• 제목/요약/키워드: Diffuser flow

검색결과 425건 처리시간 0.03초

천음속 원심압축기의 공력설계 및 수치해석 (Aerodynamic Design and Numerical Analysis on a Transonic Centrifugal Compressor)

  • 최재호
    • 한국추진공학회지
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    • 제12권4호
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    • pp.56-62
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    • 2008
  • 가스터빈에 적용되는 천음속 원심압축기에 대한 공력설계 및 수치해석을 수행하였다. 평균유선법과 준삼차원 해석을 기반으로 공력설계를 수행하고, 레이놀즈 평균 나비어-스톡스 해석을 통해 압축기 내부 유동장을 해석하였다. 천음속 압축기에서 정압계수, 스월 파라미터 및 블레이드 공력하중 등 주요 공력파라미터들에 대한 분석과 임펠러와 디퓨저 내부 유동장에 대한 고찰이 이루어졌다.

볼류트 원심펌프의 스파이럴 케이싱 - 단면 형상의 영향 - (Spiral Casing of a Volute Centrifugal Pump - Effects of the Cross Sectional Shape -)

  • 진현배;김명진;손창호;정의준
    • 한국유체기계학회 논문집
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    • 제16권4호
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    • pp.28-34
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    • 2013
  • Centrifugal pump consists of a axis, a impeller and a spiral casing. The impeller is the most important component in centrifugal pump. But to minimize flow loss in discharge passage including spiral casing, the shape of spiral casing is very important also. So, to investigate the effect of shape of the spiral casing on performance curve of pump, the characteristics of spiral casing were studied through numerical analysis for centrifugal pump used on industry field. From the results the rectangular model was showed more loss than the others because of asymmetric flow field.

워터제트의 임펠러 입구와 출구 각도에 따른 성능해석 (Performance Analysis based on Impller Inlet & Outlet Angle for Waterjet)

  • 강민규;박동진;강한빈;이석순
    • 항공우주시스템공학회지
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    • 제5권2호
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    • pp.27-32
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    • 2011
  • The purpose of this study was to suggest 10 kinds of case and perform Mixed-flow pump optimum design and performance analysis depending on the shape of the impeller for suitable to water jet propulsion system. H20 was applied to the material properties, to analysis conditions for water jet axial impeller 1000 rpm given analysis was performed. Interpretation for each case as a result of speed, pressure, flow rate, calculate the thrust at the Inlet Angle $30^{\circ}$ and Outlet Angle $30^{\circ}$ could see a persistence of optimal performance.

Bubble plume의 중첩효과가 저수지 성층파괴 효율에 미치는 영향에 대한 수리동역학적 2상-3차원 평가 (Evaluation of Destratification Efficiency by Combined Effect of Adjacent Plumes through 2-Phase and 3D Hydrodynamic Analysis in a Stratified Fluid)

  • 염경택;박희경;안제영
    • 한국수자원학회논문집
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    • 제37권3호
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    • pp.219-231
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    • 2004
  • 수중폭기장치로 저수지 성층을 파괴시켜 저수지 수질을 개선시키기 위한 방법이 최근 널리 이용되고 있다. 본 연구는 주요 성층 파괴기작인 Bubble Plume(공기 부력류)의 수리동역학적 거동특성과 플륨 간격에 따라 변하는 모멘텀 중첩효과가 성층파괴 효율에 어떠한 영향을 미치는지에 대하여 수행하였다. 이를 위해 전산유체(CFD) 소프트웨어를 이용한 2상(공기-물) 3차원의 탈성층모델을 개발했으며, 이로부터 계절에 따라 변하는 다양한 성층강도와 주입 공기량에 따라 변하는 비정상상태의 성층파괴 발달과정은 물론 최적 탈성층 효율을 갖는 플륨간격을 제안할 수 있었다. 모델검증을 위한 실험을 위해 대형 실험조를 개발했으며, 온도성층은 소금물을 이용했던 기존연구와는 달리 가열순환수를 이용한 자연성층을 재현시켜 수행하였다. 연구결과 탈성층 효율은 디퓨서 배치간격에 크게 영향을 받는 것으로 밝혀졌으며, 플륨간격이 수심의 약 1.5배 이내익 때 중첩영향이 강하게 일어났고, PN가 클수록 간격에 영향을 상대적으로 크게 받았다. 또한, 간격이 수심보다 작곤 때는 효율이 PN에 비례해서 선형적으로 증가한 반면 그 이상에서는 효율이 상대적으로 감소하면서 비선형적으로 증가하는 현상을 밝혀냈다. 이상의 연구결과를 통해 주입공기량은 PN가 약 1000, 디퓨서 배치간격은 수심의 1.5배일 때가 최적의 성층파괴 조건인 것으로 나타났다.

진공청소기 원심홴의 유동과 소음원 해석 (An Alysis of Flow and Noise Source for Vacuum Cleaner Centrigugal Fan)

  • 전완호;유기완;이덕주;이승갑
    • 소음진동
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    • 제7권1호
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    • pp.99-106
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    • 1997
  • Centrigugal fans are widely used due to their ability to achieve relatively high pressure ratios in a short axial distance compared to axial fans. Because of their widespread use, the noise generated by these machines causes one of serious problems. In general, centrigugal fan noise is often dominated by tones at BPF(blade passage frequency) and its higher harmonics. This is a consequence of the strong interaction between the periodic flow discharged radially from the impeller and the stator blades or the cutoff. But in vacuum cleaner fan the noise is dominated by not only the discrete tones of BPF but also broadband frequencies. In this study we investigate the mechanism of broadband noise and predict for the unsteady flow field and the acoustic pressure field associated with the centrifugal fan. DVM(discrete vortex method) is used to calculates the flow field and the Lowson's method is used to predict the acoustic pressures. From the results we find that the broadband noise of a circular casing centrifugal fan is due to the unsteady force fluctuation around the impeller blades related to the vortex shedding. The unsteady forces associated with the shed vortices at impeller and related to the interactions to the diffuser and the exit.

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${\cdot}$출구 위치 변화에 따른 압전 구동방식 마이크로 펌프의 성능특성에 관한 수치해석적 연구 (A Numerical Study on the Performance Characteristics of a Piezoelectric Micropump for Different Inlet and Outlet Positions)

  • 김동희;정진;김창녕
    • 설비공학논문집
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    • 제17권1호
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    • pp.33-38
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    • 2005
  • This study has been conducted to investigate flow characteristics of a micropump with piezoelectric materials. In this study, the change of flow rates has been investigated for different positions of the inlet and outlet and for different distances between them. The FSI(Fluid Structure Interaction) method has been employed for numerical analysis of the piezoelectric diffuser/nozzle based micropump. It has been found that time averaged flow rate is greater in the case that distance between the inlet and outlet is longer. For the cases where the positions of the inlet are different with the position of the fixed outlet at the center, the flow rate is increased as the inlet is located farther from the center. This study may supply fundamental understandings for the design and analysis of the prototypes of piezoelectric micropumps.

급기가 프란시스 수차의 수압 맥동에 미치는 영향 (Effect of Air Admission on Pressure Pulsation in a Francis Turbine)

  • 전윤흥;박시훈;최한수;박준관
    • 신재생에너지
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    • 제10권4호
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    • pp.9-15
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    • 2014
  • In this study pressure and shaft torque pulsation were measured with variation of head and flow during the model test for a 15 MW Francis Turbine. Pressure pulsations were measured at the inlet of the spiral casing and 4 points in the cone of the diffuser and shaft torque pulsation at the upper position of the turbine. The maximum amplitude of pressure pulsation appeared 2.03% of the maximum rated head with the frequency of 25% of the rated revolution and at the guide vane opening of $10^{\circ}$. Shaft torque pulsation appeared 0.01% of the rated shaft torque, fairly low value. Air was admitted through the cone and pressure pulsation gradually decreased with increase of air flow and kept nearly constant after 5% of the rated flow. A new Francis turbine of which specific speed is 115 m-kW had been designed to rehabilitate the old one and the model test was performed at EPFL. The commercial code, STAR-$CCM^+$ was used for numerical simulation of flow.

전자기 저항을 이용한 압전 구동방식 마이크로 펌프의 내부유동 특성과 펌핑성능에 대한 수치해석적 연구 (A Numerical Study on the Internal Flow Characteristics and Pumping Performance of a Piezoelectric-based Micropump with Electromagnetic Resistance)

  • 안용준;오세홍;김창녕
    • 한국정밀공학회지
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    • 제27권10호
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    • pp.84-92
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    • 2010
  • In this study a numerical analysis has been conducted for the flow characteristics and pumping performance of a piezoelectric-based micropump with electromagnetic resistance exerted on electrically conducting fluid. Here, electromagnetic resistance is alternately applied at the inlet and outlet with alternately applied magnetic fields in association with the reciprocal membrane motion of the piezoelectric-based micropump. A model of Prescribed Deformation is used for the description of the membrane motion. The internal flow characteristics and pumping performance are investigated with the variation of magnetic flux density, tube size, displacement of membrane and the frequency of the membrane. It turns out that the current micropump has a wide range of pumping flow rate compared with diffuser-nozzle based micropumps.

Liguid-gas Ejector의 구동성능 특성에 관한 연구 (A Study on the Characteristics of the Liquid-gas Ejector)

  • 박기태;김진화;정한식;정효민
    • 대한설비공학회:학술대회논문집
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    • 대한설비공학회 2008년도 하계학술발표대회 논문집
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    • pp.1047-1052
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    • 2008
  • The aim of this paper is that studies on the characteristics of the liquid-gas ejector. Could get data about various model using numerical analysis. Compare and analyze result that get by an experiment and numerical analysis. And studied Characteristics of the ejector. In this paper, Numerical analysis model is gotten divided according to each Throat ratio as three types. Each throat ratio is 0, 4 and 7.5. According to the result that analyze basic model, pressure became lower causing the volume flow rate increase. In CFD studies, Fixed volume flow rate by these result and analyzed ejector performance. As a result, there was no change of pressure to Throat's Enterance, and pressure became low while pass the throat. Since, pressure recovered while passing diffuser. The outer flow velocity did not change greatly to change of volume flow rate. This research expects that is utilized to data for performance elevation hereafter.

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고공시험설비에서 로켓엔진의 지상시험 플룸 거동 해석 (An Analysis on Plume Behaviour of Rocket Engine with Ground Condition at High Altitude Engine Test Facility)

  • 김성룡;이승재;한영민
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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    • pp.112-115
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    • 2017
  • 고공엔진시험설비에서 지상 시험 조건의 시험 가능 여부와 설비 안전 문제를 점검하고자 로켓 엔진 유동을 해석하였다. 진공 챔버를 개방한 상태에서 냉각수를 초음속 디퓨저로 분사하면서 엔진이 작동하는 상황이며, 2차원 축대칭과 플룸, 공기, 냉각수의 3원 혼합물로 가정하였다. 해석 결과 냉각수 유량 200 kg/sec까지 지상 조건 시험이 가능하였다. 그러나 시동 초기 플룸의 역류로 인해 진공 챔버가 고온에 노출되고, 동시에 냉각수 역류로 인해 진공 챔버 내부가 오염되었다. 따라서 충분한 단열 대책과 오염 회피를 위한 작업이 선행되어야 한다.

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