• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.17 no.5
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• pp.141-148
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• 2003

In the recently, the necessity of the hybrid type linear stepping motor(HLSM) of linear motion digital actuator has been increased in the various fields of the automatic control system. The HLSM is directly performed without any converting mechanism. Therefore, the HLSM is better advantaged in the efficiency and economical view than a rotary stepping motor. In this paper, we have designed an optimum tooth shape by the 2D finite element method(FEM) to develop the HLSM with longitudinal flux machine(LFM) type, and calculated the thrust force and normal force. And we have manufactured the prototype of it, and have experimented the thrust force characteristics of it.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.32 no.6
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• pp.126-133
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• 2004

MRE-1 Dual Thruster Module(DTM), which will be used in KOMPSAT(Korea Multi-Purpose Satellite), can provide reliable and cost-effective means for attitude and maneuvering control system. Thruster heat shield, one of the main components of DTM, is designed to prevent the critical radiative heat exchange between thruster and satellite during firing. To overcome the manufacturing difficulties, a electroforming process is preferred to classical welding process. In this case, an inner diameter of a new shield will be decreased a little due to the change of manufacturing process. Therefore, the interference problem between thruster nozzle and heat shield is investigated through structural analysis and their results are described in this paper.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.1135-1136
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• 2011

본 논문은 LCD 원판 Glass 이송용 4,000[N]급 영구자석 여자 횡자속 선형전동기를 설계하고 해석을 통해 성능을 검토하였다. 실험계획법을 활용하여 횡자속 선형전동기의 형상을 이루는 설계변수들이 추력과 추력리플에 미치는 평균분석을 통해서 민감도분석을 수행하였다. 본 연구에서 개발된 횡자속 선형전동기 적용 추진모듈은 LCD 제조 분야의 원판 Glass 이송용으로 선형이송 시스템에 적용하고자 한다.

• Proceedings of the KIEE Conference
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• 2002.11d
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• pp.30-32
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• 2002

선형동기전동기는 고추력, 고정밀 운전을 요하는 시스템에 많이 사용되고 있는데, 추력 증가에 따른 추력 리플의 증가는 고정밀 위치제어에 어려움을 주기도 한다. 철심형 선형동기전동기에서는 자석 배열과 철심 치형상의 상호 관계에 의해 발생하는 디텐트력의 영향이 매우 크므로 이를 저감하기 위한 철심 구조의 설계가 필요하다. 본 논문에서는 실제 제작성을 고려하여 치와 철심부의 챔퍼링, 길이 변경, 자석 배열의 스큐 적용 등을 통해 선형동기전동기의 디텐트력을 저감하기위한 설계법을 제시하고 그 효과를 시험기의 제작 및 실험을 통해 증명하였다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.48 no.10
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• pp.791-799
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• 2020

Launched in October 2019, Northrop Grumman's MEV-1 was the world's first unmanned mission demonstrating the practical feasibility of on-orbit servicing. Although the concept of on-orbit servicing was proposed several decades ago, it has been developed to various mission concepts providing services such as orbit change, station keeping, propellant and equipment supply, upgrade, repair, on-orbit assembly and production, and space debris removal. The historical success of MEV-1 is expected to expand the market of on-orbit servicing for government agencies and commercial sectors worldwide. The on-orbit servicing essentially requires the utilization of a highly propellant efficient electric propulsion system due to the nature of the mission. In this study, the space mission analysis for a simple on-orbit mission involving Hall thruster is conducted, which is life extension mission for geostationary orbit satellites. In order to analyze the mission, design space exploration for various Hall thruster design variable combinations is performed. The values of design variables and operational parameters of Hall thruster suitable for the mission are proposed through design space analysis and optimization, and mission performance is derived. In addition, the direction of further improvement for the current on-orbit mission analysis process and space mission analysis involving Hall thruster is reviewed.

• Proceedings of the KSME Conference
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• 2003.04a
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• pp.468-472
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• 2003

MRE-1 dual thruster module(DTM) which will be installed to the present under development KOMPSAT(Korea Multi-Purpose Satellite) can provide reliable and cost-effective means of propulsive control for attitude and maneuvering control system. Thruster heat shield, one of the main components of DTM, is designed to intercept the radiative heat exchange between thruster and satellite during firing. The inside diameter of the current configuration will be decreased a little compared with that of the previous one due to manufacturing method change. Therefore, the possibility of interference between thruster and heat shield due to configuration change is investigated through structural analysis and their results are described in this paper.

• Journal of IKEEE
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• v.24 no.3
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• pp.735-742
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• 2020

The pick & place module is used as a core module in the process equipment for producing and inspecting semiconductor components. The conventional pick & place module has the disadvantage that the precision and durability of the system are reduced and the size and weight of the module are increased by using a conversion device that converts rotary motion into linear motion. In this study, we proposed a pick & place module that implements up-and-down linear motion without a conversion device by improving such disadvantage and employs a linear motor with no limit on average thrust and travel distance. Design parameter values, that can reduce cogging force while maintaining average thrust by selecting parameters for designing a core type linear motor with a large thrust to volume ratio and analyzing the effect of cogging force according to design parameter changes through magnetic analysis, was selected. Average thrust and cogging force were measured for the pick & place module composed of the manufactured linear motor and compared with the design values.

• 전기의세계
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• v.43 no.5
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• pp.44-47
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• 1994

자기부상열차의 효율적인 추력제어 및 안전성 높은 운행을 위해서 고성능의 속도/위치 검출 시스템이 중요한 역할을 한다. 일반열차는 바퀴가 선로에 접촉하여 주행하므로 차축의 회전속도를 측정해서 열차의 선로위를 일정한 간격을 두고 부상하여 주행하므로 비접촉식 측정방법을 사용해야만 한다[1-5]. 특히, 고속으로 주행하는 자기부상열차의 속도를 측정하기 위해서는 응답속도가 빠른 센서시스템을 개발하며, 또한 열차주행에 수반되는 자기장의 영향을 극소화하도록 센서시스템을 설계해야만 한다. 본고에서는 전형적인 자기부상열차인 일본의 HSST 시스템(주행속도 100km/h)과 독일의 Transrapid 시스템(주행속도: 400km/h)에 적용되고 있는 속도/위치 검출 시스템의 작동원리를 상세히 설명한다. HSST 시스템은 유도무선(inductive radio system) 방법을 이용하고 Transrapid 시스템은 와전류근접센서(eddy-current proximity sensor)를 이용한다.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.49 no.12
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• pp.1011-1018
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• 2021

This numerical study conducts the modeling and the hover performance analyses of coaxial co-rotating rotor(or stacked rotor), using a rotorcraft comprehensive analysis code, CAMRAD II. The important design parameters such as the index angle and axial spacing for the coaxial co-rotating rotor are varied in this simulation study. The coaxial co-rotating rotor is trimmed using the torque value of the upper rotor of the previous coaxial counter-rotating rotor or the total thrust value of the previous coaxial counter-rotating rotor in hover. The maximum increases in the rotor thrust is 1.84% for the index angle of -10° when using the torque trim approach. In addition, the maximum decreases in the rotor power is 4.53% for the index angle of 20° with the thrust trim method. Thus, the present study shows that the hover performance of the coaxial co-rotating rotor for e-VTOL aircraft can be changed by the index angle.

• Proceedings of the KIEE Conference
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• 2003.10b
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• pp.171-173
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• 2003

기존의 선형 이송 시스템은 구동원으로 서보모터를 사용하고 있다. 서보 모터의 회전 운동을 직선운동으로 변환하기 위해서는 기계적인 동력전달 장치가 필요하며, 이는 위치 오차의 발생이나 주기적인 시스템의 유지보수의 필요성 등의 문제점을 야기한다. 본 논문에서는 단위 체적당 추력비가 기존의 모터에 비해 우수한 횡축형 선형전동기를 이용하여 LCD 공정에 사용되는 indexer 시스템의 선형 추진부에 적용하는 연구를 수행하였다. 실험결과 횡축형 선형전동기는 가속능력 최대 속도 및 위치결정 정밀도 등에서 indexer 시스템에 적용하기에 적합한 것을 검증하였다.