• 대한전기학회논문지:전기물성ㆍ응용부문C
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• 제53권3호
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• pp.123-127
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• 2004

Mode conversion type ultrasonic rotary motor using bolt tightened Langevin type vibrator was studied. Driving frequency of the motor, displacements and elliptical trajectories at tip of the coupler were simulated by finite element analysis program (ANSYS). Speed and torque of the fabricated motor were measured as functions of input voltage and load. As results, from FEA the driving frequency of 40.8[kHz] and useful elliptical trajectories were found. Fabricated motor rotated clockwise at frequency of 38.2[kHz]. Speed and torque of the motor were increased when the input voltage was increased. Maximum speed, torque and efficiency were 75[rpm], 0.14[Nm] and 6.28[％], respectively.

• Smart Structures and Systems
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• 제24권2호
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• pp.183-191
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• 2019

A piezoelectric paper feeder actuator using Micro Virtual Roller (MVR) is proposed, designed, fabricated and tested. This actuator can drive a sheet of paper forward or backward without any mechanical parts, such as the costly and heavy rollers used in traditional paper feeders. In this paper feeder actuator, two vibrating stators which produce traveling waves are used to drive the paper. The vibrations of the stators are similar to those of piezoelectric motors and follow a similar procedure to move the paper. A feasibility study simulated the actuator in COMSOL Multiphysics Software. Traveling wave and elliptical trajectories were obtained and the dimensions of the stator were optimized using FEM so that the paper could move at top speed. Next, the eigenfrequencies of the actuator was determined. Experimental testing was done in order to validate the FEM results that revealed the relationships between speed and parameters such as frequency and voltage. Advantages of this new mechanism are the sharp decrease in power consumption and low maintenance.

• 한국추진공학회:학술대회논문집
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• 한국추진공학회 2017년도 제48회 춘계학술대회논문집
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• pp.320-324
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• 2017

아음속 공기유동으로 수직분사하는 액체제트에 대하여 오리피스 형상이 달라질 경우, 분무특성에 어떠한 영향을 미치는지 실험적으로 연구하였다. 서로 다른 오리피스 길이 대 직경비와 타원형 노즐의 종횡비를 갖는 분사기들을 제작하여 수직분사 실험을 진행하였다. 원형노즐과 타원형 노즐에서의 분열길이를 비교하였으며, 타원형 노즐에서의 분열길이는 모든 실험조건에서 원형노즐에 비해 줄어들었다. 캐비테이션과 수력튀김 현상이 분사기 내부에 발달되는 분무차압 조건의 경우, 두 노즐 모두 분열길이가 감소하였다. 액주궤적의 경우, 장축으로부터 분무되는 액체제트가 횡방향 공기유동에 수직으로 부딪혀 나가는 경우가 액주의 궤적이 단축에 비해 더 휘어지며, 침투높이가 낮아진다.

• 한국전기전자재료학회논문지
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• 제21권4호
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• pp.335-340
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• 2008

In this study, novel structured thin ultrasonic rotary motor has been proposed. Ultrasonic motors are based on an elliptical motion on the surface of elastic body. Thin brass plate was used as a cross shaped vibrator and eight ceramic plates were attached on upper side and bottom side of the brass plate. From the thin stator, elliptical displacements of the four contact tips were obtained. To find the optimal size of the stator, motions of the motors were simulated using ATILA by changing length, width and thickness of the ceramics. The stators had commonly three resonance peaks and contact tips of the stator moved on tangential or normal trajectories at these resonance peaks. The maximum displacements at the resonance peaks were compared. As results, maximum displacements of the contact tips were obtained at the length of 16 mm, width of 6 mm and thickness of 0.4 mm. Changes of the resonance frequencies were inversely proportional to the length of ceramic and proportional to the width of ceramic. The motor was fabricated by using the designed stator. And, the characteristics of the motor were compared with the simulated results. When the motor was fabricated with these results, speed fo 935 rpm was obtained by input voltage of 25 Vrms at 93.5 kHz.

• 센서학회지
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• 제18권3호
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• pp.185-189
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• 2009

In this paper, we present design and analysis of the omni-directional linear piezoelectric actuator which was consisted of one actuator using the half-wave vibrator. Through calculating vibration speeds on each sector of the actuator, the displacement of contact point of the actuator is theoretically confirmed to be about 33 nm. To confirm an applicable possibility of omni-directional linear piezoelectric actuator, elliptical motion for linear movement, displacement of the tip, changing directions and admittance characteristics are simulated by ATILA. Compared with theoretical result, we obtained similar data with displacement of 32.5 nm at contact point. And then the actuator is simulated elliptical trajectories for linear motions and changing directions according to combination of input signal.

• Tribology and Lubricants
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• 제32권3호
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• pp.101-105
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• 2016

Trap effect of groove is evaluated in a lubricating system using computational fluid dynamics (CFD) analysis. The simulation is based on the standard k-ε turbulence model and the discrete phase model (DPM) using a commercial CFD code FLUENT. The simulation results are also capable of showing the particle trajectories in flow field. Computational domain is meshed using the GAMBIT pre-processor. The various grooves are applied in order to improve lubrication characteristics such as reduction of friction loss, increase in load carrying capacity, and trapping of the wear particles. Trap effect of groove is investigated with variations in cross-sectional shape and Reynolds number in this research. Various cross-sectional shapes of groove (rectangular, triangle, U shaped, trapezoid, elliptical shapes) are considered to evaluate the trap effect in simplified two-dimensional sliding bearing. The particles are assumed to steel, and defined a single particle injection condition in various positions. The “reflect” boundary condition for discrete phase is applied to the wall boundary, and the “escape” boundary condition to “pressure inlet” and “pressure outlet” conditions. The streamlines are compared with particles trajectories in the groove. From the results of numerical analysis in the study, it is found that the cross-sectional shapes favorable to the creation of vortex and small eddy current are effective in terms of particle trapping effect. Moreover, it is found that the Reynolds number has a strong influence on the pattern of vortex or small eddy current in the groove, and that the pattern of the vortex or small eddy current affects the trap effect of the groove.

• 전기전자학회논문지
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• 제27권4호
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• pp.411-417
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• 2023

무인 항공기(UAV) 지원 중계는 분포가 쉽고 통신 채널이 양호하며, 이동성이 뛰어나 기존 지상 중계에 비해 높은 무선 연결성을 가질 수 있다. 본 논문에서는 무선 주파수(RF) 대역을 활용하여 소스로부터 에너지를 수확하고 테라헤르츠(THz) 대역을 활용하여 2차 송신기와 해당 수신기 간에 정보를 전송할 수 있는 UAV 지원 중계 네트워크를 설계한다. 그 후, 릴레이 채널 용량을 최대화하는 UAV의 최적 위치를 결정하기 위한 최적화 문제의 해를 유도하고, 유도된 해를 활용하여 두 가지 UAV 궤적(직선 궤적과 타원 궤적)을 설계하는 알고리즘을 제안한다. 시뮬레이션 결과, 제안된 알고리즘은 UAV 직선 궤도가 수확된 에너지 및 채널 용량 측면에서 더 나은 시스템 성능을 제공할 수 있음을 보여준다.

• Wind and Structures
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• 제26권2호
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• pp.57-68
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• 2018

Wind tunnel tests are conducted to investigate wake-induced vibrations of two circular cylinders with a center-to-center spacing of 4 diameters and attack angle varying from $0^{\circ}$ to $20^{\circ}$ for Reynolds numbers between 18,000 and 168,800. Effects of structural damping, Reynolds number, attack angle and reduced velocity on dynamic responses are examined. Results show that wake-induced vortex vibrations of the downstream cylinder occur in a wider range of the reduced velocity and have higher amplitudes in comparison to the vortex-induced vibration of a single circular cylinder. Two types of wake-induced instability phenomena with distinct dynamic characteristics are observed, which may be due to different generation mechanisms. For small attack angles like $5^{\circ}$ and $10^{\circ}$, the instability of the downstream cylinder characterizes a one-degree-of-freedom (1-DOF) oscillation moving in the across-wind direction. For a large attack angle like $20^{\circ}$, the instability characterizes a two-degree-of-freedom (2-DOF) oscillation with elliptical trajectories. For an attack angle of $15^{\circ}$, the instability can transform from the 1-DOF pattern to the 2-DOF one with the increase of the Reynolds number. Furthermore, the two instabilities show different sensitivity to the structural damping. The 1-DOF instability can be either completely suppressed or reduced to an unsteady oscillation, while the 2-DOF one is relatively less sensitive to the damping level. Reynolds number has important effects on the wake-induced instabilities.

• Journal of Astronomy and Space Sciences
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• 제26권2호
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• pp.171-186
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• 2009

이 연구에서는 미래 한국의 달 탐사에 대비, 지구-달 천이궤적을 설계하고 분석하였다. 궤적 설계는 최소연료로 지구 주차궤도에서부터 달 임무궤도까지 도달하는 모든 단계에 대해서 실시하였으며 미래 한국의 달 탐사 개발 계획에 실질적인 도움이 되기 위해 2017년, 2020년, 2022년으로 각각 나누어 설계를 하였다. 탐사선의 운동방정식의 구현을 위하여 태양, 지구, 달의 중력에 의한 섭동력이 포함된 N체 운동 방정식을 사용하였으며 보다 실질적인 우주환경의 모사를 위하여 지구의 비대칭 중력장(Geopotential), 태양 복사압(Solar radiation pressure) 그리고 달의 J2 섭동에 의한 영향도 고려하였다. 임무 설계를 위해 가정된 추력은 순간 추력(Impulsive thrust)으로 가정하였으며 발사체의 성능은 현재 개발 예정인 KSLV-2로 가정하였다. 미래 한국의 가상 달 탐사선이 지구-달 천이 궤적(Trans Lunar trajectory)에 진입하는 방법으로는 지구 주차 궤도에서 직접 진입 하는 방법과 여러번의 타원 중개 궤도를 거친 후 지구-달 천이 궤적으로 진입하는 방법을 모두 이용하였다. 아울러 TLI(Trans Lunar Injection) 기동시 탐사선의 대전 지상국에서의 가시성에 따른 기동의 크기에 대한 영향이 분석되었다. 이 연구를 통한 임무 설계 결과는 달 탐사 임무 설계를 위한 발사 가능 시기(launch opportunity), 성공적인 임무 수행을 위한 임무 단계별 최적의 기동량 및 해당 궤도의 특성 그리고 다양한 임무 파라미터등의 해석을 포함하고 있다. 임무 설계 결과, 미래 한국이 쏘아 올릴 수 있는 달 탐사선의 전체 질량은 해당 임무의 수행시기 보다는 초기 지구 출발 궤도의 초기 고도와 발사제의 초기 궤도 투입 성능에 따라 더욱 크게 좌우됨을 확인하였다.