• Title/Summary/Keyword: Rotor Interference

검색결과 49건 처리시간 0.021초

리니어 모터를 위한 능동 자기 베어링의 설계 및 제어 (Design and Control of an Active Magnetic Bearing for Linear Motors)

  • 양광원;허경무
    • 대한전자공학회:학술대회논문집
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    • 대한전자공학회 2001년도 하계종합학술대회 논문집(5)
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    • pp.119-122
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    • 2001
  • This paper deals with new type of active magnetic bearing (AMB) for the linear motors. We adopted optical sensing mechanism for the gap sensing. Using the laser and the PSD (Position Sensitive Device), the absolute rotor position is obtained independent of the profile of the guide rail. With this measurement, the rotor can be controller to follow the straight beam of the laser. Another advantage of optical sensing mechanism might be the elimination of the possible interference between the proximity sensor and the electro-magnet. By adopting the push-full actuating mechanism, the bearing stiffness is increased near the equilibrium position. For the simplicity, distributed control system is constructed. Eight independent PID control algorithm is used with the full order observer. Several simulation md test results are presented.

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수평축 조류발전 터빈 설계 및 후류 특성 분석 (Design of Horizontal Axis Tidal Current Power Turbine with Wake Analysis)

  • 조철희;김도엽;이강희;노유호;김국현
    • 신재생에너지
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    • 제7권3호
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    • pp.92-100
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    • 2011
  • With the increased demand of clean energy and global warming measures, the renewable energy development has been increased recently. The TCP (Tidal Current Power) is one of the ocean renewable energy sources. Having the high tidal energy source in Korea, there are many potential TCP sites with strong current speed. The rotor, which initially converts the energy, is a very important component because it affects the efficiency of the entire system. The rotor performance is determined by various design parameters including number of blades, shape, sectional size, diameters and etc. However, the interactions between devices also contribute significantly to the energy production. The rotor performance considering the interaction needs to be investigated to predict the exact power in the farm. This paper introduces the optimum design of TCP turbine and the performance of devices considering the interference between rotors.

Dual Rotor 풍력발전을 이용한 선박에서의 효과적인 풍향 풍속 측정 (Efficient Measurement of Wind Velocity and Direction Using Dual Rotor Wind Power Generator in Vessel)

  • 최원연;박계도;이장명
    • 로봇학회논문지
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    • 제5권4호
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    • pp.309-317
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    • 2010
  • This paper proposes an efficient measurement system for the velocity and direction of the wind using the dual rotor wind power generator in vessel. Conventional digital measurement system recognizes the direction and the velocity of the wind using the electric compass or synchronous motor and Vane probe method using hall sensors. But each system has its own short-comings: the synchronous motor has a larger measurement error than the magnetic compass and magnetic compass is weak for the external disturbances such as fluctuation of the vessel. To compensate these short-comings, this paper proposes a new compensation algorithm for the fluctuation errors according to the external interference and the unexpected movement of the vessel along the roll and pitch directions. The proposed system is implemented with the dual compasses and a synchronous motor. The proposed independent power generation system can be operated by itself and can raise the efficiency of the wind power generation systems of 30 ~ 400 W installed along the vertical and horizontal axes. The proposed system also realizes the efficient and reliable power production system by the MPPT algorithm for the real-time recognition of the wind direction and velocity. An advanced switching algorithm for the battery charging system has been also proposed. Effectiveness of the proposed algorithm has been verified through the real experiments and the results are demonstrated.

탄소성 변형을 고려한 타이로드 고정 회전체의 동역학 해석 (Dynamic Analysis of Tie-rod-fastened Rotor Considering Elastoplastic Deformation)

  • 서동찬;김경희;이도훈;이보라;서준호
    • Tribology and Lubricants
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    • 제40권1호
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    • pp.8-16
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    • 2024
  • This study conducts numerical modeling and eigen-analysis of a rod-fastened rotor, which is mainly used in aircraft gas turbine engines in which multiple disks are in contact through curvic coupling. Nayak's theory is adopted to calculate surface parameters measured from the tooth profile of the curvic coupling gear. Surface parameters are important design parameters for predicting the stiffness between contact surfaces. Based on the calculated surface parameters, elastoplastic contact analysis is performed according to the interference between two surfaces based on the Greenwood-Williamson model. The equivalent bending stiffness is predicted based on the shape and elastoplastic contact stiffness of the curvic coupling. An equation of motion of the rod-fastened rotor, including the bending stiffness of the curvic coupling, is developed. Methods for applying the bending stiffness of a curvic coupling to the equation of motion and for modeling the equation of motion of a rotor that includes both inner and outer rotors are introduced. Rotordynamic analysis is performed through one-dimensional finite element analysis, and each element is modeled based on Timoshenko beam theory. Changes in bending stiffness and the resultant critical speed change in accordance with the rod fastening force are predicted, and the corresponding mode shapes are analyzed.

순시자속을 이용한 위치센서 없는 SRG의 운전 (The Position Sensorless Control of SRG using the Instantaneous Flux)

  • 김영조;오승보;김영석
    • 전력전자학회논문지
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    • 제7권5호
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    • pp.472-481
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    • 2002
  • 본 논문은 SRG(Switched Reluctance Generator)의 제어를 위하여 순시자속을 이용하여 위치를 추정하고, 추정한 위치에 근거하여 출력전압을 제어하는 방법이 제안되었다. SRG를 제어하기 위해서는 정확한 회전자의 위치정보가 필수적이다. 이러한 위치정보는 일반적으로 엔코더나 레졸버와 같은 정밀한 위치센서로부터 얻어진다. 그러나, 전자기적 간섭(Electromagnetic Interference), 진동, 열, 습도 등의 열악한 환경으로 인하여 정확한 위치를 검출하는데 많은 문제점을 가지고 있다. 따라서 이러한 문제점을 극복하기 위하여 위치·속도센서 없는 SRG의 제어기가 요구되어 진다. 본 논문에서는 SRG를 위한 새로운 위치·속도의 실시간 추정방법이 제안되었다. 순시자속은 측정한 전압과 전류에 의해 계산한 것과 위치와 자속 프로파일로부터 회전자의 위치를 추정하였다. 출력전압은 PID 제어 알고리즘에 의해 일정 제어되었다. 제안된 방법은 시뮬레이션을 통하여 확인하였고, DSP를 적용하여 구현하였다. 실험을 통하여 제안된 방법은 부하가 변동하더라도 일정하게 출력전압을 유지하고, SRG 제어가 안정됨을 확인하였다.

스마트무인기 파워효과 풍동시험 데이터 보정 (Data Correction of Wind Tunnel Test Results for Smart UAV Power Model)

  • 조태환;정진덕;최성욱;김양원;장병희
    • 한국항공우주학회지
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    • 제35권2호
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    • pp.130-135
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    • 2007
  • 스마트무인기 파워효과 풍동시험은 2005~2006에 3달여간 항공우주연구원 중형아음속풍동에서 수행되었다. 풍동시험 모델은 정적시험 모델을 활용하였고, 틸트로터 형태의 추진장치를 시험부에 고정하여 파워효과를 모사하였다. 파워효과는 기본적으로 로터가 장착된 시험과 로터가 장착되지 않은 시험의 차로 구해지나, 이 때 두 시험간의 흐름각 차이 및 지지부 간섭량 변화 등을 적절히 보정하여야 한다.

5축가공을 위한 공구경로 및 자세 제어 기술 (The Control Technology of Cutter Path and Cutter Posture for 5-axis Control Machining)

  • 황종대;임은성;정윤교
    • 한국기계가공학회지
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    • 제10권2호
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    • pp.1-8
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    • 2011
  • 5-axis NC machining has a good advantage of the accessibility of tool motion by adding two rotary axes. It offers numerous advantages such as expanding machining fields in parts of turbo machineries like impeller, propeller, turbine blade and rotor, reasonable tool employment and great reduction of the set-up process. However, as adding two rotary axes, it is difficult to choose suitable machining conditions in terms of cutter path and cutter posture at a cutter contact point. Therefore in this paper, it is proposed to decide suitable machining condition through an experimental method such as adopting various cutter paths, cutter postures types. Also, in order to increase the efficiency of 5-axis machining, it is necessary to minimize the cutter posture changes and create a continuous cutter path while avoiding interference. This study, by using an MC-space algorithm for interference avoidance and an MB-spline algorithm for continuous control, is intended to create a 5-axis machining cutter path with excellent surface quality and economic feasibility. finally, this study will verify the effectiveness of the suggested method through verification processing.

Design to Reduce Cost and Improve the Mechanical Durability of IPMSM in Traction Motors

  • Lee, Ki-Doek;Lee, Ju
    • 조명전기설비학회논문지
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    • 제28권5호
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    • pp.106-114
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    • 2014
  • The interior permanent-magnet synchronous motor (IPMSM) is often used for the traction motor of hybrid electric vehicles (HEVs) and electric vehicles (EVs) due to its high power density and wide speed range. This paper introduces the 120kW class IPMSM for traction motors in military trucks. This system, as a SHEV (series hybrid electric vehicle), requires a traction motor that can generate high torque. This study introduces a way to reduce costs by proposing a design approach that creates reluctance torque that can be maximized by varying the dq-axis inductance. If a model designed by a design approach meets the desired torque, the magnetic torque can be reduced by an amount equal to the increase in reluctance torque and consequently the amount of permanent magnets can be reduced. A reduction gear and high speed operation of motors are necessary for the miniaturization of the motor. Thus, a fairly large centrifugal force is generated due to the high speed rotation. This force causes mechanical interference between the rotor and the stator, and a design approach for adding an iron bridge is explained to solve the interference. In this study, the initial model and the improved model that reduces cost and improves mechanical durability are compared by FEA, and the models are produced. Finally, the FEM results were verified experimentally.

틸트로터 무인기의 날개-나셀 공력해석 (Aerodynamic Analysis on Wing-Nacelle of Tiltrotor UAV)

  • 최성욱;김철완;김재무
    • 한국전산유체공학회:학술대회논문집
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    • 한국전산유체공학회 2004년도 춘계 학술대회논문집
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    • pp.27-34
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    • 2004
  • In the Smart UAV Development Program, one of the 21c Frontier R&D Program, the tiltrotor has been studied as the concept of vehicle. The tiltrortor aircraft take-off and land in rotary wing mode like conventional helicopter, and cruise in fixed wing mode like conventional propeller airplane. For the conversion of the flight mode from helicopter to airplane, the nacelle located at wing tip has to be tilted from about 90 degrees of helicopter mode to about 0 degree of airplane mode. In this study, the aerodynamic characteristics of the wing with tilted nacelle is investigated using computation fluid dynamics technique. In order to feature out aerodynamic interferences between wing and nacelle, the flow calculations are conducted for the wing and the nacelle separately and for the combined geometry of wing and nacelle, respectively. Through this computations, not only the aerodynamic data-base for the wing-nacelle is constructed but also its contribution to the configuration design of the wing-nacelle is anticipated.

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수동형 마그네틱 베어링이 결합된 스텝 모터의 설계 (Design of a Step Motor with a Passive Magnetic Bearing)

  • 곽호성;최동훈;김승종
    • 한국소음진동공학회논문집
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    • 제16권12호
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    • pp.1201-1207
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    • 2006
  • This paper introduces a step motor with a passively levitated rotor which comprises a homopolar step motor and a passive magnetic bearing. Compared with conventional self-bearing motors which are mostly based on the active magnetic bearing technology, the proposed motor has a very simple structure and operating principle. For the levitation, it works just like passive magnetic bearings which use the repulsive force between permanent magnets. Halbach array is used to increase the bearing stiffness. On the other hand, its rotation principle is just the same with that of conventional motors. In this paper, we introduce the design scheme to avoid the flux interference possibly produced by electromagnets and permanent magnets, and show some results of FEM analysis to predict the performance of the proposed motor.