• Title/Summary/Keyword: Required thrust

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Position Accuracy Error Analysis in 2 Phase 8 Pole HB Type LPM (2상 8극 HB형 LPM의 위치오차 해석)

  • Kim, Sung-Hun;Lee, Eun-Woong;Lee, Dong-Ju
    • Proceedings of the KIEE Conference
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    • 1997.11a
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    • pp.38-41
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    • 1997
  • As the LPM is used for position accuracy decision device it is required that both the reason of posion error and the definition of position itself should be cleared. In this study, the precision of the position decision of LPM is affected by the geometrical shape such as tooth shape or processing accuracy. By using the analysis of magnetic circuit, we calculated the permeance come up with the gap. Once the thrust force has been obtained, the permeance due to the mechanical error of the pole pitch and the tooth pitch becomes the error of thrust force. We confirmed as well that it is being affected by the difference due to the variation of the airgap permeance.

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Combustion Characteristics of High Pressure Thrust Chamber with Single Coaxial Swirl Injector (이중와류 분사기를 적용한 고압 모델 연소기의 연소 특성 연구)

  • Seo, Seong-Hyeon;Lee, Kwang-Jin;Han, Yeoung-Min;Kim, Seung-Han;Kim, Jong-Gyu;Seol, Woo-Seok
    • 한국연소학회:학술대회논문집
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    • 2003.12a
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    • pp.131-136
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    • 2003
  • Experimental study on combustion characteristics of double swirl coaxial injectors has been conducted for the assessment of critical design parameters of injectors. A subscale thrust chamber has been fabricated with a water-cooled copper nozzle, which allows a chamber to be reused without replacing parts. Two different designs of injectors have been tested for the understanding of the effects of recess length on combustion. Clearly, the recess length drastically affects the combustion efficiency and hydraulic characteristics of the injector. Internal mixing of propellants in the injector with the recess number of two increases a combustion efficiency and reveals sound combustion although a pressure drop required for the similar amount of mass flow rates increases compared with the injector of the recess number of one.

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Improvement of the Thermal Behavior of the Secondary Part of Synchronous Linear Motors with High Speed and Thrust (고속.대추력 동기식 리니어모터 세컨더리 파트의 열특성 향상)

  • Eun, In-Ung
    • Journal of the Korean Society for Precision Engineering
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    • v.28 no.4
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    • pp.505-512
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    • 2011
  • Linear permanent magnet synchronous motors utilize high-energy product permanent magnet to produce high thrust, velocity and acceleration. Such motors are finding applications requiring high positioning accuracy and speed response, for example, machine tools, in the absence of mechanical gears and ball screw systems. A disadvantage of the linear motors is high power loss in comparison with rotary motors. For the application of the linear motors to machine tools, it is required to use water coolers and to improve the thermal behavior through insulation and structure optimization or control strategies. This paper presents the function of the secondary part of the linear synchronous motor as to the thermal behavior and the improving method. The result shows cooling pipe combined with an insulation layer is a suitable design for improving of the thermal behavior.

Design and The Characteristic Analysis of the linear pulse motor for X-Y table (X-Y테이블 구동용 리니어 펄스모터의 설계와 특성해석)

  • Park, Chang-Soon;Kwon, Tae-Gun
    • Proceedings of the KIEE Conference
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    • 2001.04a
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    • pp.182-184
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    • 2001
  • Linear pulse Motor(LPM) are used a field where smooth linear motion is required, and it's position accuracy higher than that of a lead. According to the advantage such as simplicity of mechanical frame, high reliability, precise open_loop operation, low inertia etc LPM is applied largely where it have made motor of this kind more and more attractive in many application areas such as factory automation and high speed positioning. This paper is researched to analyze for thrust force characteristic of hybrid LPM. Both the thrust and normal force are very sensitive to the airgap and tooth pitches of the force and platen. To find the optimal design parameter on the hybrid LPM for the embroidery machine. For the field analysis, the finite element method(FEM) is employed for calculating the force. The reluctance models will be used the magnetic permeance of airgap under static-conditions. The forces between forcer and platen have been calculated using the virtual work mathod.

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A Safety Evaluation of Motor-Operated Valves of Nuclear Power Plants By Using PPM (PPM을 이용한 원자력 발전소 모터구동밸브의 안전성 평가)

  • Park, Su-Ki;Kim, Tae-Woong;Jeong, Hee-Kweon;Park, Sung-Keun
    • Proceedings of the KSME Conference
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    • 2001.06b
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    • pp.718-723
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    • 2001
  • PPM (Performance Prediction Methodology) developed by EPRI was introduced and applied to calculate the stem thrust of 3 and 4 inches flexible-wedge gate valves. The calculated stem thrusts of open and close strokes including cracking were compared with the results measured at in-situ differential pressure tests. The comparison has shown that PPM is an extremely conservative method to predict the minimum required stem thrust to operate motor-operated valves in a design basis accident condition of nuclear power plants.

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A Evaluation Method of Operational Performance for Air-operated Gate Valve (공기구동 게이트밸브의 운전 성능평가 방법에 관한 연구)

  • Kim, Dae-Woong;Park, Sung-Keun;Kang, Shin-Cheul;Kim, Yang-Suk
    • The KSFM Journal of Fluid Machinery
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    • v.12 no.2
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    • pp.31-38
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    • 2009
  • The valve performance has been evaluated from the theoretical equation based on design information such as packing thrust, spring preload and friction coefficient(${\mu}$). The accuracy of those data can be lower than that of vendor's initial design data. Especially, the friction coefficient can be degraded with time than the original condition and the valve performance calculated using the previous friction coefficient can not be available. Accordingly, this paper is describing a new performance evaluation method of valve based on diagnostic test data which are acquired from a site valve tested in static and dynamic conditions. Especially, this paper provides a new method using friction coefficient(${\mu}$) which is derived from the diagnostic test data acquired in the valve's design basis condition.

A Study on the Precision Position Control for the Linear BLDC Motor (선형 브러시리스 DC 모터의 정밀 위치제어에 관한 연구)

  • Chun, Yeong-Han;Kim, Ji-Won;Jeon, Jin-Hong;Jeon, Jeong-Woo;Kang, Do-Hyun
    • The Transactions of the Korean Institute of Electrical Engineers D
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    • v.50 no.9
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    • pp.417-422
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    • 2001
  • The brushless DC motor(BLDCM) is widely used in many applications. One of the application of the BLDCM is the stage which is one of process in the semiconductor manufacturing processes. Very high performance is required in the stage process. In this paper, the 1 degree of freedom positioning system for the basic technology of the stage is studied. The linearization method is proposed to make the controller design procedures easy by measuring the thrust force ripple using the strain gauge. And through the experiments, it is proved that the inner velocity control loop is necessary to make more precise positioning control system.

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A Study on Earth-Moon Transfer Orbit Design

  • No, Tae-Soo;Lee, Ji-Marn;Jeon, Gyeong-Eon;Lee, Dae-Ro;Kim, Ghang-Ho
    • International Journal of Aeronautical and Space Sciences
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    • v.13 no.1
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    • pp.106-116
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    • 2012
  • Optimal transfer trajectories based on the planar circular restricted three body problem are designed by using mixed impulsive and continuous thrust. Continuous and dynamic trajectory optimization is reformulated in the form of discrete optimization problem. This is done by the method of direct transcription and collocation. It is then solved by using nonlinear programming software. Two very different transfer trajectories can be obtained by the different combinations of the design parameters. Furthermore, it was found out that all designed trajectories permit a ballistic capture by the Moon's gravity. Finally, the required thrust profiles are presented and they are analyzed in detail.

A Study on the Nonlinear Behavior of Plate under Thrust (면내압축하중을 받는 선체판의 비선형거동에 관한 연구)

  • 고재용
    • Proceedings of the Korean Institute of Navigation and Port Research Conference
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    • 1996.09a
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    • pp.95-110
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    • 1996
  • High Tensile Steel enables to reduce the plate thickness comparing to the case when Mild Steel is used. From the economical view point this is very preferable since the reduction in the hull weight. However to use the High Tensile Steel effectively the plate thickness may become thin so that the occurrence of buckling is inevitable and design allowing plate buckling may be necessary. If the inplane stiffness of the plating decreases due to buckling, buckling may be necessary. If the inplane stiffness of the plating decreases due to buckling the flexural rigidity of the cross section of a ship's hull also decreases. this may lead to excessive deflection of the hull girder under longitudinal bending. In these cases a precise estimation of plate's behavior after buckling is necessary and nonlinear analysis of isolated and stiffened plates is required for structural system analysis. In this connection this paper discusses nonlinear behaviour of thin plate under thrust. Based on the analytical method elastic large deflection analysis of isolated plate is perform and simple expression are derived to evaluate the inplane rigidity of plates subjected to uniaxial compression.

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Design of Pamanent Magnet Linear synchronous Motor System by parameter estimation and DC link voltage. (설계 파라미터와 DC link 전압에 의한 직선형 영구자석 동기 모터 시스템 설계)

  • Jang, Seok-Myeong;You, Dae-Joon;Jang, Won-Bum;Choi, Jang-Young;Seo, Jung-Chul
    • Proceedings of the KIEE Conference
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    • 2005.07b
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    • pp.1080-1082
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    • 2005
  • This paper presents the system design of permanent magnet linear synchronous machine with double-side PM mover and slotless iron-cored stator in the required speed and thrust. in this paper, the design of manufacturing motor is optimized by characteristics of motor parameters with the variation of PM size and coil turns. And, the permissible operating range of manufactured motor by determination of base speed and base thrust according to switching scheme of DC link voltage are offered. Finally, the results of analytical solutions are verificated by finite element analysis and experiment.

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