• Journal of Electrical Engineering and Technology
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• 제9권3호
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• pp.942-949
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• 2014

We studied about the rotor design change using a Ferrite ring magnet to reduce material cost in the condition of the same stator core design. However, this design direction has many weak points such as the decrease of BEMF, the low maximum output, the irreversible demagnetization characteristics of a permanent magnet and so on. In order to mitigate such disadvantages, an optimization design of the BLDC motor has been developed by changing each design parameter and by improving the electromagnetic structure. In the proposed water pump SPM BLDC motor using Ferrite magnet, the outer and inner diameter of stator is fixed to the value of the conventional IPM BLDC motor using Nd-Fe-B magnet. The design specification requirements should be satisfied with the same output power and efficiency characteristics in the same dimension. As a result of this study, the design comparison results considering driving performances and material cost are represented. Through the actual experiment with the prototype of the designed motor, the simulations results are verified.

• 한국군사과학기술학회지
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• 제16권6호
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• pp.771-778
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• 2013

Transmission is a core component of helicopter to transmit power from engine to rotor and must have a endurance to be able to show satisfactorily its performance required during its life time. When developing a new helicopter, both military and civil airworthiness authorities require a tie-down test to verify its endurance. Procedure for transmission endurance test is described in FAR part 29 or US military specification but its details are more or less ambiguous. In this paper, we have proposed a proper procedure for transmission endurance test by giving KUH transmission endurance test example including determination of applicable torque, load and test profile.

• 전기학회논문지
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• 제60권4호
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• pp.759-765
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• 2011

This paper proposes an effective assistant model for considering the stator slot-opening effect on air gap flux density distribution in conventional interior-type permanent magnet (IPM) motor. Different from the conventional slot-opening effect analysis in surface-type PM (SPM) motor, a composite effect of slot-opening uniquely existing in IPM motor, which additionally causes enhancement of air gap flux density due to magnet flux path distortion in iron core between the buried PM and rotor surface. This phenomenon is represented by a proposed assistant model, which simply deals with this additional effect by modifying magnetic pole-arc using an effective method. The validity of this proposed analytical model is applied to predict the air gap flux density distribution in an IPM motor model and confirmed by finite element method (FEM).

• 대한전기학회:학술대회논문집
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• 대한전기학회 2007년도 제38회 하계학술대회
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• pp.995-996
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• 2007

This study is for a design of a spindle motor for 1.8 inch hard disk drives(HDDs). Equivalent magnetic circuit model is applied for a basic design of the motor, a specific configuration design and magnetic distribution characteristics are confirmed using finite element analysis. Besides, thrust forces generated between rotor and stator core and thrust pad are calculated for pressure analysis of fluid dynamic bearings.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2007년도 제38회 하계학술대회
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• pp.884-885
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• 2007

This paper presents an window based user-friendly designed characteristics analysis program of permanent-split capacitor single-phase induction motor. For the analysis, equivalent magnetic circuit and symmetrical coordinate method are used. The saturation effect and iron loss of stator and rotor core are considered. The analysis program is made to GUI type which can be used easily by many elementary designer. The accuracy of analysis is verified by comparison with experimental results.

• Journal of Magnetics
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• 제18권3호
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• pp.260-267
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• 2013

In this paper a general 2-D model of a large air-gap synchronous machine either with non-magnetic or magnetic core rotor is investigated and electrical characteristics of the machine are analytically calculated. Considering the general model, analytical equations for magnetic field density in different regions of the large air-gap machine are calculated. In addition, self and mutual inductances in the proposed model of the machine have been developed, which are the most important parameters in the electromagnetic design and transient analysis of synchronous machines. Finite element simulation has also been performed to verify the obtained results from the equations. Analytical results show good agreement with FEM results.

• 전기학회논문지
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• 제68권1호
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• pp.36-43
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• 2019

In this paper, the characteristics of the coaxial magnetic gear according to the shape of the same gear ratio are analyzed using the two - dimensional finite element analysis. The rotor shape is SMCMG, CPCMG and RCMG. After this we analyzed the characteristics according to three shapes. Also, the amount of permanent magnet used in each shape was compared. Next, characteristics analysis of the magnetic gear according to the shape at the same torque was performed. And the total weight and efficiency of the magnetic gears were compared and verified.

• 항공우주기술
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• 제7권2호
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• pp.46-52
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• 2008

5MW급 발전용 가스터빈의 주요 구성품 중 압축기에서의 성능시험 및 해석을 위해 측정 파라미터와 그 파라미터를 계측하기 위한 센서류를 선정하고자 한다. 축류압축기의 경우 각 단의 케이싱에서 정압 분포를 평균하여 계측하고, 내부 유동장에서 Kiel 온도관을 이용하여 전압 및 전온도 분포를 계측한다. 원심압축기의 경우 임펠러 출구의 허브면과 팁면에서의 정압 분포는 일반적으로 상당한 차이가 존재하므로 각 면에서 정압을 측정하여 평균하고, 디퓨저 내부와 디스월러 내부에서의 정압 분포를 계측하기 위해 한 피치에서 5개의 유선을 따라 10 곳에서 정압을 측정하고자 한다. 또한 압축기 내 유동특성과 동익-정익간의 상호작용을 고찰하기 위해 5공 피토관을 이용하여 내부 상세유동을 계측한다.

• 한국항공우주학회지
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• 제46권8호
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• pp.679-686
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• 2018

저자의 이전 논문[1]에서 저자는 미국과 유럽의 회전익기 개발의 현황을 비교하였다. 본 논문에서는 미국에 경쟁적이 우위를 차지하기 위한 21세기를 대비하는 유럽의 회전익 기술개발 현황에 대한 좀 더 구체적으로 조사해 보고자 한다. 유럽은 21세기 초 회전익을 포함한 항공 사업을 효율적이며 조직적으로 운영하기 위해 범 유럽단위의 "ACARE"라는 비관료기관을 설립하였고, 이 조직을 중심으로 유럽연합에서 지원하는 전체 유럽의 차세대 항공사업 R&D 프로그램이 효율적이고 경쟁적이기 위한 의제를 설정하였다. 회전익기 분야의 개발에 대한 과정은 다음과 같다. 1) 객실의 소음/진동 절감(FRIENDCOPTER), 2) 회전익의 효율증가와 회전익에서 유도되는 소음 절감을 위한 핵심 기술의 개발(GRC), 그리고 최근에 시작된 고속/장거리 운행을 위한 차세대 회전익 개발(Fast Rotorcraft). 앞에서 언급하였듯이 이 모든 모든 R&D 프로그램들은 기본 연구 의제, 특히 환경 영향에 대한 요구조건을 만족하여야만 한다. 이러한 과정을 통하여 유럽 회전익 사업은 현재와 미래에서의 시장 점유에 성공적인 업적을 이루었을 뿐 아니라 시장의 요구(고속/장거리운행)를 만족하는 차세대 회전익기인 복합형/tiltrotor 형상의 개발에도 충분한 준비를 하게 되었다.

• 한국유체기계학회 논문집
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• 제18권5호
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• pp.42-48
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• 2015

To improve the core technology of the micro gas turbine, the performance test facility was developed. This paper is focusing on the explanation of the characteristics of micro gas turbine and its assist devices. Major part of micro gas turbine were radial type of compressor, annular type of combustor, radial type of turbine, thrust foil bearing, radial foil bearing and generator. The assist devices were consist of exhaust duct, inverter, data acquisition system, load bank and test cell. Before building up the test facility, the component test was previously conducted to confirm the component performance. After the test facility was prepared, the motoring test was conducted to investigate the rotor dynamic characteristics of the micro gas turbine. Also, the part load performance test was performed. With a developed micro gas turbine test facility, the improved core technology about the micro gas turbine can be suggested to the related industries.