• Title/Summary/Keyword: Electromagnet

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Stability Analysis of a Maglev Vehicle Utilizing Electromagnetic Suspension System (상전도 흡인식 자기부상열차의 주행 안정성 해석)

  • Han, Hyung-Suk;Kim, Sook-Hee;Yim, Bong-Hyuk;Hur, Young-Chul
    • Transactions of the Korean Society of Automotive Engineers
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    • v.16 no.3
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    • pp.118-126
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    • 2008
  • The levitation stability of a Maglev vehicle utilizing electromagnetic suspension is primarily influenced by the deformation, roughness, and vibration of the guideway. Optimum design for both the vehicle and the guideway is desirable in order to reduce guideway construction cost, while meeting requirements for stability and ride quality. This paper presents an analysis of the levitation stability of the UTM-01, an urban Maglev vehicle, using a numerical simulation. The ODYN/Maglev, a dynamics analysis program, is used to simulate dynamics to evaluate the stability. A running test of the UTM-01 is also carried out to verify the results of the simulation. Using the simulation results, the levitation stability of the UTM-01 can be numerically analyzed at a variety of vehicle speeds.

Study of Microrobot formed the Wing of a Insect (곤충 날개를 형상화한 마이크로로봇의 연구)

  • 김종걸;이건영
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.424-424
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    • 2000
  • The implementation of a insect-based flying microrobot has been previously proposed as using magnetic force. The flying principle of a butterfly is different from that of a airplane, which obtain lifting force above the wings by a air stream with low pressure. Butterflies obtain lifting force below the wings by flapping. They can fly when drag during the down stroke is greater that during the up stroke. The structure of flying microrobot must satisfy these condition. And that must be manufacture lightly and keep balance for rising to the air sufficiently. Moreover the efficiency of an electromagnet is high and the flux density is sustained uniformly and widely Nevertheless these condition is satisfied, the implementation of a flying microrobot is very difficult as the flying microrobot has to fly without guides or sensor. We propose differently a new model il] comparison with that other paper has suggested. This imitates the form of the Korean shield-shaped kite.

Measurement of Effective Linewidth for Ca-Zr Substituted YIG (Ca-Zr치환 YIG의 유효 선폭 측정)

  • 김약연;한진우;한기평;김덕준;이상석;최태구
    • Journal of the Korean Magnetics Society
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    • v.10 no.1
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    • pp.22-29
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    • 2000
  • The effective linewidth was measured using the conventional cavity perturbation method at 9.43 GHz in room temperature for Ca-Zr substituted yttrium iron garnet plate. The experimental set-up consists of the network analyzer, the electromagnet and the cylimdrical TE001 cavity. Measurement was performed in the static magnetic field perpendicular to the sample plane. The real and imaginary parts of diagonal component of the microwave susceptibility tensor are obtained from the resonance frequency and the quality factor Q of the cavity. Variations of the effective linewidth was qualitatively explained with the spin wave scattering theory.

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Performance Study of Magnetic Bearing Considering the Performance Limit (자기 베어링의 성능한계를 고려한 작동특성 연구)

  • 장인배;한동철
    • Journal of KSNVE
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    • v.5 no.1
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    • pp.59-65
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    • 1995
  • In this study, we investigated the operational limit of magnetic bearing-rotor system due to the maximum force limit and slew rjate limit of the electromagnetic actuator as a function of the time dependent control characteristics. The feedback gain of the controller varies the current of the electromagnet coil with the motion of the rotor. The distorsion of magnetic force due to the slew rate limit is not occurred jup to 30, 000 rpm in the magnetic bearing that we have a close relation with the rotational speed and vibration level of the rotor and the proportional gain of the controller. Therefore the maximum force limit determines the maximum allowable orbit radius of the magnetic bearing-rotor system. The maximum allowable vibration levels are exponentially decreased according to the increment of rotational speed and proportional gain of the controller.

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A study on the effects of variously configured magnets on the characteristics of inductively coupled plasma (자장의 배열 및 형태가 유도결합형 플라즈마에 미치는 효과에 관한 연구)

  • 황순원;이영준;유지범;이재찬;염근영
    • Journal of Surface Science and Engineering
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    • v.32 no.4
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    • pp.513-520
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    • 1999
  • In this study, we investigated the effects of variously configured magnets on the characteristics of the plasmas to enhance plasma uniformity and density of an inductively coupled plasma source. As the magnets, Helmholtz type axial electromagnets and various multi-dipole magnets types around the chamber wall were used. To characterize the plasma as a function of the combination of the magnets and magnetic field strengths, ion density, electron temperature, and plasma potential were measured using an electrostatic probe along the chamber diameter for Ar plasmas. The measured maximum ion densities were $8$\times$10^{ 11}$$cm^{-3}$ with 600W inductive power and at 5mTorr of operational pressure and the uniformity of ion density was less than 5.9% at 2mTorr of operational pressure. The combination of an optimized multi-dipole magnet type and an axial electromagnet showed the lowest electron temperature (3eV) and plasma potential ($34V{p}$ )

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3D Shape Optimization of Electromagnetic Device Using Design Sensitivity Analysis and Mesh Relocation Method (설계민감도해석과 요소망 변형법을 이용한 전자소자의 3차원 형상최적화)

  • ;Yao Yingying
    • The Transactions of the Korean Institute of Electrical Engineers B
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    • v.52 no.7
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    • pp.307-314
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    • 2003
  • This paper presents a 3D shape optimization algorithm for electromagnetic devices using the design sensitivity analysis with finite element method. The structural deformation analysis based on the deformation theory of the elastic body under stress is used for mesh renewing. The design sensitivity and adjoint variable formulae are derived for the 3D finite element method with edge element. The results of sensitivity analysis are used as the input data of the structural analysis to calculate the relocation of the nodal points. This method makes it possible that the new mesh of analysis region can be obtained from the initial mesh without regeneration. The proposed algorithm is applied to the shape optimization of 3D electromagnet pole to net a uniform flux density at the target region.

Analysis of the Operational Characteristics of High-Tc Superconducting Power Supply Using by BSCCO Tape (BSCCO 고온초전도선재를 이용한 고온초전도전원장치의 동작특성 해석)

  • Ahn, Min-Cheol;Kim, Ho-Min;Yoon, Yong-Soo;Ko, Tae-Kuk;Lee, Sang-Jin;Han, Tae-Su
    • Proceedings of the KIEE Conference
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    • 2001.04a
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    • pp.12-14
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    • 2001
  • This paper deals with the fabrication and characteristic experiment of a high-Tc superconducting (HTSC) power supply using by Hi-2223 tape. The purpose of this research is to apply real HTSC load. This system consists of two heaters, an electromagnet, a Bi-2223 solenoid and a Bi-2223 pancake load. In the experiment, 17sec and 8.5sec were used for pumping period. Mechanism of the superconducting switch is used for heater-trigger. In experiment, the pumping-current has reached about 1.2A.

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An Experiment Study of Semi-Active Damper Using Magnetic fluid (자성유체를 이용한 반능동식 댐퍼에 관한 실험적 연구)

  • Hwang, Seung-Sik
    • The KSFM Journal of Fluid Machinery
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    • v.7 no.4 s.25
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    • pp.24-31
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    • 2004
  • The aim of this study is to provide fundamental information for the development of Semi-Active Damper Using Magnetic fluid. To achieve the aim, the damping effect of magnetic fluid is investigated by experiments that the diameter of inner circular bar and the input amplitude were varied in the magnetic field generated by the permanent magnet and the electromagnet coil. From the study, the following conclusive remarks can be made. As the diameter of inner circular bar and input amplitude increase, the damping effect is improved. This is explained by the fact that as the contact area between inner circular bar and magnetic fluid increases, the increase of friction lowers kinematic energy. If the magnetic field is generated, the damping effect is improved. This is explained the assumption that as the intensity of magnetic fluid particle increases, there is virtual mass phenomenon.

Manufacturing and Dynamic Performance test for Prototype Bogie of half Maglev vehicle (자기부상열차 시험용 1/2차량 대차제작과 주행성능 실험)

  • Lee, Nam-Jin;Han, Hung-Suk;Lee, Wan-Sang;Kim, Chul-Geun
    • Proceedings of the KSR Conference
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    • 2009.05a
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    • pp.1575-1580
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    • 2009
  • Maglev vehicle has two kinds of suspension system such as a secondary suspension with air-spring and a primary suspension as electromagnetic suspension which composed of electromagnet, magnet driver, controller and sensors. The interaction between each dynamic component of vehicle and track effects the stability and running performance. To achieve the specified performance of vehicle, many various approaches of research were tried, then as the result of these efforts, the first commercial operating with Maglev will start soon. The bogie for revenue service from 2012 has some significant modifications compared to the previous one, and to verify the changes the half prototype vehicle was manufactured and took the running performance test. In this report, we will introduce the stage of manufacturing and report results of dynamic performance tests to verify new concept of bogie mechanism.

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Air Gap Change of a Maglev Vehicle at the Moment a Linear Induction Motor Runs (자기부상열차 고가 선로 구조특성에 따른 부상공극 응답)

  • Shin, Hyeon-Jae;Han, Hyung-Suk;Lee, Jong-Min;Rho, Kyu-Sok
    • Proceedings of the KSR Conference
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    • 2009.05a
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    • pp.1213-1217
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    • 2009
  • The air gap between electromagnet and guiderail in an EMS-type Maglev vehicle must be maintained within an allowable deviation by controlling the voltage on the magnet. In this type of vehicle, the air gap response is strongly dependent on the structural characteristics of the elevated guideway, such as stiffness, damping and mass. For this reason, the dynamic interaction between the vehicle with electromagnets and the elevated guideway must be understood to ensure safe running. The response of the air gap to guideway characteristics such as mass, stiffness, and damping are analyzed through vehicle tests over different guideways. Through such tests, the design requirements for Maglev vehicles and elevated guideways can be established, improving levitation stability.

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