• Journal of the Korean Society of Propulsion Engineers
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• v.8 no.3
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• pp.27-36
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• 2004

This paper has been conducted to design for pressure regulation system. to simulate for performance of turbo pump unit using AMESim(Advanced Modeling Environment for Simulation of Engineering Systems). With optimized of system, pressure regulation system has been confirmed dynamic characteristics of transient and steady states range based on static modeling of open type turbo pump fed engine system. These results can be utilized to verify for performance test facility of propulsion control system for analysis on control valves, review of the fundamental principle on the control logic and certificating engine feeding system.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.1127-1128
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• 2011

실제 운용중인 수도사업장을 대상으로 펌프모터로 가장 많이 쓰이는 유도전동기의 유량제어를 위해 기존의 방법인 밸브개도에 의한 유량제어 방법과 최근기술인 인버터를 이용한 유량제어 방법을 비교분석하여 효율성을 평가 하였고, 최근 전력전자 기술의 발전에 따라 문제시되고 있는 인버터 사용에 따른 고조파를 분석하여 인버터 시스템 도입에 따른 안정성을 평가하였다. 본 연구에서 평가한 펌프모터의 속도 제어를 위한 기존의 방법인 밸브개도에 의한 유량제어 방법과 인버터를 이용한 유량제어 방법에 대한 효율성 및 안정성 평가결과를 바탕으로 인버터시스템을 산업현장에 적극 도입함으로서 에너지 절감에 따른 생산원가 절감 및 수용가의 용수공급 예측을 통한 관망운영의 안정성을 기대할 수 있다.

• Journal of Industrial Technology
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• v.5
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• pp.21-26
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• 1985

본(本) 연구(硏究)는 주조(鑄造) 및 용접(溶接)을 통하여 제작(製作)된 화력발전용(火力發電用) 대형(大型)밸브에 발생한 결함(缺陷)의 원인(原因)을 규명하기 위하여 사용(使用)된 몇가지 기술에 대하여 언급하였다. 초음파(超音波) 비파괴검사(非破壞檢査)로써 내재(內在)되어 있는 균열의 위치(位置) 및 길이를 예측(豫測)하였다. 균열의 근원(根源)을 다치지 않게 보존(保存)한 채로 시험편(試驗片)에 대(對)하여 기계적 절단(絶斷)을 행하였다. 또한 균열의 원인(原因)을 직접 관찰할 수 있도록 액체 질소에서 낙추법(落錘法)을 써서 파단(破斷)시켰다. 동시(同時)에 균열의 측면양상(側面樣相)과 미세조직(微細組織)과의 관계를 금속현미경 및 전자현미경(SEM)을 통하여서 관찰하였다. 결론적으로 제조시(製造時) 도입(導入)된 결함(缺陷)은 용접과정중에 만들어진 것이 아니라 주조작업중(鑄造作業中)에 용융금속(溶融金屬)의 공급부족(共給不足)으로 인(因)하여 생긴 기공(氣孔)에서 출발(出發)하였음을 알 수 있었다.

• 유체기계공업학회:학술대회논문집
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• 2004.12a
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• pp.748-753
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• 2004

The performance of a valveless micropump driven by chamber wall oscillation was numerically investigated for various frequency and amplitude of the oscillation. The numerical study was performed in the range of oscillation frequency from 200Hz to 1000Hz and amplitude from $1{\mu}m$ to $15{\mu}m$. And optimal values for the parameters are found. At the oscillation frequency 600Hz, the net flow rate of micropump shows a maximum value. Also the results show good agreement with the experimental results. The total flow rate was increased with the oscillation amplitude. However, the net flow rate was found to be decreased over $7{\mu}m$.

• Aerospace Engineering and Technology
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• v.7 no.1
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• pp.40-48
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• 2008

Air mixing system which is composed of air pressure control system, hot pipe system and air mixer, is the facility for mixing hot air($1000^{\circ}C$, 10kg/s) from storage air heater (SAH) and decompressed air($20^{\circ}C$, 15kg/s) from high pressure air supply system. Air pressure control system reduce the pressure of the air, from 32MPa to 3.5 MPa and supply the decompressed air to air mixer. The hot pipe system supply hot air from SAH to air mixer which mix hot with the decompressed air from air pressure control system. Fully mixed air flow rate is 25kg/s and mixed temperature is up to $400^{\circ}C$. So, we can expand the operating envelop of the supersonic ground test facility to low Mach number and low altitude region.

• Journal of Advanced Marine Engineering and Technology
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• v.35 no.6
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• pp.765-772
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• 2011

In this research, the fuel cell system model capable of generating codes in real time was developed to construct of a HIL (Hardware-In-the-Loop) for a SOFC-powered ship. Moreover, the effects of the distribution of the exhaust gas flow rates in a stack, the flow rates of fuels and temperature of air supplied on the temperature characteristics of fuels supplied to the cathode and the anode, the output power of the stack and system efficiency are examined to minimize the temperature difference between fuels supplied to the stack used in a 500kW SOFC system using methane as a fuel. As a result, the temperatures of fuels supplied to the cathode and the anode maintain at 830K when the opening factor of three-way valve located at outlet of turbine is 0.839. Also the process for optimization of methane flow rate considering the fuel cell stack and system efficiency is required to increase the temperatures of fuels supplied to the stack.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.4
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• pp.419-424
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• 2009

A Xenon feed system has been developed for a 300 W Hall-effect thruster intended for orbit maintenance of small satellite. The system can store about 2 kg of xenon gas at 150 bar and is capable of controlling the mass flow rate of the gas at 0.5 SCCM resolution. The performance of the system is verified with a laboratory experiment. It is confirmed that the operation of the feed system is successful at a pressure level of $1.0{\times}10^{-6}$ torr in the vacuum chamber.

• Journal of the Korean Society of Propulsion Engineers
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• v.15 no.1
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• pp.35-44
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• 2011

Mathematical modelling for liquid rocket engine(LRE) main components were conducted to predict the dynamic characteristics when the LRE operates at the transient condition, which include engine start up, shut down, or thrust control. Propellant feeding system is composed of fuel and oxidizer feeding components except for regenerative cooling channel for the fuel circuit. Components modeling of pump, pipe, orifice, control valve, regenerative cooling channel and injector was serially made. Hydraulic tests of scale down component were made in order to validate modelling components. The mathematical models of engine components were integrated into LRE transient simulation program in concomitant with experimental validation.

• Journal of Korea Water Resources Association
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• v.48 no.10
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• pp.869-877
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• 2015

Freshwater may be injected into aquifers to combat sea water intrusion in groundwater or to store water for later retrieval. For these cases to achieve the desired goal groundwater modeling is commonly used to determine locations and rates of injection wells. When these wells are connected to a pipe network, a flow control valve is installed for each well to regulate the injection rate. When a valve opening is modified, pressure changes in the entire pipe network and thereby changes flow rates in other wells. Therefore, desired valve openings must be determined for all injection wells. The pipe flow analysis allows estimation of the minimum pump power in addition to valve openings. Methods are developed to identify valve openings for multiple wells and the minimum pump power. The methodology developed in this work can contribute to precise operation of multiple injection wells.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2017.05a
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• pp.838-842
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• 2017

The thruster valve, which is one of the key components applied to the mono-propellant system for the satellite, has a circular plate spring structure. It can be designed as a structure that does not have positional deformation and particles by friction and repetitive motion. In this study, finite element analysis and verification were performed by setting the width of the circular plate spring as a design parameter with the material, thickness and radius of the circular plate spring as fixed variables. The linearity of the spring constant is shown by the graph that is spring force with displacement. It is confirmed that the optimization design of the circular plate spring is possible by the spring force tendency according to the total area of circular plate spring.