• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2003년도 추계학술대회논문집
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• pp.459-464
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• 2003

The Roordynamic feasibility of Micro Power System supported by air foil bearings is investigated. The Micro Power System is new portable power source based on brayton cycle, which consists of compressor, turbine, generator, and combustion chamber. In this paper, the analysis of Rotordynamic characteristics of Micro Power System is performed based upon the bearing equilibrium position, Campbell diagram and stability. As a result, it is demonstrated that the air foil bearings could be adopted well to the Micro Power System. However, for more stable operation at target running speed, the damping characteristics of air foil bearing should be enhanced.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2004년도 유체기계 연구개발 발표회 논문집
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• pp.109-115
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• 2004

The micro turbo generator is new portable power source based on the Brayton cycle, which consists of a compressor, a turbine, a generator, and a combustion chamber. In this paper, the thermodynamic analysis was performed to find the required condition for hundreds watts power in the micro turbo generator, and also the rotordynamic stability was predicted using the numerical analysis of air foil bearings which support the micro turbo generator. By experimental works, the rotordynamic stability of the micro turbo generator with foil bearings was verified. While various transient dynamic situation, the micro turbo generator had stable performances. From the result, it was demonstrated that air foil bearings could be adapted to the micro turbo generator as a excellent lubrication element.

• 한국조명전기설비학회지:조명전기설비
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• 제11권3호
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• pp.97-105
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• 1997

위성통신설비를 위한 인공위성 추적 안테나 제어 시스템은 바람에 의한 외란과 베어링 공기역학적 마찰로 인한 전달함수의 파라메타 변동이 존재하므로, 이러한 시스템의 불확실성에도 불구하고 만족스러운 명령추종성을 가지는 강인한 제어 시스템의 설계가 요구된다. 본 연구에서는 $\mu$-설계법을 사용하여 피드백 \ulcorner 포워드 제어기를 각각 독립적으로 설계할 수 있는 강인한 성능을 가지는 2자유도계의 설계법을 제시한다. 또한, 제시된 설계법을 위성추적 안테나 제어 시스템에 제어 시스템에 적용되고 컴퓨터 시뮬레이션을 통하여 1자유도계와 성능을 비교 고찰하여 그 유용성을 확인한다.

• 한국공작기계학회:학술대회논문집
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• 한국공작기계학회 2001년도 춘계학술대회 논문집(한국공작기계학회)
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• pp.263-268
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• 2001

The needs for precision machining of micro to milli parts have been increased as the industry require high quality products, especially for the micro-machining of IT products. The ultra-precision machining system is essential for the micro machining of fine structures, which insures machining accuracy, low systematic and random error and repeatability. In this study, we developed micro machining system, which is equipped with air bearing stage for ultra precision machining and also we present the results of V-grooving experiments, conducted by the developed system, to verify the performance of system. The results show that the machined V-grooving had good accuracy with repeatable stability.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2000년도 춘계학술대회논문집
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• pp.485-491
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• 2000

We obtain the mathematical model of the hard disk drive actuator system from the system response data of the finite element analysis or experimental results. System response data including the dynamics of the considered system are expressed as the mathematical model. It allows the dynamic analysis of the actuator system without resort to the repetitive finite element modeling work. Even though the dynamic characteristics of the system are affected somewhat by the structural modification and the change of the dynamic properties, we can use the modified size and material properties of the actuator system in the mathematical model to some extent. In this study, we express the mathematical model of the simplified rectangular plate first and then proceed to the actual hard disk drive actuator system.

• Tribology and Lubricants
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• 제35권1호
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• pp.44-51
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• 2019

The paper presents the rotordynamic performance measurements and model predictions of a fuel cell electric vehicle (FCEV) air compressor supported on gas foil bearings (GFBs). The rotor has an impeller on one end and a thrust runner on the other end. The front (impeller side) and rear (thrust side) gas foil journal bearings (GFJBs) are located between the impeller and thrust runner to support the radial loads, and a pair of gas foil thrust bearings are located on both sides of the thrust runner to support the axial loads. The test GFJBs have a partial arc shim foil installed between the top foil and bump strip layers to enhance hydrodynamic pressure generation. During the rotordynamic performance tests, two sets of orthogonally installed eddy-current displacement sensors measure the rotor radial motions at the rotor impeller and thrust ends. A series of speed-up and coast-down tests to 100k rpm demonstrates the dominant synchronous (1X) rotor responses to imbalance masses without noticeable subsynchronous motions, which indicates a rotordynamically stable rotor-GFB system. Finite element analysis of the rotor determines the rotor free-free (bending) natural modes and frequencies well beyond the maximum rotating frequency. The predicted damped natural frequencies and damping ratios of the rotor-GFB system reveal rotordynamic stability over the speeds of interest. The imbalance response predictions show that the predicted critical speeds and rotor amplitudes strongly agree with the test measurements, thus validating the developed rotordynamic model.

• 전기전자학회논문지
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• 제1권1호
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• pp.19-30
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• 1997

인공위성 추적 안테나 제어 시스템은 로테이터에 해당하는 DC 서보모터에 의해 안테나의 방위각 및 앙각을 제어함으로써 인공위성의 현재 위치를 추적하고자 하는 시스템이다. 한편 제어 시스템의 설계를 위한 위성추적 시스템의 선형모델은 일반적인 DC 서보모터의 위치 제어 시스템과는 달리 바람에 의한 토오크 외란과 베어링 및 공기역학적 마찰로 인한 전달함수의 파라메타 변동이 존재하므로 이러한 시스템의 불확실성에도 불구하고 만족스러운 명령추종성를 가지는 강인한 제어 시스템의 설계가 요구된다. 본 연구에서는 유전 알고리즘을 사용하여 복잡한 최적화의 과정없이 가중치 함수와 설계 파라메타 ${\gamma}$를 동시에 최적화함으로써 시스템의 파라메타 변동에 대한 강인한 안정성과 기준모델에 따른 최적의 명령추종성을 가지는 위성추적 안테나 $H{\infty}$ 제어 시스템을 설계한다. 이를 위해 강인한 안정성을 가지는 해집단내에서 기준모델의 출력을 최적으로 추종하도록 유전 알고리즘을 사용하여 적절히 주어진 가중치 함수의 게인 및 동특성 파라메타와 설계 파라메타 ${\gamma}$를 동시에 최적화한다. 끝으로 컴퓨터 시뮬레이션을 통하여 설계된 위성추적 안테나 $H{\infty}$ 제어 시스템의 유용성을 확인한다.

• 한국정밀공학회:학술대회논문집
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• 한국정밀공학회 2005년도 춘계학술대회 논문집
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• pp.1883-1886
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• 2005

In this paper, a decoupled dual servo (DDS) stage for ultra-precision scanning system with large working range is introduced. In general, dual servo systems consist of a fine stage for short range and a coarse stage for long range. The proposed DDS also consists of a $XY\theta$ fine stage for handling and carrying workpieces and one axis coarse stage. Its coarse stage consists of air bearing guide system and a coreless linear motor with force ripple. The fine has four voice coil motors(VCM) as its actuator. According to a VCM's nature, there are no mechanical connections between coils and magnetic circuits. Moreover, VCM doesn't have force ripples due to imperfections of commutation components of linear motor systems - currents and flux densities. However, due to the VCM's mechanical constraints the working range of the fine is about $25mm^2$. To break that hurdle, the coarse stage with linear motors is used to move the fine about 500mm. Because of the above reasons, the proposed DDS can achieve higher precision scanning than other stages with only one servo. With MATLAB's Sequential Quadratic Programming (SQP), the VCMs are optimally designed for the highest force under conditions and constraints such as thermal dissipations due to its coil, its size, and so on. And for their movements without any frictions, guide systems of the DDS are composed of air bearings. To get precisely their positions, a linear scale with 5nm resolution are used for the coarse stage's motion and three plane mirror laser interferometers with 5nm for the fine's $XY\theta$ motions. With them, on scanning the two stages have same trajectories. The control algorithm is named Parallel method. The embodied ultra-precision scanning system has sub 100nm following error and in-positioning stability.

• Tribology and Lubricants
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• 제15권3호
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• pp.257-264
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• 1999

Recently as electronics and semi-conductor industry develop, ultra-precision machine tools that use air-spindle with externally pressurized air bearing appear in need of ultra-precision products which demand high precision property. Effects of air compressibility absorbs the vibration of shaft, this is called averaging effect, however, the higher running accuracy is demanded by degrees, the more important factor is machining errors that affect running accuracy of shaft. Actually, it would be very important in the view points of running accuracy to understand effects of machining errors on the running accuracy of the spindle system quantitatively to design and manufacture precision spindle system in the aspect that efficiency in manufacturing spindle system and performance in operation. So fu, there are some researches on the effects that machining error affect running accuracy. However, because these researches deal with one bearing of spindle system, these results aren't enough to explain how much machining errors affect running accuracy in the typical spindle system overall. In this study, we investigate the effects of the perpendicularity error of bearing and shaft on running accuracy of spindle system that consists of journal and thrust bearing theoretically, and suggest design guideline about shape tolerances.

• 한국산학기술학회논문지
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• 제8권6호
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• pp.1319-1324
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• 2007

입출력 헤드 구조의 형상을 정확하게 조절할 수 있는 기술은 하드디스크 드라이브의 성능에 결정적인 요소이다. 본 논문에서 연구한 슬라이더는 알루미나 티타늄 카아바이드로 구성되었으며 디스크를 통과할 때 공기 베어링 역할을 한다. 그러므로 슬라이더의 곡률을 조절하는 것은 매우 중요하다. 본 연구에서 곡률을 조절하기 위해 헤드 슬라이더에 잔류응력을 발생시켜 곡률을 생성하는 레이저 화선 시스템이 사용된다. 슬라이더 형상의 조절을 강화하기 위해 화선(scribe)의 형상에 따른 곡률을 예측할 수 있는 방법이 중요하다. 레이저 화선과 유사한 효과를 얻을 수 있는 응력을 발생하는 하중계를 유한요소 모델에 적용한다. 하중계에 의해 형성된 곡률은 측정값을 통해 보정된다.