• Journal of the Korea Academia-Industrial cooperation Society
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• v.17 no.10
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• pp.21-26
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• 2016

This study evaluates the magnitudes and distributions of contact tangential forces with the swaging depth of punch acting at the contact surfaces between a rotor core slot and a Cu bar during a sequential rotor core swaging process. The effects of the core slot shape on the magnitudes and distributions of the total contact forces were investigated to improve the productivity of the rotor core swaging process. Parametric elastic-plastic numerical analyses were performed using simplified two-dimensional cyclic symmetric plane strain models to evaluate the contact force distributions at the contact surfaces. The numerical analysis results show that the total contact tangential forces increased by about 55% with the adjacent Cu bar swaging process. The length of the core slot is a dominant factor in the core slot design as result of the increased total contact tangential forces during the swaging process of the rotor core.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.47 no.9
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• pp.607-616
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• 2019

Free body diagram analysis is done for key parts of pilot stage of LLV (Load Limit Valve) which is used to protect overload for static structural test of aerospace flight vehicle. It is shown through the analysis that diameter ratio($D_2)^{ten}/D_2)^{comp}$) of two poppets in a pilot stage must be equal to piston area ratio($A_{comp}/A_{ten}$) of a hydraulic actuator for making a poppet open consistently at constant force applied by an actuator. The result of the analysis is verified by measuring geometries of the poppets in the four different LLVs which are corresponding to four actuators with different capacity and have been used after being imported in this laboratory. Results of "Adjuster resolution tests" with two different pilot stages show the max. deviation of Fi(actuator force in instant of opening poppet) from average Fi obtained for each turn of adjuster is 0.3KN and max. deviation of the Fi normalized by average Fi of each turn of adjuster is 3.7%. From the results, it is verified that the two pilot stages with same poppet diameter ratio make a poppet consistently open at Fis within ${\pm}3.7%$ deviation from the average Fi. The deviation is shown to be caused from frictional force of O-ring in the poppet. Additionally, design factors for poppet spring and adjuster, which are also key parts of the pilot stage, are distinguished and procedure for deciding the factors are also shown in this study.

• Proceedings of the KIEE Conference
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• 2011.07a
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• pp.798-799
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• 2011

온라인 전기버스용 전동기는 차량의 운전특성을 고려하여 가속성 향상을 위한 높은 기동토크가 요구되며, 넓은 속도영역 운전을 위한 약계자 제어성능이 우수해야 한다. 특히 전동기의 최대 동작속도가 배터리 전압에 의해 결정되므로, 고속 운전영역 확보를 위해 전압제한을 고려한 전기설계가 필요하다. 본 연구에서는 정격속도 대비 최대속도의 비가 1:4로서 넓은 약계자 영역이 요구되는 온라인 전기버스용 전동기에 대해 개념설계를 진행하여 Active Part의 치수를 산출하고, 고정자 권선의 턴수 및 회전자 형상 변화에 따른 전압 및 출력특성을 비교 분석하여, 온라인 전기버스용 전동기에 요구되는 약계자 제어특성을 만족하도록 설계안을 도출하였다. 또한 전동기의 고속 동작시 주 손실인 철손에 의한 온도상승을 고려하여 영구자석의 감자안정성을 분석하였으며, 전자장 FEM 해석을 적용하여 설계결과의 타당성을 검증하였다.

• Journal of the Korean Society for Railway
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• v.19 no.4
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• pp.427-435
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• 2016

This study considers the design of a 130kW-class IPMSM for propulsion of a Tram-Train. This Tram-Train has a wide range of speed variation. For this reason, this study suggested IPMSM, which has wide speed variation as a motor for propulsion of the Tram-Train, a basic model suitable for the required traction force was designed. IPMSM has different electromagnetic and structural characteristics depending on the shapes of its rotor. Therefore, the suggested model was additionally designed, and by dividing a permanent magnet was changed so as th have a shape with an added bridge. Finally, by analyzing the load characteristics with finite element analysis of the basic and suggested models and by comparing electromagnetic and structural characteristics, a model has been derived that satisfies IPMSM for the propulsion of the Tram-Train.

• Transactions of the Korean Society of Mechanical Engineers A
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• v.38 no.4
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• pp.379-384
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• 2014

The most critical rotating parts of a gas turbine engine are turbine blades and disc, given that they must operate under severe conditions such as high turbine inlet temperature, high speeds, and high compression ratios. Owing to theses operating conditions and high rotational speed energy, some failures caused by turbine disks and blades are categorized into catastrophic and critical, respectively. To maximize the margin of structural integrity, we aim to optimize the vulnerable area of disc-blade interface region. Then, to check the robustness of the obtained optimized solution, we evaluated structural reliability under uncertainties such as dimensional tolerance and fatigue life variant. The results highlighted the necessity for and limitations of optimization which is one of deterministic methods, and pointed out the requirement for introducing reliability-based design optimization which is one of stochastic methods. Thermal-structural coupled-filed analysis and contact analysis are performed for them.

• The Journal of the Institute of Internet, Broadcasting and Communication
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• v.21 no.1
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• pp.115-120
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• 2021

In this paper, an operating algorithm for single-phase permanent magnet synchronous motor based on PR current controller is proposed. In general, an asymmetric gap may occur depending on the shape of the rotor of single-phase PMSM, and this causes noise and vibration during high-speed operation. Therefore, in this paper, an operating algorithm for a single-phase PMSM usihng a proportional resonant current conrtoller with excellent control stability was proposed. Proportional resonant current controller has on steady state error is relatevly robust against distortion. Also, steady state error of AC input can be eleminated without complicated calculation process. The validity and availability of the proposed algorithm are verified through the experiment.

• The Bulletin of The Korean Astronomical Society
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• v.40 no.2
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• pp.56.2-56.2
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• 2015

본 연구에서는 미국 맥도날드 천문대 (Mcdonald Observatory)에 있는 82인치 Otto Struve 망원경의 가이드 망원경으로 사용하기 위해 2개의 반사경을 이용해 구경이 100 mm이고 유효초점거리가 800 mm인 비축 반사망원경을 설계하였다. 비축 반사경은 일반적인 축 대칭인 반사경보다 가공이 매우 어렵기 때문에 형상 정밀도의 요구량을 알 수 있다면 비축 반사경을 가공하는 과정에서 시간과 비용을 절약할 수 있다. 광학계가 수차가 잘 보정된 회절한계의 성능이기 때문에 엔서클드 에너지 직경(Encircled Energy Diameter) 분석을 통해 민감도 분석을 하였다. 광학설계 소프트웨어인 CodeV를 사용하여 80 % 에너지가 $20{\mu}m$ 내에 들도록 공차한계로 설정하였으며, 기준 파장은 $587.56{\mu}m$이다. 또한 부경과 초점 면 사이의 거리를 보상자로 설정하여 공차가 광학계의 성능에 미치는 영향을 최소화하였다. 민감도 분석은 반사경의 위치, 회전, 그리고 반사경의 형상 정밀도에 대해 수행하였다. 분석 결과, 반사경의 위치와 각도는 일반적인 제작 및 조립 공차보다 매우 작은 것을 확인하였다. 그리고 형상정밀도는 주경이 부경보다 민감하였으며 자승 제곱 평균제곱근 (root-mean-square) 32 nm로 가장 민감한 결과가 나왔다.

• Journal of the Korean Society for Advanced Composite Structures
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• v.1 no.2
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• pp.36-43
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• 2010

In this study, the buckling loads and mode shapes characteristic of circular and non-circular(elliptical) closed composite shells were analyzed. To analyses the buckling behaviors, we develop and report an improved generalized shell element called 4EAS-FS through a combination of enhanced assumed strain and the substitute shear strain fields. A flat shell element has been developed by combining membrane element with drilling degree-of-freedom and a plate bending element. The combined influences of length, thicknesses, cross-sectional parameters, and fiber-angle on the critical buckling loads and mode shapes of circular and non-circular(elliptical) closed shells are examined.

• Proceedings of the KIEE Conference
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• 2006.07b
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• pp.867-868
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• 2006

리니어 모터는 일반적으로 회전하는 모터와 같이 여러 형상의 극간에서 발생되는 힘의 균형에 의해서 구동되는 것이 일반적이다. 특히 하나의 극간에서 미소 구동하는 리니어 모터는 구동력과 실제 이동하는 위치 사이에서 댐핑이나 무게와 함 사이에서 발생하는 가속력의 차이에 의해서 주어진 힘의 파형과 움직이는 위치의 괴적이 만들어가는 이동자의 위치 사이에는 다소 시간 처짐이 발생하게 된다. 본 논문에서는 구동력과 실제 이동하는 위치 사이의 시간 처짐의 원인으로 알려져 있는 딤핑의 조건을 변화시키고 이에 다른 구동력의 변화를 알아보았다. 댐핑이 전형 없는 조건과 댐핑이 조금씩 증가함으로 인해서 주어진 시스템의 기계적 공진 영역에서 발생하는 여러 가지 구동특성을 정량적으로 평가해 보았다. 60[Hz]가 공진인 이동자와 탄성체로 이루어진 시스템에서 58-62[Hz]에서 구동될 경우 힘의 주파수와 가해진 힘에 다라 이동자의 초기 거동을 알아보았으며 초기 0.3초 구간에서 구동되는 특성을 알아보았다. 전체적으로 이동자의 구동 괴적과 주어진 힘의 파형 사이에서 발생하는 시간 처짐은 댐핑계수에 가장 지배적인 영향을 받았으며 구동 힘의 주파수가 공진주파수보다 작으면 점점 증가하고 크면 점점 감소하는 경향을 가지며 공진주파수의 구동력이 가해진다면 시간 처짐은 거의 변화가 없음을 알 수 있었다.

• Journal of the Korean Institute of Illuminating and Electrical Installation Engineers
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• v.22 no.9
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• pp.47-54
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• 2008

Cost reduction requires lowering number of power devices used in the converter driving SRM. This is quite feasible in SRM drive systems than in other drive systems. This paper deals with analysis and simulation of a novel two phase SRM. A novel two phase SRM has high performance, self-starling capability, high efficiency, and low manufacturing cost. Additionally, the stator back iron does not experience any flux reversal as the flux is in the same direction whether phase A or B is excited leading to a greater reduction in core losses. The magnetic analysis and design considerations of the novel two phase SRM have been obtained by the finite element analysis (FEM).