• 제목/요약/키워드: line jet

검색결과 170건 처리시간 0.032초

간헐탈진형 충격기류식 여과집진장치의 여과포 반사거리 예측 (Prediction of Off-line Type Pulse Air Jet Bag Filter Reflection Distance)

  • 손정삼;정용현;서정민
    • 한국환경과학회지
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    • 제32권11호
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    • pp.801-809
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    • 2023
  • The purpose of this study is to predict the reflection distance following to the pulsing pressure, total air supplying, filter bag size using numercial analysis techniques and use it as an efficient operation condition and economic data for off-line type pulse air jet bag filter. In this research, filtration area 6 m2 condition, calculate filter resistance coefficient for simulation through the main experiments using coke dust. Ansys fluent V19.0 apply to CFD simulation, and analysis pulsing characteristics about pulsing pressure, filtration velocity and nozzle diameter. The maximum reflecting distance of off-line type pulse air jet bag filter is 1,000 mm regardless of total air supplying at over the 42 L/m2 conditions, that indicates off-line type can extend filter bag length 1,000 mm than on-line type. In order to effective primary and secondary pulsing of off-line type pulse air jet bag filter, over the 5 bar of pulsing pressure and over the 42 L/m2 of total air supplying are needed.

Ink-Jet Printing of Conductive Silver Inks for Flexible Display Devices

  • Kim, Dong-Jo;Park, Jung-Ho;Jeong, Sun-Ho;Moon, Joo-Ho
    • 한국정보디스플레이학회:학술대회논문집
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    • 한국정보디스플레이학회 2005년도 International Meeting on Information Displayvol.II
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    • pp.1491-1494
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    • 2005
  • We have studied ink-jet printing method for patterning conductive line on flexible plastic substrates. Synthesized silver nano-particles of ${\sim}$20nm were used for the conductive ink and the printed patterns exhibit a smooth line whose linewidth is below 100 ${\mu}m$. This ink-jet printing technique can be applied to flexible displays and electronics.

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초음속 증기제트의 충돌하중 특성에 대한 수치해석 연구 (Numerical Analysis on the Characteristics of Supersonic Steam Jet Impingement Load)

  • 오세홍;최대경;박원만;김원태;장윤석;최청열
    • 한국압력기기공학회 논문집
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    • 제14권2호
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    • pp.1-10
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    • 2018
  • Structures, systems and components of nuclear power plants should be able to maintain safety even in the event of design-basis accidents such as high-energy line breaks. The high-pressure steam jet ejected from the broken pipe may cause damage to the adjacent structures. The ANSI/ANS 58.2 code has been adopted as a technical standard for evaluating the jet impingement load. Recently, the U.S. NRC pointed out the non-conservativeness of the ANSI/ANS 58.2, because it does not take into account the blast wave effect, dynamic behavior of the jet, and oversimplifies the shape and load characteristics of the supersonic steam jet. Therefore, it is necessary to improve the evaluation method for the high-energy line break accident. In order to evaluate the behavior of supersonic steam jet, an appropriate numerical analysis technique considering compressible flow effect is needed. In this study, numerical analysis methodology for evaluating supersonic jet impingement load was developed and verified. In addition, the conservativeness of the ANSI/ANS 58.2 model was investigated using the numerical analysis methodology. It is estimated that the ANSI jet model does not sufficiently reflect the physical behavior of under-expanded supersonic steam jet and evaluates the jet impingement load lower than CFD analysis result at certain positions.

차실내 Defrost 노즐 분류의 충돌각 변화에 따른 유동특성에 관한 실험적 연구 (An Experimental Study on the Flow Characteristics with the Impinging Angles of Defrost Nozzle Jet Inside a Vehicle Passenger Compartment)

  • 김덕진;김현주;노병준;이지근
    • 대한기계학회논문집B
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    • 제31권12호
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    • pp.1024-1032
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    • 2007
  • The flow characteristics with the impinging angles of defrost nozzle jet inside a commercial vehicle passenger compartment were investigated experimentally by using the two-dimensional duct-nozzle model. The shape of the nozzle contraction was designed according to the curved line of cubic equation to the vertical plan of the flow direction. The impinging angles, defined as the angle between nozzle axis and a vertical line to the windshield, were varied from the $0^{\circ}\;to\;80^{\circ}$. The mean velocity distributions, the half-widths, and the momentum distributions with the cases of both the free jet and the impinging jet onto the dummy windshield were measured. The impinging jet flows similarly with wall jet from $X/b_o=20$, and the impinging angle has an effect on the half-width of the impinging jet. The momentum distributions onto the windshield increased with the increase of impinging angle, and then their inflection point was observed around the impinging angle of $60^{\circ}$.

Fabrication of Conductive Patterns by Ink-Jet Prining of Copper Ink

  • Park, Bong-Kyun;Kim, Don-Jo;Jeong, Sun-Ho;Lee, Seul;Moon, Joo-Ho
    • 한국정보디스플레이학회:학술대회논문집
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    • 한국정보디스플레이학회 2006년도 6th International Meeting on Information Display
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    • pp.1382-1385
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    • 2006
  • We have studied ink-jet printing method for patterning of conductive line on flexible plastic substrates. Synthesized copper nano-particles of ${\sim}40\;nm$ were used for the conductive ink and the printed patterns exhibit a smooth line whose line width is about $100\;{\mu}m$.

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축열식 저 NOx 연소기의 배기가스 내부 재순환 유동에 대한 연구 (A Study on the Self Flue Gas Recirculating Flow of the Regenerative Low NOx Burner)

  • 김종규;강민욱;윤영빈
    • 한국연소학회:학술대회논문집
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    • 한국연소학회 2001년도 제23회 KOSCO SYMPOSIUM 논문집
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    • pp.17-26
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    • 2001
  • Self flue gas recirculation flow is an effective method for low NOx emission in the regenerative low NOx burner. The object of this study is to analyze the self flue gas recirculating flow by varying jet velocity of the combustion air. Fuel and air flow rates are fixed and combustion air jet nozzle diameters are 13, 6.5 and 5mm. The stoichiometric line is obtained from the concentration of the fuel using an acetone PLIF technique. It is found that the self flue gas recirculating flow is entrained into that line using a two color PIV technique. As the jet velocity of combustion air is increased, the flue gas entrainment rate into the stoichiometric line is increased. This result suggests that NOx emission can be reduced due to the effects of flue gas which is lowering the flame temperatures.

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축열식 저 NOx 연소기의 배기가스 내부 재순환 유동에 대한 연구 (A Study on the Self Flue Gas Recirculating Flow of the Regenerative Low NOx Burner)

  • 김종규;강민욱;윤영빈;동상근
    • 한국연소학회지
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    • 제6권1호
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    • pp.20-28
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    • 2001
  • Self flue gas recirculation flow is an effective method for low NOx emission in a regenerative low NOx burner. The object of this study is to analyze self flue gas recirculating flow by varying the jet velocity of the combustion air. Fuel and air flow rates are fixed and combustion air jet nozzle diameters are 13, 6.5 and 5mm. The stoichiometric line is obtained from the concentration of fuel using the acetone PLIF technique. It is found that self flue gas recirculating flow is entrained into that line using the two color PIV technique. As the jet velocity of combustion air is increased, the flue gas entrainment rate into the stoichiometric line is increased. This result suggests that NOx emission can be reduced due to the effects of flue gas lowering the flame temperature.

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2次元 亂流 Stepped Wall Jet 의 流動特性 (Flow Characteristics of Two-Dimensional Turbulent Stepped Wall Jet)

  • 부정숙;김경천;박진호;강창수
    • 대한기계학회논문집
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    • 제9권6호
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    • pp.732-742
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    • 1985
  • 본 논문에서는 이 2차원 재부착분류(본문에서는 stepped wall jet라 명명함) 유동장을 재부착상류 부분, 재부착점 근방, 재부착 이후의 재발전 벽면분류 지역의 세 영역으로 구분하여 재부착 길이, 평균속도, 벽면정압을 측정하고 on-line에 의한 디지 틀 데이터 처리기법을 이용하여 난류강도, 레이놀즈 전단응력, 속도의 3승적(triple velocity product), integral length scale, Taylor's microscale 등을 실험적으로 구 하여 재부착 상류 부분에서는 자유분류와 비교하고, 재부착 이후에서는 2차원 벽면분 류와 비교하기로 한다.그리하여 초기 교란을 받는 분류가 벽면에 재부착하여 2차원 벽면분류로 재발전되어 가는 과정에 있어서의 평균 유동장과 급격한 변화를 갖는 난류 특성을 상세히 조사하여, 보다 일반적으로 적용될 수 있는 난류모델을 개발함에 있어 서 실험적인 자료를 제공하고자 한다. Fig. 1은 본 실험의 유동장에 대한 개약도를 보여주고 있다.

직교류에서 난류제트로 유입되는 유량에 관한 고찰 (Characteristics of an Entrainment into the Turbulent Buoyant Jet in a Cross Flow)

  • 김형민;김은필
    • 대한기계학회논문집B
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    • 제23권3호
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    • pp.342-351
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    • 1999
  • A jet injected normally into a cross flow has been found to have the cross section of a horseshoe shape. It occurs by a twin vortex motion in the region downstream of the jet injection. Such a flow is inherently and highly three-dimensional and numerical calculations should play an important role. The three-dimensional momentum equations with buoyancy effect and energy equation are solved to obtain the velocity distributions, center-line trajectories, cross sectional shape and entrainment. The density difference is sufficiently small, so that the Boussinesq approximation is considered to be valid. The SIMPLE algorithm is applied in a staggered grid system of a calculational domain for the numerical method.