• Title/Summary/Keyword: jet pump

검색결과 102건 처리시간 0.023초

해상용 원심펌프 임펠러의 침식억제법으로 음극방식 및 재료개발에 관한 기초연구(2) (Fundamental Study on Cathodic Protection and Material Development as Erosion-Control Methods of Oceanic Centrifugal Pump(2))

  • 이진열;임우조;오인호
    • Journal of Advanced Marine Engineering and Technology
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    • 제20권2호
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    • pp.92-92
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    • 1996
  • Recently, with the rapid development in the oceanic systems such as the oceanic structures and vessel, there occurs much interest in the impingement erosion-corrosion. In this paper, Cu-metal was tested by using of erosion apparatus with water-jet type and was investigated under the behaviour of impingement erosion-corrosion according to various environmental conditions, and the properties of Cu-metal were evaluated through the measurement by weight loss, weight loss rate, protective efficiency. The results were compared with those obtained using Cu-metal applied to cathodic protection and Cu-alloys added to Zn or Al-metal. As a basis of those results, the best protective efficiencies could be taken as using cathodic protection method and Cu-alloy with Al & Zn material addings, and will be suggested as the fundamental data of the anti-impingement erosion-corrosion on Cu-metal of impeller material for oceanic centrifugal pump.

해상용 원심펌프 임펠러의 침식억제법으로 음극방식 및 재료개발에 관한 기초연구 (2) (Fundamental Study on Cathodic Protection and Material Development as Erosion - Control Methods of Oceanic Centrifugal Pump(2))

  • 이진열;임우조;오인호
    • Journal of Advanced Marine Engineering and Technology
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    • 제20권2호
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    • pp.24-31
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    • 1996
  • Recently, with the rapid development in the oceanic systems such as the oceanic structures and vessel, there occurs much interest in the impingement erosion-corrosion. In this paper, Cu-metal was tested by using of erosion apparatus with water-jet type and was investigated under the behaviour of impingement erosion-corrosion according to various environmental conditions, and the properties of Cu-metal were evaluated through the measurement by weight loss, weight loss rate, protective efficiency. The results were compared with those obtained using Cu-metal applied to cathodic protection and Cu-alloys added to Zn or Al-metal. As a basis of those results, the best protective efficiencies could be taken as using cathodic protection method and Cu-alloy with Al & Zn material addings, and will be suggested as the fundamental data of the anti-impingement erosion-corrosion on Cu-metal of impeller material for oceanic centrifugal pump.

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Computational Study of the Axisymmetric, Supersonic Ejector-Diffuser Systems

  • Kim, Heuy-Dong;Lee, Young-Ki;Seo, Tae-Won;Raghunathan, Srinivasan
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2000년도 춘계학술대회논문집B
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    • pp.520-524
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    • 2000
  • A ejector system is one of the fluid machinery, which has been mainly used as an exhaust pump or a vacuum pump. The ejector system has often been pointed out to have only a limited efficiency because it is driven by pure shear action and the mixing action between primary and secondary streams. In the present work, numerical simulations were conducted to investigate the effects of the geometry and the mass flow ratio of supersonic ejector-diffuser systems on their mixing performance. A fully implicit finite volume scheme was applied to solve the axisymmetric Navier-Stokes equations, and the standard ${\kappa}-{\varepsilon}$ turbulence model was used to close the governing equations. The flow fields of the supersonic ejector-diffuser systems were investigated by changing the ejector throat area ratio and the mass flow ratio. The existence of the second throat strongly affected the shock wave structure inside the mixing tube as well as the spreading of the under-expanded jet discharging from the primary nozzle, and served to enhance the mixing performance.

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Pod형 물분사 추진장치 성능시험 연구 (Performance Test of Pod-type Waterjet Propulsion System)

  • 김기섭;송인행;안종우;문일성
    • 대한조선학회논문집
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    • 제34권4호
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    • pp.21-30
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    • 1997
  • 본 논문은 복합지지형 초고속선에 사용될 pod형 물분사 추진장치에 대한 예인수조 실험 및 성능해석 결과를 보여준다. 선체와 물분사 흡입구간의 상호작용이 매우 작은 것으로 가정하고 선체저항 및 추진성능 실험을 토대로 시험선 운항시 성능을 해석하였다. 축류식 펌프를 갖는 pod형물분사 추진장치를 설계하고 단독특성시험 시스템을 개발하여 실험을 수행하였다. 실험결과로부터 펌프 성능, 제트효율, 흡입구 및 노즐의 손실계수 등 물분사 추진장치 설계 및 특성파악에 유용한 자료를 확보하였다. 실험결과는 설계요구조건과 비교적 좋은 일치를 보여준다.

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Network Analysis of Engine Lubrication System

  • Chun, Sang-Myung;Park, Young-Hwan;Siyoul Jang
    • 한국윤활학회:학술대회논문집
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    • 한국윤활학회 2000년도 제31회 춘계학술대회
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    • pp.126-133
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    • 2000
  • A computer program for the analysis of engine lubrication systems has been developed. And a case study of a four cylinders gasoline engine is illustrated. This paper gives the mathematical models for oil flow through hydraulic tappet as well as the ones of oil jet and plain journal bearings. And the new from an oil pump and the flow resistance through an oil filter is considered at various temperatures. In the analysis, the various design guidelines are applied. The distribution of flow and pressure of an engine lubrication system are calculated, and the pressure data compared with the experimental data at a few points in the engine lubrication system. This method is helpful to design of engine lubrication system efficiently.

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스마트무인기 연료이송/공급 계통의 설계 및 성능분석 (Design and Performance Analysis of Fuel Feed and Fuel Transfer System for Smart UAV)

  • 이창호;이수철;최희주;김재무
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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    • pp.351-354
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    • 2006
  • PW206C 터보샤프트 엔진을 장착한 스마트무인기 연료시스템의 연료공급계통과 연료이송계통의 설계와 성능분석을 수행하였다. 연료공급계통은 엔진 연료입구에서의 최소압력과 최대압력 조건에 대한 성능분석을 통하여 엔진의 요구조건을 만족함을 확인하였다. 연료탱크간의 연료이송을 담당하는 제트펌프의 설계조건으로 비행체의 최대수평가속비행에서 ESDU와 Flowmaster 코드를 이용한 설계와 성능해석을 수행하였다.

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초고속 발사체의 액체 저장부 충돌에 의한 초음속 액체 제트의 분무 속도 및 분열 특성 (Spray Angle and Break-up Characteristics of Supersonic Liquid Jets by an Impinging Methods with High Speed Projectile)

  • 이인철;신정환;김희동;구자예
    • 한국가시화정보학회지
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    • 제9권1호
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    • pp.55-60
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    • 2011
  • Pulsed supersonic liquid jets injected into an ambient air are empirically studied by using a high pressure ballistic range system. Ballistic range systems which are configured with high-pressure tube, pump tube, launch tube and liquid storage nozzle. Experimental studies are conducted to use with various impact nozzle geometry. Supersonic liquid jets are generated by an impact of high speed of the projectile. High speed liquid jets are injected with M = 3.2 which pressure is 1.19 GPa. Multiple jets which accompany with shock wave and pressure wave in front of the jet were observed. The shock-wave affects significantly atomization process for each spray droplets. As decreasing orifice diameter, the averaged SMD of spray jets had the decreasing tendency.

Network Analysis of Engine Lubrication System

  • Chun, Sang Myung;Park, Young Hwan;Jang, Siyoul
    • KSTLE International Journal
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    • 제1권1호
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    • pp.21-28
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    • 2000
  • A computer program fur the analysis of engine lubrication systems has been developed. And a case study of a four cylinders gasoline engine is illustrated. This paper gives the mathematical models far oil flow through hydraulic tappet as well as those of oil jet and plain journal bearings. And the flow from an oil pump and the flow resistance through an oil filter is considered at various temperatures. In the analysis, the various design guidelines are applied. The distribution of flow and pressure of an engine lubrication system are calculated, and the pressure data compared with the experimental data at a few points in the engine lubrication system. This method is helpful to design of engine lubrication system efficiently.

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Numerical simulation of cavitating flow past axisymmetric body

  • Kim, Dong-Hyun;Park, Warn-Gyu;Jung, Chul-Min
    • International Journal of Naval Architecture and Ocean Engineering
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    • 제4권3호
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    • pp.256-266
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    • 2012
  • Cavitating flow simulation is of practical importance for many engineering systems, such as marine propellers, pump impellers, nozzles, torpedoes, etc. The present work has developed the base code to solve the cavitating flows past the axisymmetric bodies with several forebody shapes. The governing equation is the Navier-Stokes equation based on homogeneous mixture model. The momentum is in the mixture phase while the continuity equation is solved in liquid and vapor phase, separately. The solver employs an implicit preconditioning algorithm in curvilinear coordinates. The computations have been carried out for the cylinders with hemispherical, 1-caliber, and 0-caliber forebody and, then, compared with experiments and other numerical results. Fairly good agreements with experiments and numerical results have been achieved. It has been concluded that the present numerical code has successfully accounted for the cavitating flows past axisymmetric bodies. The present code has also shown the capability to simulate ventilated cavitation.

회전반사판을 이용한 건물 외벽청소로봇 개발방향 연구 (Fundamental Study of the Building Exterior wall cleaning Robot using a spinning device)

  • 박수열;김균태
    • 한국건축시공학회:학술대회논문집
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    • 한국건축시공학회 2013년도 추계 학술논문 발표대회
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    • pp.224-225
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    • 2013
  • Most of the building exterior wall cleaning robots use a water jet device for spraying water. However this method is sprayed excessive water usage than water quantity required for cleaning. And setting weight of the water pump cleaning device increase the weight of the building exterior wall cleaning robot. Therefor, this paper suggest that the mechanisms scatter minimal cleaning water using a spinning device of the building exterior wall cleaning robot.

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