• Title/Summary/Keyword: low speed region

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Characteristics of Analog Encoder for SRM Drive

  • Park, Sung-Jun;Ahn, Jin-Woo
    • KIEE International Transaction on Electrical Machinery and Energy Conversion Systems
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    • v.12B no.1
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    • pp.31-36
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    • 2002
  • In a switched reluctance motor drive, it is important to synchronize the stator phase excitation with the rotor position; therefore, the position of rotor is an essential information. Although optical encoders or resolvers are used to provide the position information, these sensors are expensive. Moreover, in the high-speed region, switching angles are fluctuated back and forth out of the preset value, which is caused by the sampling period of the microprocessor. In this paper, a low cost analog encoder suitable for practical applications is proposed. And the control algorithm to generate switching signals using a simple digital logic is presented. The validity of the proposed analog encoder with a proper logic controller is verified from the experiments.

Flow characteristics at the Impeller Exit of a Centrifugal Pump (원심펌프의 회전차 출구 유동 특성)

  • Hong, Soon-Sam;Kang, Shin-Hyoulg
    • 유체기계공업학회:학술대회논문집
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    • 2000.12a
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    • pp.36-44
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    • 2000
  • The flow at the impeller exit is important to validate engineering design and numerical analysis of pumps. We installed axisymmetric collector instead of the volute casing, so there is no interaction between the impeller and casing. A hot-film probe and a high response pressure transducer are used to investigate the flow at impeller exit and vaneless diffuser region for design and off design flow rate. For a single suction centrifugal pump of low specific speed, the flow field such as velocity, flow angle, and total pressure are measured by traversing the probe across the vaneless diffuser. These data can be used for performance prediction, design, and numerical analysis of pumps.

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LOW-SPEED AERODYNAMIC CHARACTERISTIC OF TRANSITION FLOW OVER THE NACA0012 (NACA0012 천이 유동의 저속 공력 특성 해석)

  • Jeon, Sang-Eon;Park, Soo-Hyung;Kim, Sang-Ho;Byun, Yung-Hwan;Jung, Kyung-Jin;Kang, In-Mo
    • Journal of computational fluids engineering
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    • v.15 no.3
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    • pp.1-8
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    • 2010
  • Laminar separation bubble and transitional flow over the NACA0012 are investigated at a moderate range of Reynolds numbers. A Reynolds-Averaged Navier-Stokes code is coupled with an empirical transition model that can predict transition onset points and the length of transition region. Without solving the boundary layer equations, approximated e-N method is directly applied to the RANS code and iteratively solved together. The computational results are compared with the experimental data for the NACA0012 airfoil. Results of transition onset point and the length are compared well with experimental data and Xfoil prediction. The present RANS results show at high angles of attack better agreement with experimental data than Xfoil results using the boundary layer equations.

A Numerical Study on Real Gas Effect due to High Temperature and Speed Flow (고온 고속유동으로 인한 실제 기체효과의 수치해석적 연구)

  • 송동주
    • Transactions of the Korean Society of Mechanical Engineers
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    • v.18 no.9
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    • pp.2431-2442
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    • 1994
  • In this paper the efficient space marching Viscous Shock Layer and Parabolized Navier-Stokes method have been applied to study the complex 3-D hypersonic equilibrium chemically reacting flowfilelds over sphere-cone($10^{\circ}$) vehicle at low angles of attack($0^{\circ}~5^{\circ}), Mach 20, and an altitude of 35km. The current bluntbody/afterbody space marching numerical method predicts the complex flowfields accurately and efficiently even on a small computer. The shock thickness from equilibrium air model is thinner than that from the perfect gas model. The windside wall heat-transfer rate, pressure and skin friction force were increased significantly when compared with those of leeside. The CA, CN, CM were increased almost linearly with the angle of attack in this region. The wall pressure, heat transfer, skin friction and axial force coeffient from equilibrium model were much higher than those from perfect gas model. The center of pressure moved forward with the increase of angle of attack.

Aerodynamic Load Analysis for Wind Turbine Blade in Uniform Flow and Ground Shear Flow (균일 흐름과 지상 전단 흐름에 놓인 수평축 풍력터빈 블레이드의 공력 하중 비교)

  • Kim, Jin;Ryu, Ki-Wahn
    • 한국신재생에너지학회:학술대회논문집
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    • 2007.11a
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    • pp.387-390
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    • 2007
  • Recently the diameter of the 5MW wind turbine reaches 126m, and the tower height is nearly the same with the wind turbine diameter. The blade will experience periodic inflow oscillation due to blade rotation inside the ground shear flow region, that is, the inflow velocity is maximum at uppermost position and minimum at lowermost position. In this study we compare the aerodynamic data between two inflow conditions, i.e, uniform flow and normal wind profile. From the computed results all of the relative errors for oscillating amplitudes increased due to the ground shear flow effect. Especially My at hub and $F_x$, $M_y$, $M_z$ at LSS increased enormously. It turns out that the aerodynamic analysis including the ground shear flow effect must be considered for fatigue load analysis.

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Three-Dimensional Computations of Rocket Exhaust Plume (로켓 배기플룸에 관한 3차원 수치해석)

  • Kim Y.-M.
    • 한국전산유체공학회:학술대회논문집
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    • 1999.11a
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    • pp.71-76
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    • 1999
  • The base flow regions of a three-body sounding rocket containing multiple exhaust plumes were numerically investigated in three dimensions for a free stream Mach number of 2.7 at flight altitude 18.5 km. The flowfields were calculated using the full compressible Navier-Stokes equations with an one-equation turbulence model of Baldwin-Earth. The present calculations were executed based upon a chemically frozen, single perfect gas model assumption. Due to the symmetry of the three-body rocket of each single nozzle, only one fourth of the computational domain was considered for the analysis. The results indicate that a babe heating effect is not considerable due to the small expansion of the plumes. In the base, however, a low speed recirculating flow dominates the region.

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Analog Encoder for Precise Angle Control of SRM (SRM의 정밀 각도제어를 위한 아날로그 엔코더)

  • Kim T.H.;An Y.J.;Ahn J.W.
    • Proceedings of the KIPE Conference
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    • 2003.07b
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    • pp.667-670
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    • 2003
  • In a switched reluctance motor drive, it is important to synchronize the stator phase excitation with the rotor position, because the position of rotor is an essential information. In the high-speed region, switching angles are fluctuated back and forth out of\ the preset value, which is caused by the sampling period of the microprocessor. In this paper, a low cost analog encoder suitable for practical applications is proposed. The validity of the proposed analog encoder with a proper logic controller is verified from the experiments.

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Optimal Design of a Direct-Drive Permanent Magnet Synchronous Generator for Small-Scale Wind Energy Conversion Systems

  • Abbasian, Mohammadali;Isfahani, Arash Hassanpour
    • Journal of Magnetics
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    • v.16 no.4
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    • pp.379-385
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    • 2011
  • This paper presents an optimal design of a direct-drive permanent magnet synchronous generator for a small-scale wind energy conversion system. An analytical model of a small-scale grid-connected wind energy conversion system is presented, and the effects of generator design parameters on the payback period of the system are investigated. An optimization procedure based on genetic algorithm method is then employed to optimize four design parameters of the generator for use in a region with relatively low wind-speed. The aim of optimization is minimizing the payback period of the initial investment on wind energy conversion systems for residential applications. This makes the use of these systems more economical and appealing. Finite element method is employed to evaluate the performance of the optimized generator. The results obtained from finite element analysis are close to those achieved by analytical model.

Regenerative Braking Characteristics of Linear induction Motor for MAGLEV (자기부상열차용 선형유도전동기의 회생 제동 특성 해석)

  • Park, Seung-Chan;Lee, Won-Min;Kim, Jung-Cheol;Park, Yeong-Ho
    • Proceedings of the KSR Conference
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    • 2008.06a
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    • pp.1866-1870
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    • 2008
  • In this paper, electric braking performances of linear induction motor(LIM) designed for propelling the MAGLEV are presented. Regenerative braking is carried out from 110km/h to 20km/h, and plugging which converts the direction of travelling magnetic field is carried out in the low speed region below 20km/h. It is important to reduce attractive force which can affect the magnetic levitation load during regenerative braking or plugging operation mode. So in this paper the braking performances are analyzed by finite element method. As a result, braking force, attractive force, phase current, voltage to frequency patterns and its magnetic fields of braking LIM are presented.

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An Analog Encoder for Precise Angle Control of SRM

  • Ahn, Jin-Woo;Park, Sung-Jun
    • Journal of Power Electronics
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    • v.3 no.3
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    • pp.167-174
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    • 2003
  • In a switched reluctance motor drive, it is important to synchronize the stator phase excitation with the rotor position, because the position of rotor is an essential information. Although high resolution optical encoders or resolvers are used to provide a precise position information, these sensors are expensive. Moreover, in the high-speed region, switching angles are fluctuated back and forth out of the preset value, which is caused by the sampling period of the microprocessor. In this paper, a low cost analog encoder suitable for practical applications is proposed. And the control algorithm to generate switching signals using a Simple digital logic is presented. The validity of the proposed analog encoder with a proper logic controller is verified from the experiments.