• Title/Summary/Keyword: 모사시스템

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Dynamic Behavior Simulation of Reactor for Chemical Heat Pump System Design (화학 열펌프 시스템 설계를 위한 반응기의 동적 거동 모사)

  • 김태민;김성준;최홍규;이태희
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 1994.11a
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    • pp.43-47
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    • 1994
  • 화학 열펌프 시스템의 반응기 설계를 위하여 정적 설계의 결과를 이용하여 시간에 따른 전화율, 온도, 압력, 출력 등의 변화에 대한 모사를 시도하였다. 정적 모사를 통한 설계결과는 동적 거동 모사의 결과와 유사하였으며, 이로부터 정적모사가 동적모사를 위한 적절한 초기치와 기초 설계 정보를 제공함을 알 수 있었다. 본 연구를 통하여 확립된 설계절차와 해석방법에 따른 사례연구를 통하여 향후 실용화될 화학 열펌프 시스템의 개략적인 사양과 바람직한 설계방향을 제시 할 수 있었으며, 반응기의 조작에 따른 제어변수의 영향을 평가하는 기준을 마련할 수 있었다.

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Development of Pervaporation System Simulator (투과증발 시스템 모사기 개발)

  • 장재화;유제강;안승호;이규현;류경옥
    • Membrane Journal
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    • v.7 no.1
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    • pp.31-38
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    • 1997
  • A simulator has been developed in order to simulate and to be used to design the pervaporation system for separating organic/water mixtures. This simulator is composed of simulation engine, which includes a modeling of pervaporation system and the numerical analysis, and Graphical User Interface(GUI), which enables us to operate the simulator more easily in the Windows environment. The structure and operation of simulator were clearly presented by demonstrating the full-scale ethanol dehydration process. The performance of simulator turned out to be fairly good through comparing the simulation results with the experimental data of ethanol dehydration pilot tests.

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Performance Evaluation of Heavy Residual Oils in IGCC Plants (Heavy Residual Oil IGCC 플랜트 적용 성능 평가)

  • 이승종;윤용승;유진열;이정한
    • Proceedings of the Korea Society for Energy Engineering kosee Conference
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    • 1997.10a
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    • pp.9-16
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    • 1997
  • 원유 정제의 가장 heavy한 잔류물인 중잔유(heavy residual oil)의 IGCC 프랜트의 적용성능을 평가하기 위한 방안으로, 정적시스템 모사방법을 사용하여 중잔유를 발전 연료로 사용한 IGCC 플랜트를 모사하였다. 모사에 적용한 중잔유는 Visbreaker Residue와Butane Asphalt이며, 시스템 모사방법의 검증을 위해서, 중잔유의 가스화 반응 모사결과를 Shell사에서 발표한 실증자료와 비교하여 사용된 모사방법이 적절함을 입증한 후 이 결과를 이용하여 IGCC 플랜트에 대한 모사에 적용하였다.

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Simulation of Design Factor Effects on Performance of Vacuum System (진공시스템 성능에 대한 설계인자 영향 전산모사)

  • Kim, Hyung-Taek;Jeong, Kwang-Pil
    • Journal of the Korean Vacuum Society
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    • v.16 no.6
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    • pp.405-413
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    • 2007
  • Effect of design factors on the performance of vacuum system was simulated for optimum design of system. In this investigation, the feasibility of modelling mechanism for $VacSim^{Multi}$ simulator was proposed. Simulation results of pumping design factor showed the possibilities of simulation fore-study for the detailed design factors. Simulation of roughing pump presented the expected pumping behaviors based on the specifications of commercial pump. Application of booster pump exhibited the high pumping efficiency for middle vacuum range. Combinations of optimum backing pump for diffusion and turbo vacuum system were obtained. And, the characteristics of process application of both systems were also acquired.

Trend of Simulation Systems for Satellite Development and Verification (위성 개발 및 검증을 위한 모사 환경 시스템 개발 현황)

  • Kim, Young-Yun;Cho, Seung-Won;Choi, Jong-Yeoun;Choi, Joon-Min
    • Current Industrial and Technological Trends in Aerospace
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    • v.6 no.2
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    • pp.40-50
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    • 2008
  • Most of satellite program process consists of mission analysis, thermal, structure, electronics design, and operation, etc. Each step has several steps like design phase, development phase, and verification phase, etc. As to do this kind of process, very high costs and much time are required, further high risk is included. So for solving those difficulties, satellite developers have designed and used satellite simulator system. In early stage of satellite development, simulator system was just used for a fragment of development and verification, so it could not give enough advantage on satellite development. In order to get high advantage on satellite development, full system level simulators which can be used for several steps for development and verification are evolved. So This paper introduces the trend of simulation systems for satellite development and verification used by several satellite developers.

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화학공정 비정상상태 모사기의 최적 적분전략에 대한 고찰

  • 박정애;이강주;윤인섭
    • 제어로봇시스템학회:학술대회논문집
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    • 1989.10a
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    • pp.348-353
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    • 1989
  • 화학공정 비정상상태 모사에 있어서 계산상 불리한 특성인 불연속성과 stiff한 성질에 대처할 수 있도록 sequential-clustered구조를 기본으로 하는 모사기에 불연속 처리 루틴을, 구현하였고, stiff성질의 완화를 위해 공정의 동특성 차이에 기인하는 latency를 이용하여 적절한 clustering기법으로 cluster크기를 결정하는 pre-processor를 개발하였다.

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Simulation of Vacuum Characteristics by Applications of Vacuum Valves in Display Processing (디스플레이공정 진공시스템 밸브응용에 따른 진공특성 전산모사)

  • Kim, Hyung-Taek
    • The Journal of the Institute of Internet, Broadcasting and Communication
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    • v.12 no.2
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    • pp.77-83
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    • 2012
  • Effect of valve conductance on performance of vacuum system was simulated for optimum design of vacuum system. In this investigation, the feasibility of modeling mechanism for VacSimMulti simulator was proposed. Application specific design of vacuum system is required to meet the particular process conditions for various industrial implementations of vacuum equipments. Geometry and length, diameter of vacuum valve were modeled as simulation modeling variables for conductance effects. Series vacuum system was modeled and simulated with varied dimensions and structures of exhaust valves. Variation of valve diameter showed the more significant effects on vacuum characteristics than that of pipeline length variations. It was also observed that the aperture structure of valve had the superior vacuum characteristics among the modeled systems.

Development of the Emulator on Propulsion System (추진시스템 신호모사장비 개발)

  • Chung, Soon-Bae;Kim, Jung-Hoi;Park, Kon-Kuk;Kim, Young-Sam
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2008.11a
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    • pp.431-432
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    • 2008
  • In order to develop and inspect the electronic controller of propulsion system, It must emulate the electronic signal similar to actual signal. The applied signals on propulsion system are engine speed, turbine speed, various kinds of temperatue signal, pressure signal, LVDT/RVDT position signal and so forth. Contents are the development of emulator that simulate the electronic signals similar to actual signals.

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Development of the Gas Charging Simulator for Reaction Control System of KSLV-I (KSLV-I RCS 충전모사 시스템 개발)

  • Jeon, Sang-Woon;Jung, Seul;Kim, Ji-Hun
    • Aerospace Engineering and Technology
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    • v.8 no.2
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    • pp.122-126
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    • 2009
  • KSLV(Korea Space Launch Vehicle)-I is designed as a launch vehicle to enter a 100 kg-class satellite to the LEO(Low-Earth Orbit). Attitude angles of the upper-stage, including roll, pitch and yaw are controlled by cold gas thruster system using nitrogen gas. To verify the flow rate of the gas charging system and to prepare a nitrogen gas charging scenario, the development of a gas charging simulator for RCS(Reaction Control System) is required. This paper describes the orifice design, development, and test of the gas charging simulator for RCS of KSLV-I.

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Understanding and Their Application of GoldSim Transport Pathways to Mass Trasport Simulation (질량 이동 모사 프로그램 개발을 위한 골드심 이동 패쓰웨이의 이해와 활용)

  • Lee, Youn-Myoung;Jeong, Jongtae
    • Journal of Nuclear Fuel Cycle and Waste Technology(JNFCWT)
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    • v.12 no.2
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    • pp.135-151
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    • 2014
  • It is very important to properly understand such "Transport Pathways" elements as "Pipe" and "Cell" pathways in commercial GoldSim Transport Module (GTM) for developing higer quality models and programs for performance assessment of complex radioactive waste repositories. With an illustrative case under an earthquake scenario, by which an increasement in the groundwater flow rate occurs though the geological medium, ways of avoiding possible modeling errors in the nuclide transport modeling in the radioactive waste repository system for its safety assessment by utilizing such pathways are discussed and a proper usage of the pathways is proposed.