• Title/Summary/Keyword: 흐름분리

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Separation of Colloidal Particles by Holow Fiber Flow Field Flow Fractionation Using Osmotic Sink (삼투압을 이용한 중공사막 흐름장 흐름 분획법에 의한 콜로이드 입자의 분리)

  • 신세종;이원주;전용한;이경현;민병렬
    • Proceedings of the Membrane Society of Korea Conference
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    • 1998.04a
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    • pp.110-112
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    • 1998
  • 1. 서론 : 분석화학의 중요한 과제중 하나 고효율(high efficiency)과 고해상도(high resolution)를 가지고서 혼합물에서 분자나 입자의 분리능을 개선하는 것과 낮은 수준의 농도에서 이런 분획들(fractions)을 정량화 하는 것이다. 현재의 추세는 분리하고자 하는 분자의 상한선을 증가시키는 것이 순수과학과 산업에서 중요하게 되었다. 이런 분리 기술의 응용은 거대분자(macromolecules)와 입자들(particles)인 cell fragments, plasmides, chromosomes, liposomes, synthetic polymers 등에 적용되고 있는데, 고전적인 분석방법으로는 한외여과, 원심분리, 크기배제 크로마토그래피 등이 있지만 시간이 걸리고 해상도와 효율에 제한이 있다.

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Development of an Integrated Electrode-bipolar Plate Assembly with Reduced Contact Resistance for Vanadium Redox Flow Battery (바나듐 레독스 흐름전지용 접촉저항 감소 일체형 전극-분리판 조립체 개발)

  • Amanpreet Kaur;Jun Woo Lim
    • Composites Research
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    • v.37 no.3
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    • pp.190-196
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    • 2024
  • The bipolar plate is a crucial element of the vanadium redox flow battery (VRFB) as it serves as both the electrical conduit and the structural support for the cell within the VRFB stack. Although, the graphite material is primarily used for the bipolar plate due to its excellent electrical conductivity, a significant limitation of performance of the VRFB is present due to high interfacial contact resistance (ICR) arises between the electrode and bipolar plate in the cell stack. This study aims to develop an integrated electrode-bipolar plate assembly that will address the limitations of the ICR. The integrated assembly was constructed using a single carbon felt with thermoplastic and thermoset polymers utilizing hot press method. Experimental results verify that the bipolar plate assembly exhibits reduced area specific resistance (ASR) due to the continuous electrical path. Additionally, from the charge/discharge cell test results, the integrated assembly shows improved cell performance. Therefore, the developed integrated electrode-bipolar plate assembly can serve as a substitute for the conventional bipolar plate and electrode assembly.

Analysis of Carbon Dioxide Separation with Countercurrent Flow in Hollow Fiber Membrane by Numerical Analysis (수치해석에 의한 향류 흐름 중공사 분리막의 이산화탄소 분리 성능 해석)

  • Lee, Yong-Taek;Song, In-Ho;Ahn, Hyo-Seong;Lee, Young-Jin;Jeon, Hyun-Soo;Kim, Jeong-Hoon;Lee, Soo-Bok
    • Membrane Journal
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    • v.16 no.4
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    • pp.252-258
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    • 2006
  • A numerical analysis was performed for a separation process of carbon dioxide from a flue gas stream using polyethersulfone hollow fiber membranes. Countercurrent flow governing equations were regarded to be two point boundary-value problem and the nonlinear ordinary differential equation were simultaneously solved using the finite- difference method. A computer program was developed using the Compaq Visual Fortran 6.6 software. The carbon dioxide permeate driving force and the fred gas residence time at the inside of membrane were found to be very important factors affecting the permeation characteristics of carbon dioxide. The carbon dioxide concentration in the permeate and the flow rate of the permeate were found to be slightly larger by a few percent with a countercurrent flow analysis than those with a cocurrent flow analysis.

Prediction of Hydraulic Characteristics Change around Spur-Dike Using a Two Dimensional Numerical Model (2차원 수치모형을 이용한 수제 주변 수리특성 변화 예측)

  • Kim, Tae-Beom;Jang, Ji-Yeon;Choi, Sung-Uk
    • Proceedings of the Korea Water Resources Association Conference
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    • 2011.05a
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    • pp.132-136
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    • 2011
  • 수제는 유수에 의한 하안 침식을 방지하기 위한 목적의 수공구조물이다. 최근에는 하천복원 및 생태계복원에 대한 관심이 증가되면서, 하안 침식 방지뿐만 아니라 수제에 의한 흐름분리 및 재순환영역의 생태 서식처 제공에 대한 역할이 부각되고 있다. 따라서 수제 설계 시, 수제 설치에 따른 수리특성 변화를 미리 파악하는 것이 필요하지만, 수제 간격, 설치 방향, 수제 높이, 수제 길이, 하도 특성 및 접근 유수 특성 등 다양한 인자에 의해 수리특성 변화를 예측하기란 쉽지 않으며, 비용과 시 공간 측면에서 물리 모형을 이용한 접근법도 용이하지 못하다. 따라서 본 연구에서는 2차원 수치모형을 이용하여 수제 설치에 따른 흐름특성 변화를 모의하고, 모형의 적용성을 판별하고자 하였다. 지배 방정식은 기본적으로 천수방정식을 적용하게 되는데, 수제 주변 흐름 특성은 난류에 의한 횡방향 확산이 중요한 인자로작용하게 된다. 상수 와점성(constant eddy viscosity) 모형, 포물선형 와점성 (parabolic eddy viscosity) 모형을통해 개발 모형의예측 결과와 실험수로 결과를 비교하였다. 수제하류의 재순환영역의 길이가 실험수로의 결과에 비해서 5~6 배까지 확대된 결과를 나타내고 있어, 만족할 만한 결과를 현재까지 얻지 못하였다. 횡방향 확산이 중요한 만큼 k-$\varepsilon$ 모형 등 다양한 난류 모형의 적용이 고려되어질 필요가 있으며, 또한 1차원 요소가 아닌 2차원 요소의 적용을 고려할 필요도 있다.

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Numerical analysis of flow characteristics at the bifurcation channel by changing of discharge ratio using TELEMAC-2D (TELEMAC-2D를 적용한 개수로 분류부 유량비 변화에 의한 흐름특성 분석)

  • Jung, Daejin;Jang, Chang-Lae;Jung, Kwansue
    • Journal of Korea Water Resources Association
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    • v.52 no.1
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    • pp.1-10
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    • 2019
  • This study investigates the flow characteristics, such as velocity distributions, size and location of recirculation zone, longitudinal flow change rates, and bifurcation discharge ratio in the bifurcation channel by TELEMAC-2D, a 2D numerical model. The numerical model is validated by previous experimental results and the numerical results are in relatively good agreement with the experimental results, such as the water surface elevation and velocity distribution in the channels. As the inertial force and moment in the main channel decrease, the bifurcation discharge ratio increases, and the relative high velocity distribution becomes wider and the reverse velocity of the main stream decreases in the branch channel. As the bifurcation discharge ratio increases, the size of the recirculation zone in the branch channel decreases and it can be more clearly calculated by determining the point where the longitudinal froude number $Fr{\approx}0$ as well as drawing the distribution of the streamline distribution.

Numerical Flow Visualization of 1st Cycle Motion of a Fling-clapping Wing (프링-크래핑 날개의 첫 번째 사이클 운동에 관한 수치적 흐름 가시화)

  • Sohn, Myong-Hwan;Chang, Jo-Won
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.32 no.7
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    • pp.1-12
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    • 2004
  • A flow visualization of the 1st cycle motion of a fling-clapping wing that might be employed by butterflies during flight is performed. In this numerical flow visualization, he time-dependent Navier-Stokes equations are solved for two wing motion types; 'fling followed by clap and pause' and 'clap followed by fling and pause'. The result is observed regarding the main flow features such as the sequential development of the two families of separation vortex pairs and their movement. For the fling followed by clap and pause motion, a strong separation vortex pair of counter-clockwise develops in the opening between the wings in the fling phase and they then move out from the opening in the following clap phase. For the clap followed by fling and pause motion, the separation vortex pair developed in the outside space in the clap phase move into the opening in the following fling phase. The separation vortex pair in the opening developed in the fling phase of the clap followed by fling and pause motion is observed to be stronger than that in the opening developed in the fling phase of the fling followed by clap and pause motion.