• 제목/요약/키워드: Propulsion motor

검색결과 678건 처리시간 0.033초

석유 시추선 전력 계통의 과도 안정도 해석 (Analysis on transient stability for drilling rigs power system)

  • 김윤식;김철호
    • Journal of Advanced Marine Engineering and Technology
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    • 제38권9호
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    • pp.1119-1124
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    • 2014
  • 본 논문은 석유시추선의 전력 계통 시스템의 비상시 전력 계통 해석에 대하여 기술하였다. 특히 석유시추선의 추진부하와 발전기의 탈락으로 인해 발생하는 전력계통 시스템에 미치는 영향을 검토하였다. 또한 고정 여자방식과 조속기의 제어 변수를 조정하여 임의의 사고 전후 정상상태로의 복귀까지 과도 안정도 해석으로 전력계통에 나타나는 현상을 관찰하였다. 전력계통 설계와 해석 및 과도 현상해석 프로그램인 ETAP(Electrical Transient Analysis Program)을 사용하였으며, 수치해석의 결과를 도출하여 그 특성을 분석하였다.

자기부상열차용 추진제어장치의 새로운 제어기법 (New control strategy of propulsion system for the Transit Maglev System)

  • 이은규;최재호
    • 한국철도학회논문집
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    • 제5권4호
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    • pp.267-275
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    • 2002
  • The traction drive system for the urban transit maglev system is described in this paper. To control the magnitude and frequency of the output voltage of induction motor transiently, the vector control strategy is generally used. But in case of the traction drive system for the railway vehicle, it is difficult to use the vector control caused by the one-pulse mode in the high speed region. Therefore, this paper proposes the control strategy combined the vector control in the low speed region and the slip frequency control in the high speed region. And also, the overmodulation PWM method is discussed to make the change to the one-pulse mode softly. The performance of the proposed traction drive system is verified by the MATLAB simulation results.

도시형 자기부상열차의 주행장치시스템 제작 및 성능 시험 (Manufacturing and Performance Test for Bogie System of Urban Maglev)

  • 유영돈;이남진;강광호;이원상;한형석
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2010년도 춘계학술대회 논문집
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    • pp.590-596
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    • 2010
  • Maglev vehicles levitated and propelled by electromagnet as non-contact between vehicle and guide rail is environmentally friendly transport system which have many advantages like ride comfort and guide way construction costs. As a goal of commercial operation at Incheon International Airport in 2012, development of vehicle is underway and proto-vehicle is test running at KIMM. The maglev bogie system of proto-vehicle, like railway vehicle, has functions to support weight of vehicle, transfer force of brake and propulsion and improve ride comfort through insulation of vibration and improve curve negotiation capability. The main components of a bogie are two modules consisted of electromagnetic, frame and linear motor, two tie beams to connect two modules and steering system to improve curve negotiation capability. The purpose of this paper is to describe general specification, structure, manufacturing process, performance testing, ride comfort of proto-vehicle and bogie system.

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중저속 자기부상열차에 적용 가능한 급전레일에 대한 검토 (A study on the power rail be of application to MAGLEV with middle-low speed)

  • 안영훈;노성찬;강승욱;현충일
    • 한국철도학회:학술대회논문집
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    • 한국철도학회 2007년도 추계학술대회 논문집
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    • pp.1451-1455
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    • 2007
  • MAGLEV(Magnetic Levitation) with Middle-low speed be classified as a kind of LRT(Light Rail Transit) in KOREA. Also this vehicle has adopted LIM propulsion method. The MAGLEV has adopted LIM type in operational or developing model in the world. The power rail of LIM is very similar with the 3th rail of LRT in the functional property but the structure and shape of power rail is different with that. WE have to search the optimal power rail system for Korean MAGLEV vehicle. In this paper, we suggest the conceptual design and direction of design for power rail of Korean MAGLEV developing.

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항공 운항 패턴을 고려한 고출력 소형 항공기 추진용 전동기 개발 (Development of High-Power Electric Motor for Small Aircraft Propulsion's Considering the Aircraft Flight Pattern)

  • 김용태;이진규;하재평;최거승;정연환;허윤
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2015년도 제46회 하계학술대회
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    • pp.886-887
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    • 2015
  • 선진 각국에서는 고효율, 친환경 에너지 공급 및 이용 기술, 그리고 효율적인 에너지 절약 기술 개발에 관한 연구 개발이 활발히 진행되고 있다. 이러한 연구 중 항공기 분야에서는 전동기로 프로펠러를 회전시키는 전기추진 항공기에 대한 관심과 수요가 증가하고 있다. 소형 항공기 추진용 전동기는 엔진과 함께 소형 항공기의 주 구동원으로서 중요성이 강조되고 있다. 또한 근래에 전동기의 비중이 커짐에 따라 고출력, 고효율화 되고 있는 추세이다. 본 논문에서는 항공 운항 패턴 중 이륙, 상승, 순항구간에 따라 각각 요구하는 성능을 만족하는 고출력, 고효율 전동기 개발에 대해 다루었다.

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고출력 소형 항공기 추진용 전동기의 항공 운항 패턴을 고려한 열 특성 분석 (Thermal Analysis Considering Aircraft Flight Pattern of High-Power Electric Motor for Small Aircraft Propulsion)

  • 김용태;이진규;하재평;정연환;허윤
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 2015년도 제46회 하계학술대회
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    • pp.888-889
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    • 2015
  • 세계적으로 석유 연료를 대체할 에너지원인 전기에너지에 대한 관심이 높아지고 있고, 전기자동차 뿐만 아니라 항공기에 사용할 고출력 전동기에 관한 연구 및 개발이 진행되고 있다. 고출력 밀도를 갖는 전동기의 경우 방열설계가 잘되어 있지 않으면, 발열로 인한 전동기의 성능과 내구성 및 수명이 단축되게 된다. 본 논문에서는 소형 항공기의 이륙, 상승, 순항구간에 요구되는 출력특성을 만족하도록 설계된 전동기에 대해, 항공 운항 Mission Profile의 출력 및 시간변동에 따른 온도 특성을 분석해 보았다.

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Levitation Control Experiment at Standstill in PM LSM Controlled-Repulsive Maglev Vehicle

  • Yoshida, Kinjiro;Takami, Hiroshi;Jozaki, Chiyuki;Kinoshita, Shiauo
    • 전력전자학회:학술대회논문집
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    • 전력전자학회 1998년도 Proceedings ICPE 98 1998 International Conference on Power Electronics
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    • pp.119-124
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    • 1998
  • This paper proposes a new repulsive-Maglev vehicle in which a vertical type PM linear synchronous motor (LSM) can levitate and propel simultaneously, independently of the vehicle speeds. A compact control method is developed which is based on the concept of controlling individually the levitation system by armature-current and the propulsion system by mechanical load-angle. The levitation-motion control experiments have carried out successfully together with positioning at standstill. The pitching motion has been compensated for very well by using the zero-phase-current control method proposed here.

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전자기 구동장치를 이용한 병렬형 6자유도 스테이지의 위치제어 (A Position Control for a Parallel Stage with 6 degrees of freedom Using Magnetic Actuators)

  • 이세한
    • 한국정밀공학회지
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    • 제22권7호
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    • pp.102-111
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    • 2005
  • In this paper, we address a position control for a parallel stage, which is levitated and driven by electric magnetic force. This consists of a levitating object (called platen) with 4 permanent magnetic linear synchronous motors in parallel. Each motor generates vertical force for suspension against gravity and propulsion force horizontally as well. This stage can generate six degrees of freedom motion by the vertical and horizontal force. A dynamic equation of the stage system is derived based on Newton-Euler method and it's special Jacobian matrix describing a relation between the limited velocity and Cartesian velocity is done. There are proposed two control methods for positioning which are Cartesian space controller and Actuator space controller. The control performance of the Cartesian space controller is better than the Actuator space controller in task space trajectory while the Actuator space controller is simpler than the Cartesian space controller in controller realization.

2단 변속시스템을 이용한 전기자동차의 변속제어 알고리즘 (Two-Speed Gear Shift System for Electric Vehicles)

  • 성기택;이준웅
    • 한국자동차공학회논문집
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    • 제8권1호
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    • pp.63-71
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    • 2000
  • A shift control algorithm of a newly developed two-speed gear shift system is proposed for electric vehicle applications. The algorithm is formulated according to the motor torque map and optimized to obtain the adequate propulsion characteristics for vehicle. Two speed gear system with shift control algorithm has proved greater efficiencies in terms of energy economy with its simplified hardware and software structures. The gear shifting is designed to be carried out by an actuator and the control signal from a vehicle control unit equipped with $\mu$-processor. The results of performances and efficiency of the algorithm by simulation and vehicle test are described.

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선형동기전동기의 전기자권선을 이용한 초전도 반발식 자기부상열차 시스템 (Electrodynamic Superconducting Maglev System with Quadruple Armature Windings)

  • 홍순흠;차귀수;이기식;한송엽
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1994년도 하계학술대회 논문집 A
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    • pp.199-201
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    • 1994
  • In this paper, The characteristics of the new superconducting maglev system which has quadruple armature windings is examined. This system can generate guidance force and levitation force as well as propulsion force by single ground coil. The time-domain analysis method and phasor analysis method are derived to analyze the characteristics of the proposed system. From the numerical examples for two kind of armature winding configurations, it is shown that the levitation force and guidance force can be generated by single armature winding of the linear synchronous motor without any other ground coils for levitation and guidance, and that double layer configuration has better characteristics in the qualitive characteristics. like as efficiency, pulsation of the electromagnetic forces and drag ratio, than the single layer configuration.

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