• Title/Summary/Keyword: design flow

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Design of a Propeller Type Rim-Driven Axial-Flow Turbine for a Micro-Hydropower System (마이크로 수력 발전을 위한 프로펠러형 림구동 축류 터빈 설계)

  • Oh, Jin-An;Bang, Deok-Je;Jung, Rho-Taek;Lee, Su-Min;Lee, Jin-Tae
    • Journal of the Society of Naval Architects of Korea
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    • v.59 no.3
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    • pp.183-191
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    • 2022
  • A design method for a propeller type rim-driven axial-flow turbine for a micro-hydropower system is presented. The turbine consists of pre-stator, impeller and post-stator, where the pre-stator plays a role as a guide vane to provide circumferential velocity to the on-coming flow, and the impeller as a rotational power generator by absorbing angular momentum of the flow. BEM(Blade Element Method), which is based on the turbine Euler equation, is employed to design the pre-stator and impeller blades. NACA 66 thickness form and a=0.8 mean camber line, which is widely accepted as a marine propeller blade section, is used for the pre-stator and turbine blade section. A CFD method, derived from the discretization of the RANS equations, is applied for the analysis of the designed turbine system. The design conditions of the turbine is confirmed by the CFD calculation. Turbine characteristic curve is calculated by the CFD method, in order to provide the performance characteristics at off-design operation conditions. The proposed procedures for the design of a propeller type rim-driven axial-flow turbine are established and confirmed by the CFD analysis.

Dynamic Characteristics Analysis for Optimal Design of Flow Divider Valve (Flow Divider Valve의 최적설계를 위한 동특성 해석)

  • Hwang, Tae-Yeong;Park, Tae-Jo
    • 연구논문집
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    • s.29
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    • pp.123-130
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    • 1999
  • Flow divider valve, a kind of hydraulic control valve to divide the flow from one input line to two output line uniformly, should be able to keep the constant flow to output lines despite of the change load or supply pressure. Having 5-10% flow diving error in commercial hydraulic products is one of main source of the accumulated error caused hydraulic system problem and demands the development of flow divider valve to control flow more accurately, In this paper, the dynamic characteristics of flow divider valve are investigated by the numerical estimation of the spool motion considered the external supply force. The optimum design of flow divider valve are proposed to reduce the flow diving error. For the dynamic characteristics analysis, the change of sectional area of fixed and variable orifice, and spool are studied when the input signal is accepted to a constant load.

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The Analysis for Flow Circulation System in HANARO Flow Simulation Facility (하나로 유동 모의 설비의 유체순환계통 해석)

  • Park, Yong-Chul
    • The KSFM Journal of Fluid Machinery
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    • v.7 no.1 s.22
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    • pp.30-35
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    • 2004
  • The HANARO, a multi-purpose research reactor of 30 MWth open-tank-in-pool type, has been under normal operation since its initial criticality in February, 1995. Many experiments should be safely performed to activate the utilization of the HANARO. HANARO flow simulation facility is being developed for the endurance test of reactivity control units for extended life time and the verification of structural integrity of those experimental equipments prior to loading in the HANARO. This facility is composed of three major parts; a half-core structure assembly, a flow circulation system and a support system. The flow circulation system is composed of a circulation pump, a core flow piping, a core bypass flow piping and instruments. The system is to be filled with de-mineralized water and the flow should be met the design requirements to simulate a similar flow characteristics in the core channel of the half-core structure assembly to the HANARO. This paper, therefore, presents an analytical analysis to study the flow behavior of the system. Computational flow analysis has been performed for the verification of system pressure variation through the three-dimensional analysis program with the standard $k-{\epsilon}$ turbulence model and for the verification of the structural piping integrity through the finite element method. According to the analysis results, it could be said that the design requirements and the structural piping integrity of the flow circulation system are satisfied.

Physical Design Flow & Verification of DVB Compliant Satellite Receiver Chip (디지털 비디오 방송 컴플라이언트 위성 수신 칩의 Physical 설계 및 검증)

  • 신수경;최영식
    • Proceedings of the Korean Institute of Information and Commucation Sciences Conference
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    • 2001.05a
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    • pp.345-348
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    • 2001
  • The paper describes the physical design flow & verification of Digital Video Broadcasting(DVB) compliant satellite receiver chip. It includes problems and issues of earth design flow, verification process for physical layout.

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Aerodynamic Design Program for Centrifugal/Mixed-flow Compressors - Part I : Meanline Design and Performance Prediction - (원심/사류압축기의 공력설계 프로그램 개발 - 제1부 : 평균유선 설계/성능해석 -)

  • Oh, Jong-Sik
    • 유체기계공업학회:학술대회논문집
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    • 2003.12a
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    • pp.457-463
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    • 2003
  • A general program of meanline design and/or performance prediction for centrifugal/mixed-flow compressors is successfully commercialized using various empirical loss models. 4 types of diffusers, 3 types of exit elements, shrouded/unshrouded impellers and real gas option are included in the program capabilities. Total 16 cases of benchmark test results proved its reliability to be effectively utilized in the development processes.

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Design Optimization of An Axial-Flow Compressor Rotor Using Response Surface Method (반응면 기법을 이용한 천음속 축류압축기의 삼차원 형상 최적설계)

  • Ahn, Chan-Sol;Kim, Kwang-Yong
    • Transactions of the Korean Society of Mechanical Engineers B
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    • v.27 no.2
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    • pp.155-162
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    • 2003
  • Design optimization of a transonic compressor rotor (NASA rotor 37) using response surface method and three-dimensional Navier-Stokes analysis has been carried out in this work. Baldwin-Lomax turbulence model was used in the flow analysis. Three design variables were selected to optimize the stacking line of the blade. Data points for response evaluations were selected by D-optimal design, and linear programming method was used for the optimization on the response surface. As a main result of the optimization, adiabatic efficiency was successfully improved. It is also found that the design process provides reliable design of a turbomachinery blade with reasonable computing time.

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

  • Guo En-Min;Kim Kwang-Yong;Seo Seoung-Jin
    • Proceedings of the KSME Conference
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    • 2002.08a
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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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Design of Impeller and Diffuser for Mixed Flow Pump with Inverse Design Method (역설계 방법을 적용한 사류펌프의 임펠러 및 디퓨저 설계)

  • Lee, Kyoung-Yong;Choi, Young-Seok;Kim, Jun-Ho
    • Proceedings of the SAREK Conference
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    • 2009.06a
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    • pp.1322-1325
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    • 2009
  • The impeller and vane diffuser for the mixed flow pump(NS550) was designed by using meridional selection program and inverse design method. We decided the meridional shape of the impeller from the meridional design parameter, such as the specific speed and maximum diameter at the impeller exit. The meridional shape of vane diffuser was set from the impeller shape, distribution of cross sectional area and maximum diffuser diameter. The angle of impeller blade and diffuser vane was designed by using inverse design method. The predicted overall performance by using commercial CFD code(ANSYS CFX-11) shown good agreement with design goals.

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Optimum Design of Axial-Flow Fans Including Noise Parameters (소음파라메터를 고려한 축류송풍기의 최적설계)

  • Son, B.J.;Lee, S.H.;Yoon, S.J.
    • Korean Journal of Air-Conditioning and Refrigeration Engineering
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    • v.7 no.1
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    • pp.1-12
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    • 1995
  • In order to seek various relationships among many design parameters employed in the design of the axial-flow fans the program which generates acoustic spectrum has been developed and its validity verified. Outputs of the program, with other outputs from a formerly developed performance prediction program, have been used to form a multi-objective function, for which an optimal design process was carried out. The present analysis shows that overall noise level and efficiency has contrasting trends, and the chord length turns out to be the most critical design variable. In the chosen design case of requirements $Q=2000m^2/min$, ${\Delta}P_s=67mmAq$, D=1.4m, the chord length of 0.2059m minimizes the overall noise level, while chord length of 0.1254m maximizes the efficiency. The resulting chord length in the balanced optimization is 0.1809m.

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A Design Process of Digital System in Polymachine Image (복합 기계 상에 의한 디지탈 시스템의 일반계 과정)

  • 김현재
    • Journal of the Korean Institute of Telematics and Electronics
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    • v.19 no.6
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    • pp.9-16
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    • 1982
  • This is an introduction to an art of digital hardware design using polymachine image as a target structure of the product. As in the case of software design of a computer, the design process begins with a sketch of planned system in flow chart description and the flow charts is partitioned into divergent elements. Each of the element machine is derived from those divergent elements. We can build a complete digital system with the preparation of an index, and a polymer of these element machines.

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