ}C$ which is acceptable.

• Journal of the Korean Society of Propulsion Engineers
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• v.8 no.4
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• pp.67-75
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• 2004

It is essential to develop a transient analysis model for the turbopump-fed type liquid rocket engine development, especially for deriving the number of test and its parameters. In this study we proposed a mathematical model of turbopump-fed type liquid rocket engine, and inspected transient mode changes of a rocket engine according to variations of thrust control valve opening ratio. To verify the results, we solved the same problem with AnaSyn software from Russia, and concluded that the results of transient code we developed deviated within 2% from AnaSyn results. Also, using the transient engine analysis code we showed the possibility to find out the system level design Parameters of the components. For example, we modeled a pressure stabilizer which is used to control the consistency of mixture ratio in the gas generator as forced damping system, and found the stability range of the natural frequency and the damping ratio with the transient engine system analysis code.