• 한국자동차공학회논문집
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• 제24권4호
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• pp.471-479
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• 2016

Cross-drilling and slotting on the frictional surface of a brake rotor are methods used for improving the performance of the brake system. These shapes have particular advantages, such as the shaving effect of a slotted shape, which maintains a clean pad-to-rotor contact surface, and the venting effect of a drilled shape, which provides passageways for the gas to escape. In order to understand the effect of the machined pattern on the brake performance aspect, an experimental method is adopted along with the dynamometer test. The cross-drilled rotor, slotted rotor, and mixed pattern rotor with cross-drilling and slotting machining are prepared and tested in terms of friction coefficient, temperature, braking torque, and noise.

• Journal of Electrical Engineering and Technology
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• 제12권2호
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• pp.778-789
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• 2017

This paper presents an improved subdomain method to predict the magnet field distributions and electromagnetic performance of the surface-mounted permanent magnet (SPM) machines with static or dynamic eccentricity. Conventional subdomain models are either based on the scalar magnet potential to predict the rotor eccentricity effect or dependent on the magnetic vector potential without considering the eccentric rotor. In this paper, both the magnetic vector potential and the perturbation theory are introduced in order to accurately calculate the effect of rotor eccentricity on the open-circuit and armature reaction performance. The calculation results are presented and validated by the corresponding finite-element method (FEM) results.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2006년도 제26회 춘계학술대회논문집
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• pp.331-336
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• 2006

초음속 터빈의 로터와 노즐사이의 간극은 터빈의 성능과 운전의 안정성에 직접적인 영향을 미치게 된다. 본 연구에서는 30톤급 개방형 액체로켓엔진용 터보펌프의 구동원으로 개발된 초음속 터빈에 대하여 노즐과 로터의 간극이 변화된 형상을 구현하고 이에 대한 계산을 수행한 후 그 결과를 분석하였다. 계산결과로부터 노즐-로터 간극이 증가함에 따라 이 영역에서의 전압력 손실이 증가하고 이에 따른 터빈 성능이 감소함을 확인하였다.

• 설비공학논문집
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• 제19권10호
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• pp.687-694
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• 2007

Cycle simulation is peformed for two types of the desiccant cooling system incorporating a regenerative evaporative cooler. The cooling capacity and COP are evaluated at various effectiveness values of the regenerative evaporative cooler, the desiccant rotor and the sensible heat exchanger. As either of the effectiveness of the regenerative evaporative cooler or the humidity effectiveness of the desiccant rotor increases, both the cooling capacity and COP increase, but the enthalpy leak ratio gives the opposite effect on the system performance. It is found that COP of cycle A mainly depends on the humidity effectiveness of the desiccant rotor, while for cycle B enthalpy leak ratio of desiccant rotor has the major impact on COP. The effect of the sensible heat exchanger on the cooling capacity is small about 1/10 compared with those of other components.

• International Journal of Fluid Machinery and Systems
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• 제1권1호
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• pp.76-85
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• 2008

In order to extract micro hydropower in the very low specific speed range, a Positive Displacement Turbine (PDT) was proposed and steady performance was determined experimentally. However, the suppression of large pressure pulsation is inevitable for practical application of PDT. The objective of the present study is to reveal the mechanism and the characteristics of pressure pulsation in PDT by use of CFD and to suppress the pressure pulsation. Unsteady CFD analysis has revealed that large pressure pulsation is caused by large variation of rotational speed of the following rotor, while the driving rotor, which is output rotor, keeps constant speed. Here is newly proposed a 4-lobe helical type rotor which can reduce the pressure pulsation drastically and the performance prediction of new PDT is determined.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2010년도 제35회 추계학술대회논문집
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• pp.160-163
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• 2010

부분흡입형 초음속 터빈의 노즐과 1단 로터 사이의 축방향 간극이 터빈의 단 성능과 유동장에 어떤 영향을 미치는지 알아보기 위해 터빈에 대한 3차원 유동해석을 수행하고 그 결과를 분석하였다. 상용 유동해석 프로그램 $FLUENT^{TM}$를 사용하였으며 다섯 가지 경우의 축간극에 대해 계산을 하였다. 노즐-로터 축간극이 팁 누설 유량의 증가와 로터 출구의 유동각에 영향을 주는 것을 확인하였다.

• 한국철도학회:학술대회논문집
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• 한국철도학회 2009년도 춘계학술대회 논문집 특별세미나,특별/일반세션
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• pp.585-592
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• 2009

The performance of screw compressor depends on lots of design parameters of rotor profile, such as length of seal line, wrap angle, blow hole, suction and discharge port size, number of rotor lobe, etc. The optimum rotor profile makes it possible to increase the compression efficiency with low energy consumption, and to minimize the loss of power. In this research, a new rotor profile design and performance analysis are done by computer simulation. It is expected that the volumetric efficiency is improved because the internal leakage is reduced due to the minimization of blow hole and clearance, and the stiffness of rotors is increased due to the reduction of length to diameter ratio. Also, the specific power consumption will be secured for use ranging from low to high operation speed.

• 한국항공우주학회지
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• 제48권8호
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• pp.597-609
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• 2020

동축 로터 시스템은 기존의 헬리콥터뿐만 아니라 드론, PAV, 차세대 고속 회전익기 및 화성탐사용 헬리콥터에 적용되는 등, 활용 분야가 점점 넓어지고 있다. 로터 시스템의 성능 연구는 기존 연구에서 동축 로터를 대상으로도 여러 차례 수행되었으나, 로터 블레이드의 변형에 대한 연구는 주로 단일 로터 시스템만을 대상으로 진행되었다. 하지만 동축 로터 시스템에서는 주변에서 발생하는 유동이 복잡하며, 두 로터의 간격이 로터 시스템 전체의 성능에 주요한 영향을 주므로 블레이드의 변형 연구가 더욱 중요하다. 이에 본 연구에서는 최신식 고속 영상촬영 기법 중 하나인 SPR(Stereo Pattern Recognition) 기법을 사용해 동축 로터 블레이드의 변형 측정에 대한 실험적 연구를 수행하였다. 본 연구에는 한국항공우주연구원에서 개발한 축소 동축 로터 시험장치가 사용되었으며, 로터 블레이드의 변형과 성능의 연관성을 고찰하기 위해 동축 로터 시스템의 성능시험이 선행되었다. 해당 시스템의 로터 블레이드 변형을 SPR 기법으로 측정한 결과는 사전에 진행된 성능시험 결과와 함께 본 논문에 제시되었다.

• 한국안전학회지
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• 제9권4호
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• pp.42-48
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• 1994

A rotor flux error-based approach for correcting the rotor time constant estimation used in the slip frequency calculator of indirect field oriented controller is presented in this paper. The controller was derived from the d-q induction machine model. Slip frequency gain is dependent on the machine parameter errors. And parameter errors result in rotor flux error. Thus, estimated rotor flux is compared to commanded rotor flux. The error between them is used for the estimation of rotor time constant. Simulation results which demonstrate the performance of this approach are presented.

• 대한전기학회:학술대회논문집
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• 대한전기학회 2001년도 학술대회 논문집 전문대학교육위원
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• pp.47-52
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• 2001

This paper presents a high-performance control system for Reluctance Synchronous Motor (RSM) drives with direct torque control (DTC). The system consist of stator flux observer, rotor position/speed estimator, torque estimator, two hysteresis band controllers, an optimal switching look-up table, IGBT voltage source inverter, and F240/C31DSP controller by using fully integrated control software. The stator flux observer is based on the combined voltage and current model with stator flux feedback adaptive control that inputs are current and voltage sensing of motor terminal with estimated rotor angle for wide speed range. The rotor position is estimated by the observed stator flux-linkage space vector. The estimated rotor speed can be determinated by differentiation of the rotor position used only in the current model part of the flux observer for a low speed operating area. To prove the suggested control algorithm, we have a simulation and testing at actual experimental system. The developed digitally high-performance position sensorless control system are shown a good motion control response characteristic results and high performance features using 1.0Kw RSM.