• Title/Summary/Keyword: Micro Motor

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CHARATERISTIC IMPROVEMENT OF 5 PHASE STEP MOTOR BY USING MICRO-STEP DRIVER IN X-Y AXIS SOLDERING MACHINE

  • Park, Chul-Soon;Kim, Sung-Hoon;Ahn, Ho-Kyun;Park, Seung-Kyu
    • Proceedings of the KIPE Conference
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    • 1998.10a
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    • pp.97-100
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    • 1998
  • In this paper, micro step driving method is used for the high performance motion control and low vibration and low noise in an X-Y axis soldering machine for factory automation. The improvement of the electrical and mechanical driving characteristic of a stepping motor is achieved by applying microstep driver.

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One-Chip and Control System Design of Low Cost for Micro-stepping Drive of 5-Phase Stepping Motor (5상 스테핑 모터의 마이크로스텝 구동을 위한 저가형 전용 칩 및 제어시스템 설계)

  • 김명현;김태엽;안호균;박승규
    • The Transactions of the Korean Institute of Power Electronics
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    • v.9 no.1
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    • pp.88-95
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    • 2004
  • Micro stepping method is adopted in order to eliminate effectively the resonant phenomena and to increase the positional resolution. Exist micro-step method by using Sinusoidal waveform, drive circuit is complex by using micro controller and ROM, it have fault on cost Increase. This paper proposed trapezoidal current wave form for simple control circuit and micro stepping method by using a low cost controller. This paper proposed method verify by using CPLD(EPM9320RC208-15) of low cost. This paper make experiment that comparison of exist method and proposed method. This paper obstruct a escape of motor by using high speed detect.

Parametric Study on the Design of Hybrid Motor for Air Launch System (공중발사체를 위한 하이브리드 모터 설계)

  • Gwon, Sun Tak;Lee, Chang Jin
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.31 no.3
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    • pp.72-78
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    • 2003
  • In this paper, the feasibility study and the parametric design of hybrid motor with HTPB/LOX were conducted for micro air launch system. Design results were compared with 1st stage of Pegasus XL for verification of hybrid motor. Results showed that hybrid motor replace solid booster if Isp of hybrid motor reaches 330sec. In addition, mission analysis was established for micro air launch system, and parametric design was conducted with design variables: number of port, initial oxidizer flux, and chamber pressure. And the region of Isp was identified by parametric study which satisfied design constraints and mission analysis.

A Design of Impact Control Device for High-speed Mounting of Micro-Chips (소형 칩의 고속 표면실장을 위한 충격력 제어 장치의 설계)

  • 이덕영;김병만;심재홍;조형석
    • 제어로봇시스템학회:학술대회논문집
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    • 2000.10a
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    • pp.121-121
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    • 2000
  • This paper presents a design of macro-micro system for high-speed mounting of micro-chips. A macro motion device is driven by DC servomotor and ball screw mechanism. To obtain fast response, a micro motion device utilizes a precision elector magnetic actuator In order to reduce peak impact force, We evaluate the design parameters that have an effect on it. And a characteristic of response is simulated using PID controller in velocity and force control.

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Experimental Study on Thermal Insulation and Cooling for Rotor/Bearing Area in 500W Class Micro Gas Turbine Generator (500W급 마이크로 가스터빈 발전기 회전체-베어링부의 단열 및 냉각 성능에 대한 실험적 연구)

  • Park, Cheol Hoon;Choi, Sang Kyu;Ham, Sang Yong
    • The KSFM Journal of Fluid Machinery
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    • v.17 no.3
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    • pp.19-24
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    • 2014
  • Development of long-term mobile energy sources for mobile robots or small-sized unmanned vehicles are actively increasing. The micro gas turbine generator (MTG) is a good candidate for this purpose because it has both of high energy density and high power density, and 500W class MTG is under development. The designed MTG can be divided into 2 main parts. One part consists of motor/ generator and compressor, and the other one consists of combustor, recuperator and turbine. 500W class MTG is designed to operate at ultra-high speed of 400,000 rpm in high turbine temperature over $700^{\circ}C$ to improve the efficiency. Because the magnetism of NdFeB permanent magnet for the motor/generator could be degraded if the temperature is over $150-200^{\circ}C$, MTG needs the thermal insulation to block the heat transfer from combustor/turbine side to motor/generator side. Moreover, the motor/generator is allocated to get the cooling effect from the rapid air flow by the compressor. This study presents the experimental results to verify whether the thermal insulator and air flow are effective enough to keep the motor/generator part in the low temperature less than $100^{\circ}C$. From the motoring test by using the high temperature test rig, it was confirmed that the motor/generator part could maintain the temperature less than $50^{\circ}C$ under the condition of 1.0 bar compressed air.

Fundamental Experiment for Solid Propellant Micro-Propulsion devices (고체추진 마이크로 추진 장치에 대한 기초실험)

  • Kim Youn-ho;Jung Sung-chul;Oh Hwa-young;Huh Hwanil
    • Proceedings of the Korean Society of Propulsion Engineers Conference
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    • v.y2005m4
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    • pp.39-43
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    • 2005
  • In this paper, we describe the contents of the achievement of basic experiments for manufacturing and evaluating a micro-rocket using solid propellant, as the device of the micro thrust generator which can be used for attitude control of satellites. We try to analyze performance of the rocket through visualization of the motor jet, and adopt various ignition methods to obtain confidence in ignition problem. For this purpose, we develop and test two different types of thrust measurement system.

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Induction motor Modeling and Converter circuit Simulation using Pspice (Pspice를 이용한 유도전동기 모델링과 전력변환회로 시뮬레이션)

  • 서영수;백동현;조문택;이상봉
    • Proceedings of the KIPE Conference
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    • 1997.07a
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    • pp.148-151
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    • 1997
  • Pspice is not offered a library of mechanical factor like DC Motor, Induction Motor which is needed in Power Electronics field. Therefore, Induction Motor was made library by Equibalent circuit in this study. This model is applied in Voltage-Type inverter and is investigated its characteristics. IGBT is tested by two methods of Macro and Micro Modeling as semiconductor. PWM signal is used of pulse signal. Voltage and current, speed was simulated for assurance of model.

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Motor Speed Detection Algorithm Using Three Phase Taco-Generator (3상 타코 제너레이터를 이용한 전동기 속도검출 알고리즘)

  • Choi, Jung-Soo;Cho, Kyu-Min
    • Proceedings of the KIEE Conference
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    • 1995.07a
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    • pp.278-281
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    • 1995
  • In this paper, a instantaneous speed measurement methode using a three phase sinusoidal taco-generator is described and it's simulations are developed. The proposed methode can easily detect the motor speed by using that the output voltage of taco-generator is propotion to the motor speed. Because the proposed methode consists of some calculation, the proposed system can be implemented with analog devices or micro processor conveniently. From the simulation resualts, the proposed measurement methode can acculately detect the real motor speed over wide range.

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A comprehensive study of spin coating as a thin film deposition technique and spin coating equipment

  • Tyona, M.D.
    • Advances in materials Research
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    • v.2 no.4
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    • pp.181-193
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    • 2013
  • Description and theory of spin coating technique has been elaborately outlined and a spin coating machine designed and fabricated using affordable components. The system was easily built with interdisciplinary knowledge of mechanics, fluid mechanics and electronics. This equipment employs majorly three basic components and two circuit units in its operation. These include a high speed dc motor, a proximity sensor mounted at a distance of about 15 mm from a reflective metal attached to the spindle of the motor to detect every passage of the reflective metal at its front and generate pulses. The pulses are transmitted to a micro-controller which process them into rotational speed (revolution per minute) and displays it on a lead crystal display (LCD) which is also a component of the micro-controller. The circuit units are a dc power supply unit and a PWM motor speed controlling unit. The various components and circuit units of this equipment are housed in a metal casing made of an 18 gauge black metal sheet designed with a total area of 1, $529.2cm^2$. To illustrate the use of the spin-coating system, ZnO sol-gel films were prepared and characterized using SEM, XRD, UV-vis, FT-IR and RBS and the result agrees well with that obtained from standard equipment and a speed of up to 9000 RPM has been achieved.