• Proceedings of the Korean Society of Propulsion Engineers Conference
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• v.y2005m4
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• pp.219-224
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• 2005

In order to investigate transient behaviour of the CRW(Canard Rotor Wing) type UAV(Uninhabited Aerial Vehicle) propulsion system during flight mode transition considering flow control valve operation, the propulsion system was modelled using SIMULINK commercial program. For transient simulation of the main engine system, the ICV(Inter-Component Volume) method was applied. The valve system is to control the gas flow of the rotary duct system and the main duct system, and the analysis was performed with an assumption that the total gas mass flow of the main engine is the same as summation of the rotary duct flow and the main duct flow, and with consideration of valve loss, flow rate and effective area in valve angle variation. The performance analysis was carried out during flight mode transitions from the rotary flight mode to the fixed wing flight mode and vice versa mode at altitude of 1Km, flight Mach number 0.1 and maximum engine rpm.

• Journal of the Korean Society of Propulsion Engineers
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• v.9 no.3
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• pp.127-132
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• 2005

In order to investigate transient behavior, of the CRW(Canard Rotor Wing) type UAV(Uninhabited Aerial Vehicle) propulsion system during flight mode transition considering flow control valve operation, the propulsion system was modelled using SIMULINK commercial program. The valve system is to control the gas flow of the rotary duct system and the main duct system, and the analysis was performed with an assumption that the total gas mass flow of the main engine is the same as summation of the rotary duct flow and the main duct flow, and with consideration of valve loss, flow rate and effective area in valve angle variation. The performance analysis was carried out during flight mode transitions from the rotary flight mode to the fixed wing flight mode and vice versa mode at altitude of 1km, flight Mach number 0.1 and maximum engine rpm.

• Journal of Advanced Marine Engineering and Technology
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• v.38 no.3
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• pp.292-301
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• 2014

This paper describes development of distributed type independent electro-hydraulic ballast valve remote control system with diagnostic function based on fuzzy inference using redundant Modbus communication and ethernet Modbus TCP/IP. Diagnostic function estimate degradation of system components and diagnose system faults, which results in shortage of fault maintenance time and improvement of system safety. Slave devices which control each valve and master device which command, monitor and diagnose slave system are developed. Slave devices are connected to master device with redundant Modbus networks and master device is connected to ship's integrated control system with Modbus TCP/IP. Also this paper describes development of simulator to test and confirm whether developed system can be integrated with ship's integrated control and monitoring system.

• Proceedings of the KIPE Conference
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• 2018.11a
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• pp.18-20
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• 2018

본 논문에서는 위치-속도 모드전환 제어기를 제안하고 이 제어기를 활용한 운동범위 제약을 가진 기계의 연착륙 방법을 제시한다. EGR 밸브와 같은 기계제품들은 이동할 수 있는 범위를 가지며 범위 내에서 위치를 제어한다. 위치제어 중 양끝 위치로 이동시 기계는 빠른 속도로 충돌할 수 있다. 속도가 빠르면 빠를수록 충돌 시, 충격력이 커지며, 충격력으로 기구물은 빠르게 마모되고 수명을 단축시킬 수 있다. 따라서 양끝 위치 이동 시, 일시적으로 속도를 제어할 수 있는 제어기가 필요하다. 제안된 위치-속도 모드전환제어기는 Hanus Scheme을 사용하여 모드전환 시, 범프효과로 인한 부작용을 감소시켰으며, 모드전환 이후 모드 전환된 제어기의 지령을 빠르게 추종한다. 마지막으로, EGR 밸브 양끝 위치 학습알고리즘에 적용시켜 시험하였다.

• 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 KIPE Conference
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• 2010.07a
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• pp.528-529
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• 2010

VVA(Variable Valve Actuation) 기술은 엔진의 흡기 밸브 작동 모드를 가변하여, 엔진의 연비와 성능을 향상시키는 차세대 엔진 기술이다. 흡기캠에 의해 밸브가 직접 작동되는 일반 엔진과 달리 VVA 엔진은 흡기캠, VVA기구, 모터, 제어기 등에 의해 밸브 작동 모드가 정밀하게 제어되므로, 엔진에서 발생되는 손실을 줄여 연비가 크게 향상되고 엔진의 최고 성능이 향상된다. 또한 VVA 엔진을 장착한 차량은 차량의 발진 응답성이 향상되고, 배기가스 배출량을 줄일 수 있어 친환경 저연비 차량을 실현하는데 핵심 차량부품기술이다. 본 논문에서는 이와 같은 VVA 기구의 적용을 위한 DC모터 및 제어기를 개발하였다.

• Proceedings of the Korean Nuclear Society Conference
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• 1996.05b
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• pp.17-22
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• 1996

차세대원자로의 안전계통 성능향상을 위하여 축압기 설계에서 채택하고 있는 피등적 유량조절 장치인 vortex 밸브의 특성을 분석하였다. 단순화된 해석모델을 이용하여 vortex chamber의 유동 pattern을 분석하였으며 vortex 밸브의 성능에 중요한 영향을 미치는 기하학적 인자들의 영향 유동모드 전환시 주유량이 공급되는 수관의 수위거동 특성을 분석하였다. 또한 3차원 모의가 가능한 FLUENT 코드를 사용하여 vortex chamber의 유동장을 해석하여 vortex 밸브의 유동특성을 분석하였다.

• Journal of the Korea Academia-Industrial cooperation Society
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• v.18 no.1
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• pp.454-459
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• 2017

In this study, a thermal system was designed using a 3-way valve and PTC attached to a solar module. This design could help solve the problem of rising fossil fuel costs caused by limited reserves and environmental problems resulting from fossil fuel use. The thermal system is a hot-air and heating control system composed of a temperature sensor part, mode setting part (for hot air and heating modes), supply part, and thermal system control part. The temperature sensor part has piping and an indoor temperature display, and the temperature setting part has multiple monitoring functions. The mode setting part switches between hot air and heating modes and can be used to set the temperature. The thermal system control part performs functions such as PTC control and temperature setting, PTC day and night and time selection, hot air and heating control, and three-way valve selection. The results verify that the system operates with stable response speeds of $680{\mu}s$ in the temperature sensor part, $700{\mu}s$ in the mode setting part, and $610{\mu}s$ in the thermal system control part.

• Journal of IKEEE
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• v.23 no.2
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• pp.675-680
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• 2019

The coal-fired power plant is operated by a combined operation method, which is operated by sliding pressure operation under low load and by fixed pressure operation under high load for improved efficiency. The combined operation is divided into two and three valve open modes. Each plant is operated by selecting the turbine control valve mode in accordance with the manufacturer's recommendation, but is not really operating at the optimal sliding pressure operation according to load range, also Load range of each plant is configured differently. The internal efficiency of the high-pressure turbines is reduced due to loss of the turbine valves and the plant efficiency is reduced. To solve these problems, In this paper, the optimum load range is selected through the analysis method of thermal performance by each load in order to improve the optimum variable pressure operation load range by turbine control valve mode.

• Journal of the Korean Society for Precision Engineering
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• v.17 no.10
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• pp.69-76
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• 2000

Lots of semi-active control devices have been developed in recent years because they have the best features of passive and active system. Especially, controllable magneto-rheological(MR) fluid devices have received significant attention in these area of research. The MR fluid is the material that reversibly changes from a free-flowing, linear viscous fluid to a semisolid with a controllable yield strength in milliseconds when exposed to a magnetic field. If the magnetic field is induced by moving a permanent magnet instead of applying current to a solenoid, it is possible to design a MR damper consuming low power because the power consumption is reduced at steady state. This paper proposes valve mode MR damper using permanent magnetic circuit that has wide range of operation with low power consumption, a design parameter is adopted. The magnetic circuit, material of choke and choke type are selected experimentally with the design parameter. The behaviors of the damper are examined and torque tracking control using PID feedback controller is performed for step, ramp and sinusoidal trajectiories.