• 제목/요약/키워드: rotor loss

검색결과 299건 처리시간 0.021초

축류펌프 안내 깃 최적화 설계를 위한 전산 유동해석 (CFD Analysis for Optimization of Guide Vane of Axial-Flow Pump)

  • 윤정의
    • 대한기계학회논문집B
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    • 제40권8호
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    • pp.519-525
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    • 2016
  • 펌프 성능 관점에서 바라보면 회전날개의 충격손실을 최소화하는 것은 매우 중요하다. 본 연구는 회전날개의 충격손실에 직접적으로 영향을 미치는 흡입 케이싱 내에 설치되는 안내깃의 형상 및 설치 각 변화가 축류 펌프의 성능에 미치는 효과를 수치 해석 방법을 통해 살펴보았다. 그리고 주어진 운전조건에서 흡입 케이싱 내에 설치되는 안내깃의 최적형상 및 설치 각을 최적화 기법을 사용하여 최적화하였다.

3MW 해상풍력용 영구자석 동기발전기 개발현황 (Status of 3 MW PM Synchronous Generator Development Project for Off-shore WECS)

  • 김동언;한홍식;이홍기;정영규;서형석;정진화
    • 한국신재생에너지학회:학술대회논문집
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    • 한국신재생에너지학회 2007년도 춘계학술대회
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    • pp.423-426
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    • 2007
  • Pohang Wind Energy Research Center (PoWER-C) is developing a 3 MW Radial Flux Permanent Magnet (RFPM) Synchronous Generator for offshore Wind Energy Converter (WEC). The rotor rpm is 15.7 and the gear ratio is set to be 92.93. The nominal generator rpm at the rated load is about 1459. To reduce the switching loss in the power electronics, the maximum frequency is limited to 100 Hz. This requirement limits the number of pole to six or eight. Permanent magnet excitation is assumed for higher energy yield and higher efficiency. In this report, the requirements and the first efforts for the physics design are described.

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3상 6/8극 SRM의 설계 및 운전 특성 (Design and Drive of 3-phase 6/8 SRM)

  • ;이동희;안진우
    • 전력전자학회논문지
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    • 제8권1호
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    • pp.48-55
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    • 2003
  • 본 논문은 3상 6/8극 스위치드 릴럭턴스 전동기의 설계 및 특성해석에 대해 다루었다. 고정자와 회전자 극호각의 설계 범위를 해석하고 최적값을 해석하였다. 최적의 값은 선형, 비선형으로 나누어 전통적인 설계접근 방식과 설계용 CAD를 이용하여 해석하였으며 실제 전동기를 제작하여 설계결과를 확인하였다. 이 전동기는 동일한 8/6 SRM에 비해 구동회로가 단순해지며, 권선의 전류밀도와 동손이 감소하여 효율이 상승하는 장점이 있다.

Thermal Analysis of a Canned Induction Motor for Main Coolant Pump in System-Integrated Modular Advanced Reactor

  • Huh, Hyung;Kim, Jong-In;Kim, Kern-Jung
    • KIEE International Transaction on Electrical Machinery and Energy Conversion Systems
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    • 제3B권1호
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    • pp.32-36
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    • 2003
  • The three-phase canned induction motor, which consists of a stator and rotor with a seal can, is used for the main coolant pump (MCP) of the System-integrated Modular Advanced Reactor (SMART). The thermal characteristics of the can must be estimated exactly, since the eddy current loss of the can is a dominant parameter in design. Besides the insulation of the motor winding is compared of Teflon, glass fiber, and air, so it is not an easy task to analyze. A FEM thermal analysis was per-formed by using the thermal properties of complex insulation which were obtained by comparing the results of finite element thermal analysis and those of the experiment. As a result, it is shown that the characteristics of prototype canned induction motor have a good agreement with the results of FEM.

고조파감소 및 역률개선을 위한 SRM 구동시스템에 관한 연구 (SRM drive system with reduced harmonics and improved power factor)

  • 신규재;권영안;임근희
    • 전자공학회논문지S
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    • 제34S권10호
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    • pp.151-157
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    • 1997
  • Switched relutance motor(SRM) has the advantages of simple structure, low rotor intertia, and high power rate per unit volume. However, SRM has the disadvantages of high current harmonics, and low power factor because of the discontinuous excitation of pulse type. The harmonics brings about the distortion and loss of power system, and brings about the incorrect opertion of electronic system. This paper investigates the SRM drive system with the reduced harmonics and improved power factor. The system consists of the switching power converter with poewr factor correction(SPC-PFC), DC/DC converter and 3-phase inverter. The performances in the proposed system are verified through the simpuation and experiment.

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유한요소법과 프라이자흐 모델을 이용한 동기형 릴럭턴스 전동기(Synchronous Reluctance Motor: SynRM)의 On-line 관측기시스템 특성해석 (The On-line Observer System Characteristics Analysis of Synchronous Reluctance Motor Using a Coupled FEM & Preisach Model)

  • 김홍석;이중호
    • 전기학회논문지
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    • 제56권12호
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    • pp.2103-2108
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    • 2007
  • This study investigates the dynamic characteristics of Synchronous Reluctance Motor (SynRM), with segmental rotor structure, using finite element method in which the moving mesh technique is considered. The focus of this paper is the efficiency of on-line parameter identification system for position sensorless control of a SynRM considering saturation and iron loss. Comparisons are given with angle of the observer and those of proposed FEM & Preisach model of synchronous reluctance motor, respectively. The position sensorless control using identified motor parameters is realized, and the efficiency of the on-line parameter identification system is verified by experimental results.

전향각이 큰 선형터빈 익렬을 통하는 난류유동의 수치해석 (Numerical simulation of turbulent flows through linear turbine cascades with high turning angles)

  • 이훈구;유정열;윤준원
    • 대한기계학회논문집B
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    • 제20권12호
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    • pp.3917-3925
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    • 1996
  • A numerical analysis on three dimensional turbulent incompressible flows through linear cascades of turbine rotor blades with high turning angles has been performed by using a generalized k-.epsilon. model which is a high Reynolds number form and derived by RNG(renormalized group) method to account for the variation of the rate of strain. A second order upwind scheme is used to suppress numerical diffusion in approximating the convective terms. Body-fitted coordinates are adopted to represent the complex blade geometry accurately. For the case without tip clearance, velocity vectors and static pressure contours are shown to be in good agreement with previous experimental results. For the case with tip clearance, the effects of the passage vortex and tip clearance flow on the total pressure loss as well as their interactions are discussed.

산업현장에서 벡터제어용 유도전동기의 오프라인 파라미터 추정 (Off-line parameter Estimation of Induction Motors for Vector Control in Industrial Field)

  • 권병기;박가우;신원창;조응상;이진섭;최창호
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 1998년도 전력전자학술대회 논문집
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    • pp.234-238
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    • 1998
  • Parameter estimation of induction motor for vector control presented in this paper can be easily implemented and applied to inverters in the industrial field, because it needs no additional hardware such as voltage sensor and measuring equipment. At first, the stator resistance including switching loss of inverter is measured by simple voltage-current equation. Next, in pre-magnetization of machine by imposing the d-axis constant field-current, q-axis torque current is forced to the machine until its speed feedback reachs to pre-defined level of speed limit. At this time, we can measure the rotor time-constant by decreasing the distorted output-voltage of inverter. At last, stator inductance, transient inductance, and moment of inertia can be measured by the relationship of output voltage, output torque and speed feedback. The validity and usufulness of this method is verified by experimental results.

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자기저항 동기전동기의 정수추출을 통한 특성 연구 (Performance Analysis According to Parameter Measurement of Synchronous Reluctance Motor)

  • 이정섭;홍정표;한성진;주수원
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1999년도 추계학술대회 논문집 학회본부 A
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    • pp.73-75
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    • 1999
  • The performance of a SRM in terms of torque and power factor depends on the two-axis inductances (Ld and Lq) and iron loss of the machine. Finite element method has been used to determine these parameters for a motor with segmented rotor structure. Fock and Hart Method has been conducted to compare to verify the accuracy of proposed analysis method.

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UH-1H 조종사의 전신진동 노출에 따른 임무별 비행시간 한계에 관한 연구 (A Study on the Flight-time Limitation at each Mission in Whole-Body Vibration Exposure of UH-1 Pilot)

  • 송근식;정완섭;이달호
    • 한국산업안전학회:학술대회논문집
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    • 한국안전학회 1998년도 추계 학술논문발표회 논문집
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    • pp.353-358
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    • 1998
  • Vibrations exposured to human whole-body are transmitted through the contact area of a human body, such as feet, hip and back directly in contact with vibrating surface. they apparently leads to the decrease of human comfort, the reduction of working efficiency or normal activities, and, furthermore, causes the loss of health and safety. In this study, UH-1 vibration has been measured to produce the flight-time limitation at each mission Results of this study show that the most significant peaks appear at a main rotor blade-passage frequency and that the vibration level in ground is higher than that in airborne In addition, it is shown that the most affective aspect for the flight-time limitation is ground vibration level

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