• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.731-736
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• 2011

A pneumatic driving solenoid valve operates pneumatic control devices by opening/closing operating flow passage when the command is given by control system for the liquid-propellant feeding system of space launch vehicle. The simulation model of pneumatic driving solenoid valve is designed with AMESim to verify the designs and evaluate the dynamic characteristics and pneumatic behaviors of valve. To validate a valve simulation model, the simulation results of their operating durations of valve by AMESim analysis are compared with the results of experiments. In addition, the results of internal flow simulation with FLUENT are utilized to improve the accuracy of valve-modeling. Using the model, we analyze performance of valve; opening/closing pressure, operating time on various design factors; shape of control valve seat, drainage seat, rate of sealing diameter, volume of control cavity. This study will serve as one of reference guides to enhance the developmental efficiency of ventilation-relief valves with the various operating conditions, which shall be used in Korea Space Launch Vehicle-II.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.30 no.3
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• pp.239-248
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• 2017

According to the structure, solenoid valve can be categorized as spool valve or poppet valve. While various research on spool valve which has simple structure and fine susceptibility to contamination has been conducted, poppet valve which has less susceptibility to contamination and advantage in a long time operation still need much research because of its complicated structure. In order to design the poppet valve, various parameters such as the diameter of the poppet, the angle of the poppet, the diameter of the disk, the spring stiffness, the spring preload and flow path structure should be considered. Conventional studies on poppet valve usually take only one design parameters and did not much focused on the effect of the parameters on flow characteristics. In this paper, the change of the flow characteristics according to the design parameters of the poppet valve for 3/2Way solenoid valve is analyzed. The previous studies and the results of initial model analysis was referred for the selection of the design parameters. The effects of design parameters on maximum pressure, minimum pressure, and pressure drop was examined using analysis of means(ANOM).

• Aerospace Engineering and Technology
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• v.11 no.2
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• pp.109-116
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• 2012

A vent-relief valve performs as a safety-valve assembly for liquid propellant feeding system of space launch vehicle, which relives pressurant propellant tanks during the filling and the flight. At vent mode, valve is opened and closed by driving pneumatic pressure, and at relief mode, valve is automatically operated to set relief pressure. In this study, we have analyzed a basic layout of vent-relief valve which is designed using foreign LVs(Saturn) to satisfy requirements of Korean Space Launch Vehicle. The simulation model of vent-relief valve is designed by using the AMESim code to verify design parameters and evaluate pneumatic behaviors of valve. In this study, we performed dynamic characteristic simulations on design parameters. And we could predict opening/closing time and pressures, operating performances on design parameters. Using this results, we could suggest detail design and boundary conditions of design.

• Proceedings of the Korea Institute of Fire Science and Engineering Conference
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• 2010.10a
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• pp.332-336
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• 2010

알람밸브는 습식 스프링쿨러 시스템에 필수적으로 사용되는 밸브로써 알람밸브의 오작동 및 고장 등은 치명적인 인명 및 재산의 손실을 가져 올 수 있으므로 소방밸브의 안전성 기준은 매우 높다. 이에 현재 제작되고 있는 알람 밸브는 강도 안전성 측면에서 매우 안전하게 설계가 되어있으며 주철 재질로 주물을 통해 제작된다. 하지만 이러한 과도한 안전설계는 오히려 과도한 무게의 부담으로 시스템에 무게 부담을 주기도 한다. 그러므로 본 논문에서는 밸브의 무게를 경감시키면서 충분한 강도안전성을 가지는 밸브의 설계안을 제시하고 유한요소 해석을 통하여 그 결과를 살펴보았다.

• Journal of Advanced Marine Engineering and Technology
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• v.40 no.7
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• pp.663-670
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• 2016

This paper introduces the concept of the computer-aided engineering(CAE) design method for a bypass valve in a system that is used for the safe lifting of mineral resources in deep-seabed mining. Although the bypass valve has a simple mechanism, its design is very difficult because of various influencing factors. This equipment, which has a complex design process, should be developed by CAE-based design method. The method can perform the design, design verification, and virtual experiment at the same time. In this study, the CAE-based method for the design of the bypass valve has been developed using fluid dynamics, multi-body dynamics, and optimization method.

• Proceedings of the Korea Water Resources Association Conference
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• 2022.05a
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• pp.185-185
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• 2022

상수도 관망의 운영 단계에서 비정상상황의 발생은 필연적으로 발생하며, 비정상상황 발생 시상수도 관망 내 설치된 제수 밸브의 차폐를 통해 해당 구역의 격리 후 복구를 진행한다. 일반적으로 제수밸브를 통해 격리될 수 있는 최소 구역은 세그먼트로 정의하고, 제수밸브 설치 시 세그먼트의 격리로 인한 상수도 관망의 피해를 줄일 수 있도록 위치를 선정한다. 제수 밸브를 통한 격리 시 상수도 관망의 흐름 경로와 유향, 유속의 변화와 같은 수리적 특성 변화가 불가피하다. 지난 '19년도에 발생했던 3건의 수질 사고가 수리적 특성 변화에서 기인했던 것을 고려할 때, 제수밸브 차폐로 상수도 관망의 부분 격리 시 발생 가능한 수리적 특성 변화에서도 수질 사고가 야기될 가능성이 있다. 기존 제수밸브 위치를 결정한 연구들을 보면, 대부분 제수밸브 위치에 따라 결정된 세그먼트의 격리 시 수압 저감을 고려하여, 격리 시에도 상수도 관망의 성능을 최대한 유지할 수 있도록 결정하는 것이 일반적이다. 다만, 앞서 언급한 것과 같이 격리 시 발생 가능한 수리적 특성 변화로, 수압 저감 외에도 예기치 못한 수질 사고의 발생 원인이 되기도 한다. 이에 따라 제수밸브의 최적위치를 결정할 때 수리적 특성 변화를 고려해야 예지치 못한 2차 피해를 줄일 수 있을 것이다. 이에 본 연구는 그래프이론을 활용하여 격리 전후 관로의 유향 변화를 최소화하도록 제수밸브 최적 위치 결정하는 방법론을 제안한다. 그래프이론은 망의 형태를 가지는 상수도 관망의 연결성을 정량화할 수 있으며, 본 연구에서는 수리학적 거리 인자를 적용하여 격리 시에도 각 수요절점이 최소 경로를 확보할 수 있도록 유도하였다. 해당 방법론은 가상 관망에 적용하여 수리학적 거리 인자에 따른 설계와 기존 상수도 관망 성능 극대화 설계 안을 비교하였다. 또한 수질 사고 위험도 인자를 정의하여 해당 인자에 따른 각 설계 안의 효과를 분석하였다. 본 연구는 향후 수질 사고를 고려한 밸브 시스템의 설계 및 운영에 활용할 수 있을 것으로 기대한다.

• Journal of the Korean Institute of Gas
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• v.10 no.4 s.33
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• pp.23-28
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• 2006

This paper presents the strength safety and the weight reduction analysis of nine gas valve models for a LPG cylinder using a finite element analysis program, MARC and Taguchi's experimental method. The maximum Von Mises stress of a gas valve body represents a safety of a brass valve structure for the given gas pressure of $91kg/cm^2$, which considered a safety factor of a LPG gas cylinder. The weight reduction analysis is very important for reducing a gas flow friction loss and a manufacturing cost as a design parameter. The calculated results present an design model 9 as an optimized design data with 10mm radius of a lower part gas flow pipe A, 6mm radius of an upper part gas flow pipe B and a connecting length 2 mm of tapered pipe D between lower and upper pipes.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2011.11a
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• pp.725-730
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• 2011

A 2-way solenoid valve regulates to maintain the pressure of ullage volume of propellant tanks when the command is given by control system for the liquid-propellant feeding system of space launch vehicle. The simulation model of solenoid valve for pressurization is designed with AMESim to verify the designs and evaluate the dynamic characteristics and pneumatic behaviors of valve. To validate a valve simulation model, the simulation results of their operating durations of valve by AMESim analysis are compared with the results of experiments. Using the model, we analyze performance of valve; opening/closing pressure, operating time on various design factors; shape of control valve seat, basic valve seat, rate of sealing diameter. This study will serve as one of reference guides to enhance the developmental efficiency of ventilation-relief valves with the various operating conditions, which shall be used in Korea Space Launch Vehicle-II.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.21 no.1
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• pp.387-392
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• 2020

This paper proposes a flow-rate control system for industrial valves. Industrial valves are used in piping systems to control the flow rate and pressure. In general, valves used in pipelines are classified into globe valves, butterfly valves, and ball valves according to the shape. Motor, hydraulic, and pneumatic systems are used for operating valves. The flow meter should measure the flow rate when configuring the flow-rate control system. On the other hand, because the flow rate of the valve can be expressed by flow coefficient, a control scheme is proposed using the pressure deviation, which measures at the front and rear of the valve. The transfer function for the valve, according to the control input, was estimated using the signal compression method. Based on the induced transfer function, the disturbance observer was designed to improve the command following the performance of the valve stem. The performance of the proposed control method is compared with the flow-rate control result using the flow meter used.

• Journal of Aerospace System Engineering
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• v.13 no.4
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• pp.50-59
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• 2019

The design of the main control valve, which is the main component of the flap control system, was based on actual manufacturing experience on the basis of trial and error method. In this paper, a model-based part design method is proosed. The flap control system consists of a main control valve, fail-safe valve, solenoid valve, LVDT and force motor. The main control valve consists mainly of a spool and slot. The important design parameters of the main control valve are the slot width, overlap and clearance. AMESim is linked to the model and it analyzes the flow path of the main control valve. Applying the proposed design procedure, it was confirmed that the required performance was satisfied within the allowable machining error range.