• Title/Summary/Keyword: Control of separation

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Design and control of extractive distillation for the separation of methyl acetate-methanol-water

  • Wang, Honghai;Ji, Pengyu;Cao, Huibin;Su, Weiyi;Li, Chunli
    • Korean Journal of Chemical Engineering
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    • v.35 no.12
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    • pp.2336-2347
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    • 2018
  • The azeotrope of methyl acetate methanol and water was isolated using extractive distillation with water as entrainer. The pressure-swing extractive distillation (PSED) process and vapor side-stream distillation column (VSDC) with the rectifier process were designed to separate the methyl acetate, methanol and water mixture. It was revealed that the VSDC with the rectifier process had a reduction in energy consumption than the PSED process. Four control schemes of the two process were investigated: Double temperature control scheme (CS1), $Q_R/F$ feedforward control of reboiler duty scheme for PESD (CS2), $Q_R/F$ feedback control scheme for VSDC (CS3), the feedback control scheme of sensitive plate temperature of side-drawing distillation column to dominate the compressor shaft speed (CS4). Feed flow and composition disturbance were used to evaluate the dynamic performance. As a result, CS4 is a preferable choice for separation of methyl acetate-methanol-water mixture. A control scheme combining the operating parameters of dynamic equipment with the control indicators of static equipment was proposed in this paper. It means using the sensitive plate temperature of side-drawing column to control the compressor shaft speed. This is a new control scheme for extractive distillation.

Effects of vortex generators on the wind load of a flat roof: A computational study

  • Zhao, Yagebai;Deng, Xiaolong;Zhang, Hongfu;Xin, Dabo;Liu, Zhiwen
    • Wind and Structures
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    • v.32 no.1
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    • pp.1-9
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    • 2021
  • Vortex generators are commonly used in mechanical engineering and the aerospace industry to suppress flow separation owing to their advantages of simple structure, economic viability, and high level of efficiency. Owing to the flow separation of the incoming wind on the leading edge, a suction area is formed on the roof surface, which results in a lifting effect on the roof. In this research, vortex generators were installed on the windward surface of a flat roof and used to disturb to roof flow field and reduced suction based on flow control theory. Computational fluid dynamics (CFD) simulations were performed in this study to investigate the effects of vortex generators on reduce suction. It was determined that when the vortex generator was installed on the top of the roof on the windward surface, it had a significant control effect on reduce suction on the roof leading edge. In addition, the influence of parameters such as size, placement interval, and placement position of the vortex generator on the control effect of the roof's suction is also discussed.

Control of the Asymmetric Flow in a Supersonic Nozzle (초음속 노즐에서 발생하는 비대칭 유동의 제어에 관한 연구)

  • Matsuo, Shigeru;Setoguchi, Toshiaki;Hashimoto, Tokitada;Tokuda, Seiya;Nagao, Junji;Kim, Heuy-Dong
    • Journal of the Korean Society of Visualization
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    • v.9 no.2
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    • pp.61-65
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    • 2011
  • Several previous works on rocket nozzle flows have revealed the existence of the transition from FSS to RSS and the occurrence of asymmetric flow associated with the boundary layer separation, which can cause excessive side-loads of the propulsion system. Thus, it is of practical importance to investigate the asymmetric flow behaviors of the propulsion nozzle and to develop its control method. In the present study, the asymmetric flow control method using a cavity system was applied to supersonic nozzle flow. Time-dependent asymmetric flow was experimentally investigated with the rate of change of the nozzle pressure ratio. The results obtained showed that the cavity system installed on nozzle wall would be helpful in fixing the unsteady motions of the boundary layer separation, consequently reducing the possibility of the occurrence of the asymmetric flow.

Continuous Cultivation of Lactobacillus rhamnosus with Cell Recy-cling Using an Acoustic Cell Settler

  • Yang, Yun-Jeong;Hwang, Sung-Ho;Lee, Sang-Mok;Kim, Young-Jun;Koo, Yoon-Mo
    • Biotechnology and Bioprocess Engineering:BBE
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    • v.7 no.6
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    • pp.357-361
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    • 2002
  • Continuous production of lactic acid from glucose by Lactobacillus rhamnosus with cell recycling using an acoustic cell settler was carried out. The performance of the system, such as the concentration of cell and product were compared with the control experiment without recycling. The acoustic settler showed cell separation efficiency of 67% during the continuous operation and the cell concentration in the fermentor with recycle exceeded that of the control by 29%. Com-pared with the control, tactic acid production was increased by 40%, while glucose consumption was only increased by 8%. The higher value of lactic acid production to substrate consumption (Yp/s, product yield coefficient) achieved by cell recycling is interpreted to indicate that the recycled cell mass consumes less substrate to produce the same amount of product than the control Within system environmental changes due to the longer mean cell residence time induced the cells maintaining the metabolic pathways to produce Less by-Product but more product, lactic acid.

A Study of the Control of Plume-Induced Flow over a Missile Afterbody (Missile Afterbody에서 Plume-Induced Flow의 제어에 관한 연구)

  • ;Young-Ki Lee
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • 2003.05a
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    • pp.45-48
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    • 2003
  • The plume interference is a complex phenomenon, consisting of plume-induced boundary layer separation, separated shear layer, multiple shock waves, and their interactions. The base knowledge of plume interference effect on powered missiles and flight vehicles is not yet adequate to get an overall insight of the flow physics in plume-freestream flow field. Computational studies are performed to better understand the flow physics of the plume-induced shock and separation for Simple, Rounded, Porous-extension test model configurations. The present study simulates highly underexpanded exhaust plume effect on missile body at the transoni $c^ersonic speeds. In order to investigate the plume-induced separation phenomenon, Simple, Rounded and Porous-extension plate are attacked to the missile afterbody. The computational result shows that the rounded afterbody and the porous-extension wall attached at the missile base can alleviate the plume-induced shock wave and separation phenomenon and improve the control of the missile body.dy.

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A Coexistence Study of Low-power Short-range Wireless Network and Incumbent Service in the 6GHz band (6GHz 비면허 대역의 저전력 근접 무선통신과 기존 무선업무와의 공존 연구)

  • Kim, Seung-Nam;Lee, Il-Kyoo;Sung, Joo-Young
    • Journal of the Korea Institute of Information and Communication Engineering
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    • v.25 no.8
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    • pp.1074-1081
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    • 2021
  • It has recently been noticed that the headway of unlicensed wireless technology is necessary as user's demands of wireless tech increase and the development of high-speed data service by using low-power short-range wireless network is needed. Hence, it is inevitable to study sharing and coexistence for broadband spectrum of diverse unlicensed application with wide bandwidth. In this paper, an interference examination between unlicensed WiFi (Wireless Fidelity) in the 6GHz and OB (Outside Broadcasting) system which is an incumbent service in the same frequency band was conducted and it suggests separation distance for the coexistence. Thus, MCL (Minimum Coupling Loss) and MC (Monte Carlo) methods were used to set up interference scenarios for the interference analysis and compute the separation distance between two systems according to the same frequency band and frequency separation.

THE STUDY ON THE SEPARATED FLOW OF A HUMP USING RANSMODELING (RANS 모델링을 이용한 Hump 형상의 박리 유동에 대한 연구)

  • Lee, J.;Bae, J.H.;Jung, K.J.
    • Journal of computational fluids engineering
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    • v.22 no.1
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    • pp.8-14
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    • 2017
  • In this paper, separated flow characteristics is studied using the RANS(Reynold-averaged Navier-Stokes) modeling. The analysis is performed for the NASA's hump configuration which is the combination of a flat plate and a hump. This configuration was used in NASA's flow control workshop and it was one of validation cases for RANS and LES simulations. The separation occurs at the 65% of model length where a slot is positioned for the flow control. No flow control case and steady suction case are studied using RANS modeling. The Spalart-Allmaras model and the SST(Shear Stress Transport) model are applied and their accuracy are compared. To correlate CFD analysis with experimental data, the optimal boundary condition was investigated and the effect of a cavity around the slot is studied for the no flow case.

Design and Implementation of test system for safety separation and performance verification of aircraft weapons/equipment (항공기 무장/장착물의 안전 분리 및 성능 검증을 위한 점검 시스템 설계 및 구현)

  • Kim, Hyo-joung;Kim, Yang-won;Kwon, Byung-Gi
    • Journal of Advanced Navigation Technology
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    • v.26 no.2
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    • pp.47-53
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    • 2022
  • With the recent development of defense technology, various aircraft armaments/equipments are being developed. Among them, cruise guided weapons(missile) for launching aircraft can be installed on aircraft aftersecuring reliability and safety through varioustests. In order to avoid collision with aircraft, missile separated from aircraft must release restraint of wing at the specified time, control wing in the specified direction. In order to confirm this, a test system that can control MIL-STD-1760 according to safety separation procedure and verify release performance is required. test system needs a function to check circuit for release of restraints and a function to check driving performance by controlling MIL-STD-1760. In addition, test system should be simulate environment separated from aircraft. This paper presented a testsystemthat can verify circuit and driving performance mounted on missile according to the safety separation procedure, and it was confirmed that it was normally separated from aircraft through flight tests.

Development of EPICS-IOC Measuring Magnetic Field at A/Q separator for Separating Specific Ions (가속이온 분리를 위한 A/Q Separator에서 자장측정용 EPICS-IOC 개발)

  • Lee, Su-Yeong;Yim, Hee-Joong;Kim, Jae-Hong;Mun, Jun-Yeong;Park, Mi-Jeong;Lee, Sang-Il;Lee, Dong-Hoon
    • Journal of the Institute of Convergence Signal Processing
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    • v.22 no.3
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    • pp.91-98
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    • 2021
  • The installation and performance test of the ISOL (Isotope Separation On Line) system for the generation and separation of Rare Isotopes (RI) beams is in progress at the Rare Isotope Science Project (RISP), Institute for Basic Science (IBS). The various RI beams generated by the ISOL target/ion source go through the beam lines and separators, and only the RI beam desired by the user is selected and transmitted to the superconducting linear accelerator at the downstream of the ISOL. In the ISOL system, two separators are installed to separate a specific RI beam, and control is performed by the Experimental Physics and Industrial Control System (EPICS). In this study, an EPICS IOC (Input-Output Control) was developed to measure the magnetic field of a dipole magnet for mass separation of a multivalent (n+) RI beam in the A/Q separator, which is one of the ISOL RI beam separators. The operational stability of the A/Q separator was tested through a magnetic field measurement using a Hall probe.

Study of micro-plastics separation from sea water with electro-magnetic force

  • Nomura, Naoki;Mishima, Fumihito;Nishijima, Shigehiro
    • Progress in Superconductivity and Cryogenics
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    • v.23 no.3
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    • pp.10-13
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    • 2021
  • The method of removing micro-plastics from sea water has been developed using electro-magnetic force. Plastics are difficult to decompose and put a great load on the marine environment. Especially a plastic with a size of 5 mm or less is defined as micro-plastic and are carried by ocean currents over long distances, causing global pollution. These are not easily decomposed in the natural environment. The Lorentz force was generated in simulated sea water and its reaction force was applied to the micro-plastic to control their motion. Lorentz force was generated downward and the reaction force to the plastics was upward. The plastic used in the experiment was polystyrene with a diameter of 6 mm, and the density was 1.07 g/cm3. The polystyrene sphere levitated at the current density of 0.83 A/cm2 and the external field of 0.87T. The particle trajectory calculation was also made to design separation system using superconducting magnet.