• 제목/요약/키워드: Thermal Transpiration

검색결과 23건 처리시간 0.021초

열천이 현상을 이용한 마이크로 펌프내의 희박기체유동 해석 (Numerical Analysis on Thermal Transpiration Flows for a Micro Pump)

  • 허중식;이종철;황영규;김윤제
    • 한국유체기계학회 논문집
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    • 제10권5호
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    • pp.27-33
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    • 2007
  • Rarefied gas flows through two-dimensional micro channels are studied numerically for the performance optimization of a nanomembrane-based Knudsen compressor. The effects of the wall temperature distributions on the thermal transpiration flow patterns are examined. The flow has a pumping effect, and the mass flow rates through the channel are calculated. The results show that a steady one-way flow is induced for a wide range of the Knudsen number. The DSMC(direct simulation Monte Carlo) method with VHS(variable hard sphere) model and NTC(no time counter) techniques has been applied in this work to obtain numerical solutions. A critical element that drives Knudsen compressor Is the thermal transpiration membrane. The membranes are based on aerosol or machined aerogel. The aerogel is modeled as a single micro flow channel.

진공환경에서 열적발산원리의 배압에 따른 효율분석 (Efficiency Analysis of Thermal Transpiration According to Back Pressure under Vacuum Condition)

  • 정성철;허환일
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제29회 추계학술대회논문집
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    • pp.76-79
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    • 2007
  • 마이크로 노즐의 유동특성에 대한 선행연구로부터 우리는 마이크로 노즐에서 점성과 배압에 의해 유동손실이 발생함을 확인하였다. 이러한 유동손실을 극복하기 위해 열적발산원리를 이용한 새로운 개념의 마이크로 추진장치에 대한 연구를 진행하였으며,이는 움직이는 부품이 없이 오직 온도구배만으로 추진제를 낮은 온도에서 높은 온도로 펌핑이 가능하다. 대부분의 열적발산원리에 대한 연구는 많은 발전을 거듭해 왔으며, 주로 대기압 환경에서 에어로젤과 같은 나노 다공물질을 이용하여 소형 진공설비나 가스 크로마토그래피에 적용 목적으로 연구되었다. 하지만 본 연구에서는 폴리이미드 재질을 이용하여 진공환경에서 열적발산원리를 이용한 추진장치의 기초연구를 진행하였다.

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우주진공환경에서의 마이크로 추진 (Micro Propulsion under High Altitude Space Environments)

  • 정성철;허환일
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.405-408
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    • 2008
  • From the previous researches about flow characteristic of micro-nozzle, we found that viscosity and back pressure induced heavy losses in micro nozzle. To overcome thess losses, we began to study new conceptual micro propulsion system that is thermal transpiration based micro propulsion system. It has no moving parts and can pump the gaseous propellant by temperature gradient only (cold to hot). Most of previous research on thermal transpiration is in its early stage and mainly studied for application to small vacuum facility or gas chromatography in ambient condition using nanoporous material like aerogel. In this study, we focus on basic research of propulsion system based on thermal transpiration using polyimide material in vacuum conditions.

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Characteristic Study of Micro-Nozzle Performance and Thermal Transpiration Based Self Pumping in Vacuum Conditions

  • Jung, Sung-Chul;Huh, Hwan-Il
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.866-870
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    • 2008
  • In this study, we designed cold gas propulsion system with minimum 0.25 mm nozzle and micro-thrust measurement system to analyze flow characteristic of micro propulsion system in ambient and vacuum condition. Argon and Nitrogen are used for propellant and the result of experiments is compared with CFD analysis and theory. But there is a point where reduced scale versions of conventional propulsion systems will no longer be practical. Therefore, a fundamentally different approach to propulsion systems was taken. That is thermal transpiration based micro propulsion system. It has no moving parts such as lubricants, pressurizing system and can pump the gaseous propellant by temperature gradient only(cold to hot). We are advancing basic research of propulsion system based on thermal transpiration in vacuum conditions and had tried experiment process and theoretical access in advance. To characterize membrane of Knudsen pump, we select Polyimide material that has low thermal conductivity(0.29 W/mK) and can stand high temperature($300^{\circ}C$) for long time. And we fabricated hole diameter 1, 0.5, 0.2, 0.1 mm using precision manufacturing. Experimental results show that pressure gradient efficiency of Knudsen pump is increased to maximum 82% according to Knudsen number and thick membranes are more effective than thin membranes in transition flow regime.

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도시 가로수의 증산 작용으로 인한 불쾌지수 변화 분석 (Analyzing Change of Discomfort Index for Transpiration of Street Tree)

  • 윤석환;이동근;박채연
    • 한국환경복원기술학회지
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    • 제23권5호
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    • pp.29-43
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    • 2020
  • Thermal environment of city is getting worse due to severe urban heat island caused by climate change and urbanization. The cooling effect of street tree is regarded as a effective way to ameliorate the urban heat environment. The effect is largely made up of shadow formation and transpiration. This study aims to identify how the transpiration affects the discomfort index by analyzing comprehensive impact of the transpiration on the air temperature and relative humidity. The changes in the amount of transpiration, air temperature, and relative humidity were estimated for Seogyo-dong area which has a lot of floating population in Seoul, at 2 p.m. in dry day in July and August. On average, the transpiration of the street tree decreased the temperature 0.3℃ and increased the relative humidity 2.6% in an hour. As a result of these changes in temperature and humidity, the discomfort index rose mostly(0.036 on average). It was always get rise especially on the day when the discomfort index was above 80(0.05 on average). However, compared with the significant change in temperature and humidity, the variation of the discomfort index itself was very slight(up to 0.107). Therefore, the effect of transpiration by the street trees might not be effective in the planning to improve the thermal environment(especially on the day when the discomfort index is high). It is necessary to select the species of trees and planting location considering the cooling effect of shade formation synthetically.

마이크로 추진장치에 적용을 위한 누센수에 따른 열적발산원리의 효율분석 (Efficiency Analysis of Thermal Transpiration According to Knudsen Number for Application to Micro-propulsion System)

  • 정성철;허환일
    • 한국항공우주학회지
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    • 제36권5호
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    • pp.483-490
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    • 2008
  • 마이크로 추진장치에서 노즐의 소형화는 많은 유동손실을 유발한다. 이러한 유동손실을 극복하기 위해 본 연구에서는 열적발산원리를 이용한 마이크로 추진장치에 대한 기초연구를 진행하였다. 움직이는 부품 없이 오직 온도구배만으로 추진제를 낮은 온도에서 높은 온도로 자체 펌핑이 가능한 열적발산장치를 설계, 제작 하였으며, 진공환경에서 누센수에 따른 맴브레인 압력구배효율을 분석하였다. 실험결과 천이영역에서는 두꺼운 맴브레인의 효율이 다소 높았으며, 자유분자영역에서는 두께에 관계없이 최대 압력구배 효율이 82%까지 증가하는 것을 확인할 수 있었다.

Thermal Fatigue Behavior of 3D-Woven SiC/SiC Composite with Porous Matrix for Transpiration Cooling Passages

  • Hayashi, Toshimitsu;Wakayama, Shuichi
    • Advanced Composite Materials
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    • 제18권1호
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    • pp.61-75
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    • 2009
  • The effect of porous matrix on thermal fatigue behavior of 3D-orthogonally woven SiC/SiC composite was evaluated in comparison with that having relatively dense matrix. The porous matrix yields open air passages through its thickness which can be utilized for transpiration cooling. On the other hand, the latter matrix is so dense that the air passages are sealed. A quantity of the matrix was varied by changing the number of repetition cycles of the polymer impregnation pyrolysis (PIP). Strength degradation of composites under thermal cycling conditions was evaluated by the $1200^{\circ}C$/RT thermal cycles with a combination of burner heating and air cooling for 200 cycles. It was found that the SiC/SiC composite with the porous matrix revealed little degradation in strength during the thermal cycles, while the other sample showed a 25% decrease in strength. Finally it was demonstrated that the porous structure in 3D-SiC/SiC composite improved the thermal fatigue durability.

열천이 현상을 이용한 마이크로 펌프내의 희박기체유동 해석 (Numerical Analysis on Thermal Transpiration Flows for a Micro Pump)

  • 허중식;이종철;황영규;김윤제
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.493-496
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    • 2006
  • Rarefied gas flows through two-dimensional micro channels are studied numerically for the performance optimization of a nanomembrane-based Knudsen compressor. The effects of the wall temperature distributions on the thermal transpiration flow patterns are examined. The flow has a pumping effect, and the mass flow rates through the channel are calculated. The results show that a steady one-way flow is induced for a wide range of the Knudsen number. The DSMC(direct simulation Monte Carlo) method with VHS(variable hard sphere) model and NTC(no time counter) techniques has been applied in this work to obtain numerical solutions.

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열적발산원리를 이용한 마이크로 추진장치에 대한 연구 (Study of Micro Propulsion System Based on Thermal Transpiration)

  • 정성철;신강창;김연호;김혜환;이용우;허환일
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2007년도 제28회 춘계학술대회논문집
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    • pp.25-29
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    • 2007
  • 마이크로 인공위성의 자세제어를 위한 마이크로 추진장치에 대한 연구는 대부분 기존의 추진장치를 소형화하는 방향으로 진행되고 있다. 본 연구에서는 이러한 미소추력 발생을 위한 노즐의 소형화로 인한 점성손실, 배압에 의한 손실 등을 대기압실험, 진공환경실험, CFD 해석을 통하여 검증하였다. 또한 마이크로 노즐에서의 유동 손실을 극복하기 위한 방법으로 열적발산원리에 대해 이론적 접근을 시도하였다. 마이크로 추진장치에 적용을 위한 열적발산원리는 움직이는 부품 없이 오직 온도 구배만으로 유동을 제어할 수 있기 때문에 추진장치의 소형화로 야기되는 손실을 극복할 수 있을 것으로 기대된다.

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초소형 추진장치에 적용을 위한 누센펌프의 멤브레인 종류에 따른 질유량 특성 (Mass flow rate of Knudsen pump According to Membrane Type for Micro Propulsion Applications)

  • 김혜환;허환일
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년도 제31회 추계학술대회논문집
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    • pp.36-40
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    • 2008
  • 마이크로 추진장치에서 노즐의 소형화는 많은 유동손실을 유발한다. 이러한 유동손실을 극복하기 위해 본 연구에서는 열적발산원리를 이용한 새로운 개념의 마이크로 추진장치에 대한 기초연구를 진행하였다. 움직이는 부품 없이 오직 온도구배만으로 추진제를 낮은 온도에서 높은 온도로 자체 펌핑이 가능한 열적발산장치를 설계, 제작 하였으며, 진공환경에서 누센수에 따른 멤브레인 압력구배효율을 분석하였다. 또한 기존 누센펌프의 멤브레인인 폴리이미드와 종이재질의 전통 한지를 사용하여 질유량 특성을 비교하였다.

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