• 제목/요약/키워드: Gas Flow Rate

검색결과 2,391건 처리시간 0.035초

공기 중 메틸에틸케톤 제어를 위한 Pilot-Scale 흡수 시스템의 운영인자 분석 (Analysis of Operation Parameters of Pilot-Scale Packed-Absorption System for Airborne Methyl Ethyl Ketone Control)

  • 조완근;김왕태
    • 한국환경과학회지
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    • 제20권4호
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    • pp.501-509
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    • 2011
  • Unlike many laboratory-scale studies on absorption of organic compounds (VOCs), limited pilot-scale studies have been reported. Accordingly, the present study was carried out to examine operation parameters for the effective control of a hydrophilic VOC (methyl ethyl ketone, MEK) by applying a circular pilot-scale packed-absorption system (inside diameter 37 cm ${\times}$ height 167 cm). The absorption efficiencies of MEK were investigated for three major operation parameters: input concentration, water flow rate, and ratio of gas flow-rate to washing water amount (water-to-gas ratio). The experimental set-up comprised of the flow control system, generation system, recirculation system, packed-absorption system, and outlet system. For three MEK input concentrations (300, 350, and 750 ppm), absorption efficiencies approached near 95% and then, decreased gradually as the operation time increased, thereby suggesting a non-steady state condition. Under these conditions, higher absorption efficiencies were shown for lower input concentration conditions, which were consistent with those of laboratory-scale studies. However, a steady state condition occurred for two input concentration conditions (100 and 200 ppm), and the difference in absorption efficiencies between these two conditions were insignificant. As supported by an established gas-liquid absorption theory, a higher water flow rate exhibited a greater absorption efficiency. Moreover, as same with the laboratory-scale studies, the absorption efficiencies increased as water-to-gas ratios increased. Meanwhile, regardless of water flow rates or water-to-gas ratios, as the operation time of the absorption became longer, the pH of water increased, but the elevation extent was not substantial (maximum pH difference, 1.1).

액체로켓 추진제 공급계에서 캐비테이션 벤튜리의 유량 제어 특성 (Flow Rate Control Characteristics of a Cavitating Venturi in a Liquid Rocket Propellant Feed System)

  • 조원국;문윤완;권오성;조인현
    • 한국항공우주학회지
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    • 제30권6호
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    • pp.46-52
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    • 2002
  • 액체로켓 추진제 공급장치에 정착된 캐비테이션 벤튜리의 유량 제어 특성을 해석하였다. 해석에는 실험과 수치해석이 병행되었으며 캐비테이션이 존재하는 유동에서 두 결과의 유량 차이는 약 10%로 나타났다. 벤튜리 상류의 압력을 $22.8{\times}10^5$pa로 일정하게 유지하고 하류의 압력을 변동시켰을 때 $3{\times}10^5$pa 이상의 압력 차이에 대하여 유량이 증가하지 않음을 확인하였다. 비응축 기체의 농도 변화에 의하여 벤튜리 내부에 발생하는 증기의 분포는 크게 달라지지만 유량은 같은 수준이 유지되어 비응축 기체의 농도가 1.5PPM에서 150PPM로 커질 경우, 유량이 약 2% 감소하였다. 이는 작동유체가 포함하고 있는 비응축 기체의 팽창과 생성된 증기가 압력 회복을 저해하는 영향이 유사하기 때문으로 풀이된다.

HNx 분위기가스중에서 BAF소둔시 코일의 온도변화에 관한 연구 (A Study on Temperature Variation of Coil on BAF Annealing in HNx Atmospheric Gas)

  • 전언찬;김순경
    • 대한기계학회논문집
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    • 제18권5호
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    • pp.1227-1234
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    • 1994
  • A cold spot temperature control system for the batch annealing furnace has been established in order to reduce energy consumption which is essential to improve productivity and stabilize the properties of products. A relationship between annealing cycle time and gas flow rate is developed and also for the variation of coil cold spot temperature with time during heating, and actual temperature measurements at mid-width of each coil during soaking. The results of the temperature variation effect on the cold rolled steel sheet batch annealing are as follows. (1) Cooling rate increasing gradually with increasing atmospheric gas flow, but heating rate is hardly increasing without atmospheric gas component change. (2) In case of short time heating, the slowest heating part is the center of B coil and in case of ling time heating, the low temperature point moves from the center of coil to inside coil. (3) The outside of top coil is the highest temperature point under heating, which becomes the lowest temperature point under cooling. (4) Soaking time determination depends on the input coil width, and soaking time for quality homogenization of 1214 mm width coil must be 2 hours longer than that of 914 mm width coil.

진공 열 플라즈마 용사공정을 통한 NiTiZrSiSn 벌크 비정질 코팅 형성 (Vacuum Plasma Sprayed NiTiZrSiSn Coating)

  • 윤상훈;김준섭;김수기;이창희
    • Journal of Welding and Joining
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    • 제25권4호
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    • pp.42-48
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    • 2007
  • An inert gas atomized NiTiZrSiSn bulk metallic glass feedstock was sprayed onto the copper plate using vacuum plasma spraying process. In order to change the in-flight particle energy, that is, thermal energy, the hydrogen gas flow rate in plasma gas mixture was increased at the constant flow rate of argon gas. Coating and single pass spraying bead were produced with the least feeding rate. Regardless of the plasma gas composition, fully melted through unmelted particle could be observed on the overlay coating. However, the frequency of the unmelted particle number density was increased with the decrease of the hydrogen gas flow rate. The amorphous phase fraction within coating was also affected by the number density of the unmelted particle.

Immune Based Intelligent Tuning of the 2-DOF PID Controller for Thermal Power Plant

  • Kim, Dong-Hwa
    • 제어로봇시스템학회:학술대회논문집
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    • 제어로봇시스템학회 2002년도 ICCAS
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    • pp.101.3-101
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    • 2002
  • Contents 1 Abstract- In the thermal power plant, there are six manipulated variables; main steam flow, feedwater flow, air flow, spray flow, fuel flow, and gas recirculation flow. Therefore, the thermal power plant control system is a multi-input and output system. In the control system, the main steam temperature typically is regulated by the fuel flow rate and the spray flow rate, and the reheater steam temperature is regulated by the gas recirculation flow rate. Up to the present time, the PID controller has been used to operate this system. This paper focuses on the characteristic comparison of the PID controller, the modified 2-DOF PID Controller on the DCS, in order to design an optimal...

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High Speed Etching for Saw Damage Removal Using by RF DBD

  • 고민국;양종근;이헌주
    • 한국진공학회:학술대회논문집
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    • 한국진공학회 2013년도 제45회 하계 정기학술대회 초록집
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    • pp.139.2-139.2
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    • 2013
  • 6" Multi-crystal Silicon wafer has etched suing a remote - type RF Dielectric barrier discharge (RF DBD) at atmospheric pressure. DBD source is composed of Al electrode and coated Al2O3 dielectric as function of Ar/NF3 gas combination and input power used 13.56 MHz power supply. Ar gas flow rate is changed from 2 to 10 Slm, and NF3 flow rate is changed from 0.2~1 slm. At the result, NF3 flow rate Si etching rate also increase whit the increasing of NF3 flow rate But at 2 slm etching rate was decrease. In this experience, Max etching rate is 2.3 ${\mu}m/min$ when the scan time is 45 sec.

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PECVD 기법에 의해 제조된 nc-Si : H 박막의 나노 구조적 특성 (Nanostructural Features of nc-Si : H Thin Films Prepared by PECVD)

  • 심재현;정수진;조남희
    • 한국결정학회지
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    • 제14권2호
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    • pp.56-61
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    • 2003
  • Nanocrystalline hydrogenated silicon (nc-Si : H) thin films were deposited at room temperature by plasma enhanced chemical vapor deposition (PECVD): a mixture of SiH₄ and H₂ gas was introduced into the evacuated reaction chamber. When the H₂ gas flow rate was low, the density of Si-H₃ bonds was high in the films. On the other hand, when the H₂ gas flow rate was high, e.g., 100 sccm, a large number of Si-H bonds contributed to the passivation of the surface of the large volume of Si nanocrystallites. The relative fraction of the Si-H₃ and Si-H₂ bonds in the amorphous matrix varied sensitively with the H₂ gas flow rate. The variation was associated with the change in the intensity as well as the wavelength of the main PL peaks, indicating the change in the total volume as well as the size of the Si nanocrystallites in the films.

압축기 설계조건이 가스터빈 엔진의 탈설계점 성능에 미치는 영향 (The Effects of Compressor Design Conditions on the Off-Design Performance of a Gas Turbine Engine)

  • 강동진;정평석;안상규
    • 대한기계학회논문집
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    • 제18권9호
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    • pp.2413-2422
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    • 1994
  • The effects of compressor design conditions on the off-design performance of a single-shaft gas turbine engine have been studied. Three different geometric design conditions are considered and three different values for the specific mass flow rate at the inlet to the compressor are assumed. For each of nine compressor design, the off-design performance of the gas turbine engine is predicted using the method previously proposed by present authors. Results show that the predicted off-design performances are quite different from each other even though they have the same performance at design point: it means that compressor design conditions should be determined in consideration of the off-design performance of the engine. The specific mass flow rate at the inlet to the compressor is also shown that it might be optimized with respect to the net power of the engine.

Pyrolytic Carbon Coating on A Simulated Fuel by Fluidized Bed Type Chemical Vapour Deposition

  • Park, Y.;Kim, Bong G.;Lee, Young W.;Dong S. Sohn
    • 한국원자력학회:학술대회논문집
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    • 한국원자력학회 1997년도 춘계학술발표회논문집(2)
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    • pp.159-164
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    • 1997
  • Pyrolytic carbon layer was coated on A1203 balls by fluidized bed type chemical vapour deposition unit to develop the coating technology for the preparation of coated nuclear fuel. The deposition was carried out at the temperature ranges between 110$0^{\circ}C$ and 130$0^{\circ}C$ with various gas contents and flow rates. Source and carrier gas were propane and argon, respectively. X-ray analysis shows that the deposition layer was typical carbon spectra. The growth rate of carbon layer depended on the amount of source gas and the deposition temperature. For the alumina balls with 2mm in diameter, the deposition rate was 11${\mu}{\textrm}{m}$/hr in the flow gases containing 30% source gas at 130$0^{\circ}C$ with a total flow rate of 2.0$\ell$/min. Microstructural observation of the deposits with scanning electron microscope revealed that the deposits had relatively dense and isotropic structure. Chemical analysis by energy dispersive spectroscopy showed that the layer was pure carbon.

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LNG 연료를 이용한 가스 터빈 연소기의 연소유동 해석 (Analysis of Combustion Flow of LNG-Fueled Gas Turbine Swirl Burner)

  • 김태호;강기하;최정열;김성철
    • 한국연소학회지
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    • 제13권3호
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    • pp.33-40
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    • 2008
  • Two- and Three- dimensional numerical simulations are carried out to understand the combustion characteristics of LNG-fueled gas turbine combustor for power generation using imported and domestic natural gases. Reacting flow characteristics of the swirl stabilized natural gas combustor were understood from the numerical results with the flow conditions selected from the gas turbine operation data. The thermal influences of different natural gases were very small and the fuel composition and flow rate were considered to be tuned well. The flow structures of the recirculation and combustion region was understood from the comparison of the two- and three-dimensional results. The complexity of the three-dimensional swirl flows inside the gas turbine combustor with multiple swirlers was understood those resulting from the interactions of the stage and pilot burners.

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