• 제목/요약/키워드: Spin Motor

검색결과 33건 처리시간 0.022초

고속공작기계용 모터내장형 주축의 열거동 및 자켓냉각특성 해석 (Analysis Of The Thermal Behavior and Jacket Cooling Characteristics of Motor Integrated Spindle for High Speed Machine Tool)

  • Park, D.B.;Kang, J.P.;Song, J.B.
    • 한국정밀공학회지
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    • 제14권2호
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    • pp.33-40
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    • 1997
  • Recently, there are an increasing needs for high speed rotating spindle which is an important mechanical ele- ment for a high efficiency machine tool in order to shorten machining time and cut production costs. The heat gen- eration is the most important problem in the motor integrated spindle. In this study, the effects of temperature distribution and thermal behavior according to the oil-air lubrication and cooling conditions are investigate theo- retically and experimentally on the motor-integrated spindle under unloading condition. The experimental spin- dle system is composed with the angular contact steel ball bearings, oil-air lubrication, air or oil jacket cooling system. To analyze the thermal behavior and cooling characteristics for the motor integrated spindle, the analysis using the finite element method is carried out. The analytical results are compared with the experimental results.

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디그레시브 펀 권사(Degressive Pirn Winding)를 위한 기구학적 권사 제어 알고리듬에 관한 연구 (A Study on the Kinematic Winding Control Algorithm for Degressive Pirn Winding)

  • 최영휴;정원지;김광영
    • 한국정밀공학회지
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    • 제20권3호
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    • pp.133-139
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    • 2003
  • Direct motor-driven winding has been increasingly applied in winding machinery. However, it is necessary to analyze the kinematics of winding prior to developing the winding control algorithm, because direct motor-driven winding machine should be operated in accordance with the pre-determined kinematic information for the winding control. This paper presents the kinematics of the degressive winding method and its kinematic winding control algorithm in order to wind the required volume of a pirn package in a desired shape. The proposed algorithm can give the appropriate yarn speed, traverse speed, and the spin speed of the spindle at every traverse stroke, which are utilized for controlling the spindle motor and traverse motor of the winding machine. Computer winding simulations showed that the proposed algorithm is successful in the degressive pirn winding.

가스터빈 초기 구동용 시동시스템의 제동특성 연구 (Study on the Braking Characteristics of Starting System Used for Initial Spin-up of Gas Turbine)

  • 송주영;박준철;이기훈;김성현;남삼식
    • 한국추진공학회:학술대회논문집
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    • 한국추진공학회 2011년도 제37회 추계학술대회논문집
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    • pp.379-382
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    • 2011
  • 발전용 가스터빈 초기 구동용 시동시스템의 제동특성 평가를 위해 시동모터 단독 무부하 시험과 엔진 장착 부하시험을 수행하였다. 시동모터의 제동저항 용량 차이에 따른 제동 성능의 실험적 평가를 통해 가스터빈 시동과정 중 비상정지 상황에서 안정적인 제동특성을 확보하기 위한 정량적 데이터를 확보하였다. 본 연구를 통해 가스터빈의 시동 신뢰성과 안정성을 제고하기 위한 최적의 시동모터 제동저항 선정이 가능하게 되었다.

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궤도경사각을 가진 통신위성의 빔 포인팅에 대한 연구 (THE BEAM POINTING OF COMMUNICATIN SATELLITE IN GEOSYNCHRONOUS INCLINED ORBIT)

  • 김방엽;최규홍
    • Journal of Astronomy and Space Sciences
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    • 제12권1호
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    • pp.112-122
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    • 1995
  • 1995년 7월에 발사될 무궁화호 통신위성이 원지점 모터 분사의 오차로 인해 예정된 지구정지궤도진입에 실패했을 경우를 가정하였다. 원지점 모터 분사시에 연료 저장 상태의 불균형, 추력축의 회전 등으로 인하여 원지점 모터 분사가 잘못되어, 통신위생이 정지 궤도 요소 충 궤도 경사각이 $0^{\circ}$가 아닌 지구 통주기 궤도를 도는 상황을 모의실험하였다. 이 때, 궤도 의 진화과정을 섭통론을 통해 분석하였고 이심율과 경사각의 변화를 조사하였다. 궤도 경사각이 $0^{\circ}$가 아닌 지구동주기 궤도를 도는 통신위성이 8자 궤적을 그리게 되면 빔 지향점도 위성의 이동에 따라 움직이는데 이 문제를 해결하기 위해 위성의 roll각을 조정하여 빔 지향점을 고정시킬 수 있는 알고리즘을 무궁화호에 적용시켰다. 그리고 승교정과 강교점을 통과할 때 일어나는 펀파면의 회전 현상도 통신 효율에 큰 영향을 주는데, 편파변의 회전 현상을 줄일 수 있는 yaw각 조정방법올 역시 무궁화호에 적용했다.

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Experimental Evaluation on Power Loss of Coreless Double-side Permanent Magnet Synchronous Motor/Generator Applied to Flywheel Energy Storage System

  • Kim, Jeong-Man;Choi, Jang-Young;Lee, Sung-Ho
    • Journal of Electrical Engineering and Technology
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    • 제12권1호
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    • pp.256-261
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    • 2017
  • This paper deals with the experimental evaluation on power loss of a double-side permanent magnet synchronous motor/generator (DPMSM/G) applied to a flywheel energy storage system (FESS). Power loss is one of the most important problems in the FESS, which supplies the electrical energy from the mechanical rotation energy, because the power loss decreases the efficiency of energy storage and conversion of capability FESS. In this paper, the power losses of coreless DPMSM/G are separated by the mechanical and rotor eddy current losses in each operating mode. Moreover, the rotor eddy current loss is calculated by the 3-D finite element analysis (FEA) method. The analysis result is validated by separating the power loss as electromagnetic loss and mechanical loss by a spin up/down test.

Functional Magnetic Resonance Imaging with Arterial Spin Labeling: Techniques and Potential Clinical and Research Applications

  • Kim, Ju Ho;Choi, Dae Seob;Park, Sung Eun;Choi, Ho Cheol;Kim, Seong Hu
    • Investigative Magnetic Resonance Imaging
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    • 제21권2호
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    • pp.91-96
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    • 2017
  • Purpose: To describe technical methods for functional magnetic resonance imaging (fMRI) study with arterial spin labeling (ASL) compared to blood oxygenation level-dependent (BOLD) technique and discuss the potential of ASL for research and clinical practice. Materials and Methods: Task-based (n = 1) and resting-state fMRI (rs-fMRI) (n = 20) were performed using ASL and BOLD techniques. Results of both techniques were compared. Results: For task-based fMRI with finger-tapping, the primary motor cortex of the contralateral frontal lobe and the ipsilateral cerebellum were activated by both BOLD and ASL fMRI. For rs-fMRI of sensorimotor network, functional connectivity showed similar results between BOLD and ASL. Conclusion: ASL technique has potential application in clinical and research fields because all brain perfusion imaging, CBF measurement, and rs-fMRI study can be performed in a single acquisition.

손실을 고려한 500W급 마이크로 가스터빈 발전기용 전동발전기의 요구동력 및 요구효율 선정 (Prediction of Power and Efficiency Requirement of Motor/generator for 500W Class Micro Gas Turbine Generator Considering Losses)

  • 박철훈;최상규;함상용
    • 한국유체기계학회 논문집
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    • 제14권5호
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    • pp.24-30
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    • 2011
  • 500W class MTG(Micro turbine generator) operating at 400,000 rpm is under development. From the cycle analysis, it is decided that the self-sustaining speed of MTG is 200,000rpm and the generating speed is 400,000 rpm. Therefore, motor should be designed so that it is able to rotate the rotor up to 200,000rpm and generator should designed so that it is able to generate 500W output at 400,000rpm. First step to design motor/generator is to determine the power and efficiency requirement. Not only the power into the compressor and from the turbine at the operating speed but also the mechanical and electrical losses should be considered in determining the power and efficiency requirement. This study presents the procedure and the results of determining the power and efficiency requirement considering the mechanical and electrical losses depending on the rotating speed which is measured from the experiment.

자이로 구동장치를 이용한 공중물체의 자세제어 및 안정화 (An Attitude Control and Stabilization of an Unstructured Object using CMG Subsystem)

  • 이건영;권만오
    • 대한전기학회논문지:시스템및제어부문D
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    • 제49권8호
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    • pp.459-466
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    • 2000
  • In this paper, we propose an attitude controller for an unstructured object using CMG(Control Moment of Gyro) subsystem, which has a stabilizer function. The CMG subsystem consists of one motor for spinning the wheel and the other motor for turning the outer gimbal. While the wheel of CMG subsystem is spinning at high speed, applying force to the spin axis of the wheel leads the torque about the vertical axis. We utilize the torque to control the attitude of object in this study. For the stabilizer function, in additiion, holding the load at the current position, the power applied to the gimbal motor of CMG will be cut, which result in the braking force to stop the load by gyro effect. However, due to the gear reduction connected to outer gimbal, slow load motion cannot generate the braking force. Thus, in this study, we are willing to make a holding force by applying control power to the gimbal motor from the signal of piezoelectric gyroscopic sensor that detected the angular velocity of the load. These two features are demonstrated in experiment, carrying a beam with crane. As a result, load was started to rotate by controlling gimbal positiion and was stopped by turning off the gimbal power. Moreover, slow movement of the load was also rejected by additional control with gyroscopic sensor.

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공중 물체의 자세 제어를 위한 자이로 엑츄에이터 설계 (Design of a Gyro Actuator for the Attitude Control of an Unstructured Object)

  • 정영구;이건영
    • 대한전기학회:학술대회논문집
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    • 대한전기학회 1998년도 하계학술대회 논문집 B
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    • pp.490-492
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    • 1998
  • An intention of this paper is design of a gyro actuator for the attitude control of an unstructured object. It is well known that the attitude control of an object hanging with wire is not easy using usual actuators. Even though an actuator such as a pan can be used for control of the object, it is difficult to meet a desired control objectives. We, for this reason, propose a gyro actuator for the attitude control of an unstructured object. The proposed gyro actuator consists of two motors. The first motor is responsible to spin the wheel and the second motor is used to turn the outer gimbal. Appling the torque to the second motor, which results in the turn of the outer gimbal, torque about the vertical axis will be obtained while a wheel of the gyro is spinning constantly. This torque is used to control the attitude of the object attached. The aim of this paper is of deriving the transfer function of the actuator and presenting the guideline of the design parameters such as the weight and the dimension of the wheel, motors, and the load capacity. Simulations to the mathematical model which has a state feedback control are conducted to show the validity of the proposed gyro actuator.

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유연복합재 구동축의 동특성에 관한 실험 분석 (Experimental Investigation Into the Dynamic Characteristics of Flexible Matrix Composite Driveshafts)

  • 신응수
    • 한국공작기계학회논문집
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    • 제15권2호
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    • pp.93-98
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    • 2006
  • This study provides a comprehensive experimental study on the dynamic characteristics of a flexible matrix composite(FMC) driveshaft. A primary objective is to verify the analytic results of the FMC drivetrain based on the equivalent complex modulus approach and the classical lamination theory. A test rig has been constructed, which consists of a FMC shaft, a foundation beam, bearings, external dampers and a driving motor. The frequency response functions and transient responses are obtained from the external excitation and the spin-up testings. It turns out that the analytic results are in good agreement with the experimental ones.