• 제목/요약/키워드: impeller pump

검색결과 340건 처리시간 0.027초

연구용 원자로 냉각계통의 ASME 스트레이너 설계 및 성능시험 (Design and Test of ASME Strainer for Coolant System of Research Reactor)

  • 박용철;박종호
    • 한국유체기계학회 논문집
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    • 제2권3호
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    • pp.24-29
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    • 1999
  • The ASME strainers have been newly installed at the suction side of each reactor coolant pump to get rid of the foreign materials which may damage the pump impeller or interfere with the coolant path of fuel flow tube or primary plate type heat exchanger. The strainer was designed in accordance with ASME SEC. III, DIV. 1, Class 3 and the structural integrity was verified by seismic analysis. The screen was designed in accordance with the effective void area from the result of flow analysis for T-type strainer. After installation of the strainer, it was confirmed through the field test that the flow characteristics of primary cooling system were not adversely affected. The pressure loss coefficient was calculated by Darcy equation using the pressure difference through each strainer and the flow rate measured during the strainer performance test. And these are useful data to predict flow variations by the pressure difference.

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터보펌프 축추력 조절용 캐비티 베인에 대한 수치해석적 연구 (Numerical Study on the Effect of Cavity Vanes to Control the Axial Thrust of a Turbopump)

  • 최창호;김진한;노준구
    • 한국유체기계학회 논문집
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    • 제9권2호
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    • pp.39-43
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    • 2006
  • The magnitude of the axial force acting on turbopump bearings has a great influence on the operational reliability and service life of a turbopump. In the turbopump under current investigation the cavity vanes are introduced to the pump shroud casing to control the axial thrust of the turbopump. To investigate the effect of the cavity vanes, 3D computational flow analyses for a propellant pump stage including an inducer, impeller, volute and secondary flow passages are performed with and without the vanes. The results show that the cavity vanes are very effective in reducing the magnitude of axial thrust without notable changes on the overall performance of the turbopump.

로켓엔진용 산화제펌프의 수류 시험 (The Hydraulic Tests of LOX Pumps for a Liquid Rocket Engine)

  • 김대진;홍순삼;최창호;김진한
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2006년 제4회 한국유체공학학술대회 논문집
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    • pp.523-526
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    • 2006
  • A series of hydraulic and cavitation tests are performed in water environment in order to verify the hydraulic and cavitation performance of three types of LOX pumps. All the performances of the pumps are found to be satisfied with each design requirement. In the hydraulic tests, the head and efficiency are increased as the gap between floating ring seals and the impeller shoulder is decreased. In the cavitation tests, some pumps show decrease in the cavitation performance as the flowrate of the pump is decreased.

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원전 펌프의 성능저하 특성 (Degradation characteristics of pumps in nuclear power plants)

  • 이도환;박성근;홍성대;이병학
    • 한국소음진동공학회:학술대회논문집
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    • 한국소음진동공학회 2008년도 춘계학술대회논문집
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    • pp.593-598
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    • 2008
  • In the present study, degradation characteristics of pumps in nuclear power plants were investigated to provide the information of degradation mechanism and stressors. The failure records of pumps for the periods 2000 to 2006 on INPO(Institute of Nuclear Power Operations) EPIX(Equipment Performance and Information Exchange System) DB were reviewed. The 1,834 failure records reveal that the critical areas of pump failures are bearing, mechanical seal, gasket/o-ring, shaft, impeller, coupling and packing. Based on the failure rate of critical areas, the important degradation mechanism and stressors were determined. Additionally, the relationship between degradation mechanism and stressors such as wear was examined. Finally, the monitoring parameters related to degradation and stressors were discussed for the future development of degradation evaluation and prognosis technology of pumps.

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터보펌프 축추력 조절용 캐버티 베인에 대한 수치해석적 연구 (Numerical Study on the Effect of Cavity Vanes to Control the Axial Thrust of a Turbopump)

  • 노준구;최창호;김진한
    • 유체기계공업학회:학술대회논문집
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    • 유체기계공업학회 2005년도 연구개발 발표회 논문집
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    • pp.354-358
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    • 2005
  • The magnitude of the axial force acting on turbopump bearings has a great influence on the operational reliability and service life of a turbopump. In the turbopump under current investigation the cavity vanes are introduced to the pump shroud casing to control the axial thrust of the turbopump. To investigate the effect of the cavity vanes, 3D computational flow analyses for a propellant pump stage including an inducer, impeller, volute and secondary flow passages are performed with and without the vanes. The results show that the cavity vanes are very effective in reducing the magnitude of axial thrust without notable changes on the overall performance of the turbopump.

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직류전동기 구동 원심펌프-파이프 계통의 고장검출진단시스템: 등가관계 접근법 (Fault Detection and Isolation System for DC motor driven Centrifugal Pump-Pipe Systems: Parity Relation Approach)

  • 박태건;류지수;이기상
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 하계학술대회 논문집 B
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    • pp.819-821
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    • 1998
  • This paper deals with a method or a residual generation for fault isolation in a centrifugal pump with a water circulation system, driven by a speed controlled dc motor. It is based on parity relations derived from the moving-average model of the system and is used to identify sensor faults and two possible brush and impeller faults, where the former is dealt with additive faults, while the latter characterized as discrepancies between the nominal and actual plant parameters of the system is modelled by multiplicative faults. We will represent the propagation of this uncertainty to the model matrices by the approximate handling of partial derivatives of polynomials. With multiplicative faults, the transformation matrix implemented in the residual generator are calculated on-line. The simulation studies demonstrate that small changes of the system can be detected and diagnosed by using the method.

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원심펌프 측면흡입구의 유동특성에 관한 수치해석적 연구 (A Numerical Study on the Flow Characteristics of Side-suction Inlet Geometry for Centrifugal Pump)

  • 김성;최영석;이경용
    • 한국유체기계학회 논문집
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    • 제12권6호
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    • pp.7-12
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    • 2009
  • This paper presents a numerical study on the design of side-suction inlet geometry which is used for multi stage centrifugal pumps or inline centrifugal pumps. In order to achieve an optimum inlet geometry and to explain the interactions between the different geometric configurations, the three dimensional computational fluid dynamics and the design of experiment methods have been applied. Geometric design variables describing the cross sectional area distribution through the inlet were selected. The objective functions are defined as the non-uniformity of the velocity distribution at the passage exit which is just in front of the impeller eyes. From the 2k factorial design results, the most important design variable was found and the performance of the side suction inlet was improved compared to the base line shape.

Study of the Adhesive Coefficient Effect on the Hydraulic Losses and Cavitation

  • Pochly, Frantisek;Fialova, Simona;Kozubkova, Milada;Zavadil, Lukas
    • International Journal of Fluid Machinery and Systems
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    • 제3권4호
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    • pp.386-395
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    • 2010
  • The article is focused in three areas. In the first part there are analyzed the adhesion forces at the liquid and solid surface interface. There are shown the measured values of surface energy for different types of surfaces. The value of surface energy is decisive for determining the extent of the surface wettability by the liquid. The second part points to the possible negative effects of partly wettable surfaces, showing susceptibility to cavitation. The third section describes the practical aspects of surface wettability by the liquid. Under the new boundary conditions bases, expressing the effect of adhesion forces, there are determined the centrifugal pump characteristics.

Leakage Flow Influence on SHF pump model performances

  • Dupont, Patrick;Bayeul-Laine, Annie-Claude;Dazin, Antoine;Bois, Gerard;Roussette, Olivier;Si, Qiaorui
    • International Journal of Fluid Machinery and Systems
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    • 제8권3호
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    • pp.193-201
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    • 2015
  • This paper deals with the influence of leakage flow existing in SHF pump model on the analysis of internal flow behaviour inside the vane diffuser of the pump model performance using both experiments and calculations. PIV measurements have been performed at different hub to shroud planes inside one diffuser channel passage for a given speed of rotation and various flow rates. For each operating condition, the PIV measurements have been trigged with different angular impeller positions. The performances and the static pressure rise of the diffuser were also measured using a three-hole probe. The numerical simulations were carried out with Star CCM+ 9.06 code (RANS frozen and unsteady calculations). Some results were already presented at the XXth IAHR Symposium for three flowrates for RANS frozen and URANS calculations. In the present paper, comparisons between URANS calculations with and without leakages and experimental results are presented and discussed for these flow rates. The performances of the diffuser obtained by numerical calculations are compared to those obtained by the three-holes probe measurements. The comparisons show the influence of fluid leakages on global performances and a real improvement concerning the efficiency of the diffuser, the pump and the velocity distributions. These results show that leakage is an important parameter that has to be taken into account in order to make improved comparisons between numerical approaches and experiments in such a specific model set up.