• 제목/요약/키워드: Venturi Pump

검색결과 11건 처리시간 0.019초

LightGBM을 이용한 수력 펌프 유량 추정의 실험적 연구 (An Experimental Study on the Estimation Flow-rate of Venturi Pump Using LightGBM)

  • 정진범;이지환;강명철
    • 드라이브 ㆍ 컨트롤
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    • 제20권4호
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    • pp.123-132
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    • 2023
  • In disaster situations, to facilitate rapid drainage, electric underwater pumps are installed manually. This poses a high risk of electric shock accidents due to a short circuit, and a lot of time is required for hose connection and installation of electrical devices. To solve these problems, a Venturi pump using the venturi effect without external power is used. However, Venturi pumps that operate without external power make it difficult to install flow sensors such as electric devices; consequently, it is difficult to check the real-time flow rate. This paper proposes a flow estimation logic to replace the function of the flow sensor for the venturi pump . To develop the flow estimation logic, the flow characteristics of the venturi pump, according to the operating conditions, were checked. After that, the relationship with the flow rate of the venturi pump was defined using a pressure sensor corresponding to a low-cost sensor. Finally, an analysis of the estimation error was performed using the developed flow estimation logic.

정상상태에서 카뷰레터 더미모델의 스로틀 개도에 따른 압력특성 (The characteristics of suction pressure by throttle opening of the carburetor dummy at steady state)

  • 조형문;김병국;최영하;윤석주;한종규
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2008년도 춘계학술대회논문집
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    • pp.711-714
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    • 2008
  • The objective of this paper is to know the characteristics of pressure through a simplified typical carburetor used in small engines at the different throttle opening conditions. The carburetor is the device responsible for creating the right air-fuel mixture according to the different engine operating conditions. It is activated by the static or the dynamic pressure. The carburetor dummy is geometrically similar of LPG brush-cutter engine's diaphragm carburetor and is made of acrylic. Suction system gives body to crankcase vacuum using the vacuum pump and throttle opening conditions are controled by transfer device. Carburetor venturi throat and fuel charging tube diameter is each 20mm, 4.1mm. The result of the work presents an unprecedented phenomenon of suction pressure variation inside the carburetor venturi. It is predicted that these unprecedented pressure variation be caused by minor losses; sudden contraction or expansion, open or partially closed and so on.

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제트 폄프 요소 내부의 유동 해석 (Internal Viscous Flow Computation Within the Jet Pump Elements)

  • 조장근;오상욱;박원규;오세민;이수원
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 1996년도 춘계 학술대회논문집
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    • pp.99-104
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    • 1996
  • The jet pump is being used in many fields for several purposes because of its simple construction and easy operation. The characteristics of the geometrical variables, pressure gradient and velocity distribution of the jet pump are studied using the CFD technique. The flow calculations through a bended nozzle. a mixing chamber and a venturi are presented and phenomenological aspects are discussed. This study solve 3-D steady incompressible Navier-Stokes equations using the Iterative time marching scheme. The governing equations are differenced with 1st-order accurate backward difference scheme for the time derivatives and 3rd-order accurate QUICK scheme for the convective terms. The Mark-and-cell concept was applied efficiently to solve continuity equation, which is differenced 2nd-order accurate central differenced scheme. The 4th-order artificial damping is added to the continuity equation for numerical stability. A O-type of grid system is generated inside a nozzle and venturi of the jet pump. It has concluded that the results of present study properly agree with physical flow phenomena.

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버터플라이 밸브의 유량측정 불확도에 대한 영향 (Effect of a Butterfly Valve on the Uncertainty of Flow Rate Measurement)

  • 윤석호;이정호;유청환;박상진;정장환
    • 한국유체기계학회 논문집
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    • 제13권4호
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    • pp.18-24
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    • 2010
  • For testing large-capacity pumps, the accurate flow rate measurement is needed in the test loop. As a measuring method of flow rate, venturi tube is recommended due to its low pressure loss. However, upstream disturbance of loop component such as a valve has an effect upon the accuracy of flow rate measurement. For controlling flow rate in case of high flow rate and large-scale piping system, a butterfly-type valve is generally used due to its compactness. However, a butterfly valve disturbs downstream flow by generating turbulence, cavities, or abrupt pressure change. In this study, the effect of downstream disturbance of butterfly valve on the flow rate measurement using a venturi tube is investigated. Test loop consists of circulation pump, reservoir, butterfly valve, venturi tube, and reference flow meter. The test is conducted with regard to a different valve opening angle of butterfly valve. According to the valve opening angle, the uncertainty of flow rate measurement is investigated.

수리동력학적 캐비테이션을 이용한 하수 슬러지의 전처리-I: 전처리 시스템의 최적화 (Sludge Pre-Treatment by Hydrodynamic Cavitation-I: Optimization of Pre-Treatment System)

  • 맹장우;이은영;배재호
    • 대한환경공학회지
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    • 제32권12호
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    • pp.1119-1125
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    • 2010
  • 하수 슬러지의 혐기성 소화성을 향상시키기 위한 다양한 전처리 방법이 제시되어 있지만, 대부분 낮은 경제성 등의 문제로 현장 적용에 제한을 받고 있다. 본 연구는 장치의 구성 및 유지관리가 용이한 수리동력학적 캐비테이션 방법을 이용한 venturi cavitation system (VCS)의 전처리 효율을 향상시키기 위한 최적 설계 및 운전조건을 도출하기 위하여 수행하였다. VCS에서 벤츄리의 직렬 연결 개수는 3개일 때 가장 높은 전처리 효율을 나타내었고, 펌프는 흡입방식이 압송방식에 비하여 단위 에너지 투입량 당 1.6배 높은 전처리 효율을 나타내었다. 캐비테이션이 발생하는 조건에서 벤츄리의 목 직경 조합은 전처리 효율에 영향을 주지 않았다. 또한 3개의 벤츄리가 직렬로 연결된 벤츄리를 병렬로 설치할 경우 에너지 투입량 당 전처리 효율이 30% 향상되었다. 병렬 연결 운전조건으로 슬러지를 처리하였을 때, 에너지 소모량 당 가용화 효율은 5.6 mg ${\Delta}SCOD/g$ TS/kWh로 기존의 수리동력학적 전처리장치보다 우수하였다.

자흡방식에 의해 마이크로버블을 발생시키는 충돌 노즐에 대한 연구 (A Study on the Collision Nozzle for Generating Microbubble by Self-Suction Method)

  • 강우진;박상희;유성훈
    • 한국산업융합학회 논문집
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    • 제26권6_2호
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    • pp.1047-1053
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    • 2023
  • An experimental study was performed on the collision nozzle system that generates microbubble by air self-suction using a venturi nozzle. This study experimentally investigates the pressure of a pump and a dissolution tank, water flow rate, air self-suction amount and microbubble generation amount. The experimental conditions were varied by changing the diameter of the collision nozzle (de=4,5,6,7,8mm), the pumping power(0.5hp, 1.0hp) and the capacity of the dissolution tank(4.4L, 8/8L). The pressure change of the pump according to the outlet diameter of the collision nozzle showed that the 1.0hp pump power operated more stably than the 0.5hp pump. The pressure change in the dissolution tank was shown to decrease rapidly as the outlet diameter of the nozzle increased. The flow rate of recirculating water was shown to increase as the nozzle diameter increased. Additionally, it was shown that the pump capacity of 1.0hp increased the flow rate more than that of 0.5hp. The self-suction air flow rate was shown to occur above de=6mm, and the air flow rate increased as the nozzle diameter increased. Also, as the pump capacity increased, the self-suction amount of air increased. It was shown that the amount of microbubble less than 50mm generated was maximum when the nozzle diameter was 6mm, the pump power was 1.0hp, and the dissolution tank capacity was 8.8L.

Flow Instability of Cryogenic Fluid in the Downstream of Orifices

  • Thai, Quangnha;Lee, Chang-Jin
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2008년 영문 학술대회
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    • pp.413-418
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    • 2008
  • Flow instability in the rocket turbo pump system can be caused by various reasons such as valve, orifice and venturi, etc. The inception of cavitation, especially in the propellant feeding system, is the primary cause of the mass flow and pressure oscillation due to cyclic formation and depletion of cavitation. Meanwhile, the main propellant in liquid rocket engine is the cryogenic one, which is very sensitive to temperature variation, and the variation of propellant properties caused by thermodynamic effect should be accounted for in the flow analysis. The present study focuses on the formation of cryogenic cavitations by adopting IDM model suggested by Shyy and coworkers. Also, the flow instability was investigated in the downstream of orifice by using a developed numerical code. Calculation results show that cryogenic cavitations can lead to flow instability resulting in mass flow fluctuations due to pressure oscillations. And the prediction of cavitations in cryogenic fluid is of vital importance in designing feeding system of LRE.

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양액 자동조제용 액제 정밀계량 장치 개발 (Development of a Low -Cost and Precise Liquid Metering Device for Automatic Nutrient-Solution Control)

  • 이정훈;류관희;이규철
    • 한국농업기계학회:학술대회논문집
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    • 한국농업기계학회 1997년도 동계 학술대회 논문집
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    • pp.255-262
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    • 1997
  • A low-cost and precise metering device, which is suitable to automatic mixing of nutrient-solution for hydroponic culture, was developed for small-scale growers. The metering device was composed of three parts those were supply pumps, metering cylinders and venturi tube. Those parts were controlled by personal computer with time-based odoff control method. To verify the performance of the developed metering device, the relationship between operating time and discharge was examined and the accuracy of the developed metering device was compared with commercial metering pumps. The results of this study are as follows. 1. The correlation coefficient between the flow rate and operating time was 0.9999, and the linear regression equation computed was y=21.759x, where y is the discharge(g) and x is the operating time(s). 2. The developed device has greater accuracy than commercial metering pumps in terms of the full-scale error. Calculated errors for the developed metering device and two commercial pump were $\pm$0.3 %, $\pm$2.45 % and $\pm$1.38 % respectively. 3. Above results show developed metering device is a useful tool for nutrient-solution control system.

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극저온 유체의 공동 발생에 의한 오리피스 후류의 유동 불안정 (Flow instability of cryogenic fluid in the downstream of orifice)

  • 이세영;이창진
    • 한국항공우주학회지
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    • 제36권7호
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    • pp.695-702
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    • 2008
  • 액체 로켓 엔진의 연료 공급 시스템은 다양한 원인으로 인해 유동 불안정이 발생한다. 특히 연료 공급 시스템에서 발생하는 공동 현상은 공동의 생성과 소멸로 인해 후류 쪽의 압력 및 유량의 진동을 유발하게 된다. 액체 로켓은 주 추진제로 극저온 유체를 사용하게 되는데, 극저온 유체는 온도에 민감한 성질을 갖고 있기 때문에 공동 현상의 해석에 있어 온도 변화에 대한 효과를 반드시 고려해주어야 한다. 본 연구에서는 Shyy등이 제안한 “MUSHY IDM"모델을 이용하여 극저온 유체에서 발생하는 공동 현상을 모사하였다. 이를 바탕으로 오리피스에서 발생하는 공동 현상이 유동 불안정에 어떠한 영향을 미치는 지와 오리피스 형상 변화가 후류 유동의 불안정에 끼치는 영향을 연구하였다.

포 소화설비용 소화약제 혼합장치의 성능향상을 위한 정량 혼합특성에 관한 연구 (A Study on Foam Mixing Characteristics in Steady State to Enhance the Performance of Proportioner for Foam System)

  • 구재현
    • 한국방재학회 논문집
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    • 제9권5호
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    • pp.63-68
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    • 2009
  • 본 연구에서 물 흐름에 일정한 농도로 포 소화약제를 정확하게 혼합하는 포 소화설비용 소화약제 혼합장치의 성능향상을 위하여 포소화약제의 정량 혼합특성을 분석하였다. 펌프, 탱크, 압력계, 유량계, 노즐로 구성되는 성능평가 시스템을 사용하여 개발된 프로포셔너의 성능이 실험적으로 평가하였다. 결과적으로 라인프로포셔너의 포소화약제 혼합성능은 벤츄리 효과에 의한 물유량 증가와 오리피스 단면적 증가에 따라 증가하고 오차율 $\pm4%$이내의 범위에서 물 유량과 포소화약제 양의 혼합농도 3%의 성능을 보였다. 프레셔프로포셔너의 경우 물 유량 증가와 입구압력 증가에 따라 혼합성능이 증가하고 오차율 $\pm2%$이내의 범위에서 물 유량과 포소화약제 양의 혼합농도 3%의 성능으로 분석되었다.