• 제목/요약/키워드: Gas temperature

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가스의 배경 온도 차이(방사율)가 OGI(Optical Gas Image)의 선명도에 미치는 영향 (Effects of Gas Background Temperature Difference(Emissivity) on OGI(Optical Gas Image) Clarity)

  • 박수리;한상욱;김병직;홍철재
    • 한국가스학회지
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    • 제21권5호
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    • pp.1-8
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    • 2017
  • 현재 산업현장의 가스 안전관리는 접촉식은 LDAR(Leak Detection and Repair), 비접촉식은 레이저 메탄검지기와 IR 카메라를 사용하고 있다. LDAR 방식은 전체 관리를 하는데 많은 인력과 소요시간이 들고, 관리자가 측정을 위해 가까이 접근해야 하므로 안전의 위협을 받을 수 있어 비접촉식이 더 효율적이다. 비접촉식에서 IR(infrared)을 이용한 가스 측정 방안에 대한 연구가 주목받고 있다. 산업 가스 중 메탄가스를 활용하여 측정 거리에 따라 가스 분출량을 변화시켜 OGI(optical gas image)를 촬영하였다. 본 논문은 가스의 배경온도차이가 OGI 의 선명도에 미치는 영향을 확인하기 위한 실험이다. OGI를 통해 가스의 구름모형을 정확하고, 선명하게 보기 위하여 배경온도 조절판을 제작하였다. 배경온도 조절판을 통해 배경온도와 대기온도 차이가 ${\Delta}T0^{\circ}C$일 때 보다 ${\Delta}T-6^{\circ}C$ 차이의 낮은 온도 조건으로 OGI 촬영을 한 결과가 육안을 확인하였을 때 더 선명한 차이가 나타났다. 선명도 차이의 객관성을 부여하기 위하여 추가로 MATLAB 의 RGB 분석법으로 확인한 결과, ${\Delta}T$$-6^{\circ}C$ 일 경우 RGB 값의 수치가 약 20% 낮게 나왔다. 배경온도가 대기온도보다 $-6^{\circ}C$ 낮을 때 더 선명하게 보이는 것은 총 복사법칙으로 설명이 가능하다. 가스의 배경온도가 대기온도에 비해 낮게 될 때 OGI 렌즈로 들어오는 가스의 복사에너지가 증가되어 가스가 더 선명하게 보이게 된다.

Effect of the Stagnation Temperature on the Normal Shock Wave

  • Zebbiche, Toufik
    • International Journal of Aeronautical and Space Sciences
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    • 제10권1호
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    • pp.1-14
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    • 2009
  • When the stagnation temperature increases, the specific heat does not remain constant and start to vary with this temperature. The gas is perfect, it's state equation remains always valid, except, it was called by gas calorically imperfect or gas at high temperatures. The purpose of this work is to develop a mathematical model for a normal shock wave normal at high temperature when the stagnation temperature is taken into account, less than the dissociation of the molecules as a generalisation model of perfect for constant heat specific. A study on the error given by the perfect gas model compared to our model is presented in order to find a limit of application of the perfect gas model. The application is for air.

세라믹 열교환기의 성능평가를 위한 실험적 연구 (An Experimental Study for Performance Evaluation of a Ceramic Heat Exchanger)

  • 최현수;신동훈
    • 한국연소학회지
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    • 제16권1호
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    • pp.46-51
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    • 2011
  • Exhaust gas of an industrial furnace used at such as metallurgy or ceramic manufacturing usually contains thermal energy with high temperature which can be recycled by heat exchanger. However, when the temperature of the exhaust gas is high such as more than $1,000^{\circ}C$, ordinary metallic heat exchanger cannot fully recover the heat due to the limitation of operating temperature depending on the material property. In the present study, a compact ceramic heat exchanger of cross flow type is introduced and evaluated by heat exchange rate and operating temperature. The ceramic heat exchanger can endure the gas temperature more than $1,300^{\circ}C$, and its volumetric heat exchanging rate exceeds 1 MW/$m^3$. The experimental data is also compared with the previous numerical result which shows reasonable agreement. Meanwhile, the gas leakage rate is measured to be about 3~4%, and heat loss to environmental air is about 23~26% of the fuel energy.

배기 가스 유량 제어를 이용한 버너방식 디젤 입자상물질 제거 장치의 재생 (Regeneration of Burner Type Diesel Particulate Trap System Through Active Exhaust Gas Feeding)

  • 김재업;박동선;이만복;김응서
    • 한국자동차공학회논문집
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    • 제5권1호
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    • pp.1-13
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    • 1997
  • The key point that guarantees the durability of the ceramic monolith filter is to lower peak temperature and temperature gradient inside filter during regeneration. The control of the exhaust gas flow rate into the filter, by the bypass technique of the exhaust gas, enables the gas temperature in filter to be constant for regeneration. A couple of methods, which are the ON/OFF and PID control of the bypass valve, were used for feedback control of the gas temperature. These techniques showed that the ceramic filter was regenerated perfectly under the peak temperature and peak temperature gradient limitations for durability.

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Supersonic Axisymmetric Minimum Length Nozzle Conception at High Temperature with Application for Air

  • Zebbiche, Toufik
    • International Journal of Aeronautical and Space Sciences
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    • 제9권1호
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    • pp.1-30
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    • 2008
  • When the stagnation temperature of a perfect gas increases, the specific heats and their ratio do not remain constant any more and start to vary with this temperature. The gas remains perfect; its state equation remains always valid, except, it is named in more by calorically imperfect gas. The aim of this work is to trace the profiles of the supersonic axisymmetric Minimum Length Nozzle to have a uniform and parallel flow at the exit section, when the stagnation temperature is taken into account, lower than the dissociation threshold of the molecules, and to have for each exit Mach number and stagnation temperature shape of nozzle. The method of characteristics is used with the algorithm of the second order finite differences method. The form of the nozzle has a point of deflection and an initial angle of expansion. The comparison is made with the calorically perfect gas. The application is for air.

분광학적 방법에 의한 Plasma Jet의 온도분석 측정 (Spectroscopic Measurement of Temperature Distribution in Some Plasma Jets)

  • 전춘생;박용관;임명선
    • 전기의세계
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    • 제26권2호
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    • pp.104-110
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    • 1977
  • This paper investigates temperature distribution of plasma jets which used argon gas, and nitrogen gas mixed with argon as working fluids in spectroscopic method, and studies correlations between them main results are as follows; 1) The temperature at the center of plasma jet increases with are current and gas flow, and decreases with magnetic flux density along the axial direction. 2) The changing rate of temperature of plasma jet in the radial direction decreases rapidly beyond 2mm from central axis. 3) Temperature drop rate of plasma jet in the central axis direction appears most apparant beyond 13mm above the nozzle exit. 4) When argon gas mixed with a small amount of nitrogen, plasma temperature increases at same are current compared with the case of argon gas only.

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레이저흡수분광을 이용한 난류유동 배기가스 온도장 실시간 분석 연구 (Real-time Analysis of Exhaust Gas Temperature Field in Turbulent Flow Using Laser Absorption Spectroscopy)

  • 최두원
    • 열처리공학회지
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    • 제37권2호
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    • pp.73-78
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    • 2024
  • This study presents a real-time method that uses Laser Absorption Spectroscopy (LAS) to measure exhaust gas temperatures in turbulent flow fields. It was possible to measure temperature by passing a laser beam through the exhaust gas in a grid pattern, and obtain a temperature distribution image through time series analysis at 0.1 second intervals. Temperature image resolution has been improved with CT reconstruction algorithms. Estimating maximum temperature values and locations enabled 2D temperature analysis, surpassing single-point methods like thermocouples. The accuracy of LAS measurements was evaluated by comparison with thermocouple measurements. This approach will contribute to automotive technology and environmental protection by providing reliable temperature data for interpreting turbulent temperature distributions.

열건조기내에서 슬러지 입자의 증발현상에 관한 수치해석 연구 (A Numerical Study on Evaporation of Sludge Particles in a Sludge Dryer)

  • 구본기;김상수
    • 대한기계학회논문집B
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    • 제22권8호
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    • pp.1064-1072
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    • 1998
  • The evaporation of sludge particles in a sludge dryer has been numerically investigated with commercial CFX4.1 code. Gas flow field, gas temperature field, sludge particle trajectories, and the moisture content variation of sludge particles are calculated fort various influencing factors, i. e., gas swirl velocity, initial particle distribution, gas temperature. Evaporation of sludge particles increases with gas swirl velocity, several supplying positions, and gas temperature, respectively due to increased residence time, increased contacting surface area, and increased temperature difference between gas and particle.

온도 변화에 대한 Q.C.M.의 가스 반응 특성 (Gas Response Properties of Q.C.M. for Various Temperature)

  • 진철남;김경환;강현욱;유승엽;박재철;권영수
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 하계학술대회 논문집 D
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    • pp.1503-1505
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    • 1998
  • Stearic acid was deposited on surface of 9[MHz], AT-cut quartz crystal microbalance as gas sensing material using Langmuir-Blodgett(LB) technique. We measured gas response between deposited LB films and organic gas for various temperature($0{\sim}80^{\circ}C$). The resonant frequency changed due to absorbance of organic gas such as methanol and butanol gas at room temperature. However, the resonant frequency not responded to methanol gas at temperature above melting point of deposited LB films.

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Gas-lift를 이용한 극저온 추진제의 재순환 성능에 대한 실험 (Experimental Study on Cryogenic Propellant Circulation using Gas-lift)

  • 권오성;이중엽;정용갑
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.551-554
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    • 2006
  • Inhibition of propellant temperature rising in liquid propulsion rocket using cryogenic fluid as a propellant is very important. Especially propellant temperature rising during stand-by after filling and pre-pressurization can bring into cavitation in turbo-pump. One of the method preventing propellant temperature rising in cryogenic feeding system is recirculating propellant through the loop composed of propellant tank, feed pipe, and recirculation pipe. The circulation of propellant is promoted through gas-lift effect by gas injection to lower position of recirculation pipe. In this experiment liquid oxygen and gas helium is used as propellant and injection gas. Under atmospheric and pressurized tank ullage condition, helium injection flow-rate is varied to observe the variation of recirculating flow-rate and propellant temperature in the feed pipe. There is appropriate helium injection flow-rate for gas-lift recirculation system.

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