• 제목/요약/키워드: impeller geometry

검색결과 59건 처리시간 0.036초

Effect of Internal Flow in Symmetric and Asymmetric Micro Regenerative Pump Impellers on Their Pressure Performance

  • Horiguchi, Hironori;Matsumoto, Shinji;Tsujimoto, Yoshinobu;Sakagami, Masaaki;Tanaka, Shigeo
    • International Journal of Fluid Machinery and Systems
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    • 제2권1호
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    • pp.72-79
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    • 2009
  • The effect of symmetric and asymmetric micro regenerative pump impellers on their pressure performance was studied. The shut off head of the pump with the symmetric impeller was about 2.5 times as that with the asymmetric impeller. The computation of the internal flow was performed to clarify the cause of the increase of the head. It was found that the contribution of the angular momentum supply was larger than that of shear stress for the head development in both cases. The larger head and momentum supply in the case of the symmetric impeller were caused by larger recirculated flow rate and larger angular momentum difference between the inlet and outlet to the impeller. The larger recirculated flow rate was caused by smaller pressure gradient in the direction of recirculated flow. The decrease of the circumferential velocity in the casing was attributed to the smaller local flow rate in the casing.

Aspect-Ratio Effects and Unsteady Pressure Measurements inside a Cross-Flow Impeller

  • Hirata, Katsuya;Onishi, Yusuke;Nagasaka, Shigeya;Matsumoto, Ryo;Funaki, Jiro
    • International Journal of Fluid Machinery and Systems
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    • 제5권3호
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    • pp.117-125
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    • 2012
  • In the present experimental study, the authors try to clarify the characteristics of the flow around and inside a cross-flow impeller in a typical geometry, over a wide parameter range of an aspect ratio $L/D_2$. In order to eliminate the complicated casing factors, the impeller rotates in open space without any casings. As a result, by using hot wire anemometer measurements and by conventional flow visualisations with a particle image velocimetry technique, the authors show that both the outflow rate and the maximum vorticity attain the maximum for $L/D_2$ = 0.6. In order to investigate the aspect-ratio effect, we further reveal minute fluctuating pressures on an impeller end wall for a singular $L/D_2$ = 0.6. Especially in these pressure measurements, the eccentric vortex is prevented to revolute by the insertion of a tongue, in order to consider the spatial structure of flow more precisely.

자동차 밀폐형 워터펌프의 토출구 형상이 수력성능에 미치는 영향 (Effect of Shape of Discharge Port on Hydraulic Performance of Automotive Closed Type Water Pump)

  • 허형석;이기수;배석정
    • 한국자동차공학회논문집
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    • 제14권1호
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    • pp.39-47
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    • 2006
  • Recent trend in pursuit of high performance and effectiveness for automotive cooling system has changed the application of material for impeller of automotive water pump from metal to high ability engineering resin, which can achieve optimization of design of impeller geometry and realize lightweight high efficiency water pump. Closed type water pump improves hydraulic loss of fluid through the clearance between volute casing and impeller compared with that of the existing open type water pump(Although closed type is heavier than open type for the same size and same material, adoption of plastics can solve the problem.). In the present study, the characteristics of hydraulic performance of closed type water pump were investigated with respect to the angle between shroud and hub of impeller and the shape of discharge port of volute casing. Performance tests were carried out for 4 cases, that is, for 2 impellers and 2 casings. The modification of shape of only discharge port can enhance the hydraulic performance by 10 percent and the pump efficiency by 4-6 percent.

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.

횡류형 파워터빈의 최적화 설계에 관한 수치해석 연구 (A Numerical Study on an Optimum Design of a Cross-flow Type Power Turbine (CPT))

  • 하진호;김현철;김철호
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2007년도 춘계학술대회B
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    • pp.3050-3055
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    • 2007
  • A wind turbine is one of the most popular energy conversion systems to generate electricity from the natural renewable energy source and an axial-flow type wind turbine is the most popular system for the electricity generation in the wind farm nowadays. In this study, a cross-flow type turbine has been studied for the application of wind turbine for electricity generation. The target capacity of electric power generation of the model wind turbine developing on the project is 12 volts, 130A/H (about 1.56kW). The important design parameters of the model turbine impeller are the inlet and exit angle of the turbine blade, number of blade, hub/tip ratio and the exit flow angle of the casing. In this study, the radial equilibrium theorem was used to decide the inlet and exit angle of the impller blade and CFD technique was used to have the performance analysis of the designed model power turbine to find out the optimum geometry of the CPT impeller and casing. The designed CPT with 24 impeller blades at ${\alpha}=82^{\circ}$, ${\beta}=40^{\circ}$ of turbine blade angle was estimated to generate 284.6 N.m of indicated torque and 2.14kW of indicated power.

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2단 사류펌프의 임펠러 성능향상 방안 연구 (STUDY ON THE HYDRAULIC DESIGN OF 2 STAGE MIXED FLOW PUMP)

  • 김영주;우남섭;권재기;정소걸;박의섭;배상은;박수한
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2011년 춘계학술대회논문집
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    • pp.556-560
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    • 2011
  • The seawater lift pump system is responsible for maintaining the open canal level to provide the suction flow of circulating water pump at the set point. The objective of this paper is to design a 2-stage mixed flow pump(for seawater lifting) by inverse design and to evaluate the overall performance and the local flow fields of the pump by using a commercial CFD code. Rotating speed of the impeller is 1,750 rpm with the flow rate of 2,700 $m^3/h$. Finite volume method with structured mesh and Realizable ${\kappa}-{\varepsilon}$ turbulent model is used to guaranty more accurate prediction of turbulent flow in the pump impeller. The numerical results such as static head brake horse power and efficiency of the mixed flow pump are compared with the reference data. Also, the periodic condition calculation method for the mixed flow pump was carried out in order to investigate the pump performance characteristics with the modification of impeller geometry.

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저점도 액 통기 교반용 글라스라이닝 홈베이스 임펠러의 최적 형상 (Optimum Geometry of Glass Lined HOMEBASE Impeller for Gas-Liquid System of Low Viscosity Liquid)

  • 고승태
    • Korean Chemical Engineering Research
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    • 제59권4호
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    • pp.542-547
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    • 2021
  • 글라스 라이닝 임펠러는 강산을 포함한 대부분의 화학물질들에 대해 내부식성이 있고, 또한 평활하고 눌어붙지 않는 표면을 가지며 세정이 용이하고 프로세스에 불순물들을 유입하지 않는 강점을 갖고 있다. 글라스 라이닝 HOMEBASE 임펠러는 저점도 유체에서 고점도 유체까지 폭넓은 점도 범위의 액체를 교반할 수 있도록 개발된 다목적형 대형 교반 임펠러이나, 그중에서도 세포 배양이나 효모의 배양, 맥주 발효 솥 등은 저점도 액의 통기 교반에 많이 사용하며, 특히 공기-수계의 통기성 교반에 많이 적용한다. 구조가 간단하면서도 성능 면에서 경쟁력을 갖는 HOMEBASE 임펠러에 대한 글라스 라이닝은 제작상 임펠러와 샤프트의 접합 면적을 가능한 한 작게 할 수 있도록 상하 분할이 필수적이다. 임펠러의 상하 분할은 혼합 성능에는 거의 영향을 미치지 않지만, 통기 성능을 저하하였다. 본 연구에서는 Glass Lined HOMEBASE 임펠러 형상의 최적화를 위해, 상·하부로 분할된 임펠러 사이의 장착각도차와 임펠러 사이의 간격 및 방해판의 개수가 통기 동력에 미치는 영향에 관한 연구를 수행하였다. 상·하부로 분할된 임펠러 사이의 장착각도차와 간격이 통기를 할 때의 동력 Pg와 통기가 없을 때의 동력 P0의 비인 Pg/P0를 저하시킨다는 연구 결과를 통해 Glass Lined HOMEBASE 임펠러 최적 형상과 방해판 조건을 도출하였다.

R134a용 터보냉동기의 원심압축기 개발 Part 1 : 원심압축기 설계 (Development of the Centrifugal Compressor for a R134a Turbo-Chiller Part 1 : Design of the Centrifugal Compressor)

  • 이용덕;정진희;이현구;윤필현;김길영
    • 한국유체기계학회 논문집
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    • 제3권4호
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    • pp.44-51
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    • 2000
  • The present study has been conducted to design the high efficiency centrifugal compressor for a R134a turbo-chiller. The centrifugal compressor consists of an impeller with splitters, two vaneless diffusers, a low-solidity vaned diffuser and a volute. A cycle analysis program for a turbo-chiller was developed to obtain compressor design parameters and requirements. We have designed the high efficiency centrifugal compressor by applying the repeated design procedure including a meanline design, a 3D geometry generation and fluid dynamic loading calculations.

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공력음향학적 특성을 고려한 시로코 팬의 설계 방법 (Design Method of the Sirocco Fan Considering Aeroacoustic Performance Characteristics)

  • 이찬
    • 한국유체기계학회 논문집
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    • 제13권2호
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    • pp.59-64
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    • 2010
  • A design method of Sirocco fan is developed for constructing 3-D impeller and scroll geometries, and for predicting both the aerodynamic performance and the noise characteristics of the designed fan. The aerodynamic blading design of fan is conducted by blade angle, camber line determinations and airfoil thickness distribution, and then the scroll geometry of fan is designed by using logarithmic spiral. The aerodynamic performance of designed fan is predicted by the meanline analysis with flow blockage, slip and pressure loss correlations. Based on the predicted performance data, fan noise is predicted by two models for cutoff frequency and broadband noise sources. The present predictions for the performance and the noise level of actual fans are well agreed with measurement results.

관류익형송풍기의 공력해석 및 설계 (Aerodynamic Analysis and Design of Inline-Duct Fan)

  • 곽은민;김광용;서성진
    • 대한기계학회:학술대회논문집
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    • 대한기계학회 2002년도 학술대회지
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    • pp.639-642
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    • 2002
  • A tubular centrifugal fin is designed by using various methods of analysis and design. A preliminary design method based on empirical optimum curves for centrifugal fin is used to determine the geometric parameters for tubular centrifugal fan. And, Quasi-3D streamline curvature duct-flow analysis is used to provide the primary position of streamlines and spanwise distribution of flow angle f3r generation of blade geometry based on S1 surface. Three-dimensional CFD solution then is obtained to optimize the blade design. Constriction of flow path in the region of impeller, backward swept blade, and central cone, which are introduced to improve the design, successfully remove or suppress the vortices downstream of the impeller.

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