• Radiation Oncology Journal
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• 제21권2호
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• pp.174-181
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• 2003

목적: 유방암 환자를 삼문으로 방사선치료할 경우 유방의 접면 영역과 쇄골상 영역의 기하학적 일치를 이루기 위해 갠트리를 회전한 상태에서 테이블을 회전하는 방법이 사용되며, 이때 접면 조사의 posterior edge에 발생할 수 있는 어긋남을 필름선량측정법과 삼차원입체조영치료계획을 통하여 확인하고, 그 어긋남의 해결방법으로 콜리메이터의 각도를 보정해주는 방법들을 연구하였다. 대상 및 방법: 어긋남의 보정을 위해 쇄골상 영역과 유방의 접면 영역을 반쪽 빔 블록과 tangential field block을 사용하여 모의치료한 후 테이블 회전을 하지 않은 상태에서 환자의 몸에 접면 빔의 posterior edge에 선을 긋고, 테이블을 회전시킨 상태에서의 광조사야의 posterior edge와 테이블 회전 이전에 환자의 몸에 그어 놓은 선과 일치되도록 콜리메이터를 회전시키는 방법과, 본 연구에서 고안한 방법인 삼각함수로부터 유도시킨 다음과 같은 공식에 따라 콜리메이터를 회전하여 posterior edge의 어긋남을 보정하고 두 방법을 비교하였다. Co=$2sin^{-1}${$sin\{theta}\{cdot}sin(C/2)$} (Co: collimator angle, $\theta$: angle between tangential beam and table, C: couch angle) 결과: 필름선량측정법을 이용하여 콜리메이터를 보정하지 않은 경우 내외측의 접면 빔의 posterior edge가 어긋남을 확인할 수 있었으며, 콜리메이터를 보정함으로써 posterior edge의 일치함을 확인할 수 있었다. 위 두 방법에서 콜리메이터의 회전 각도는 동일하였다. 또한 전산화된 삼차원입체조영치료계획을 통하여, 접면 빔의 posterior edge의 어긋남을 확인할 수 있었으며, 콜리메이터를 회전하여 보정 함으로써 posterior edge의 일치를 확인할 수 있었다. 각각의 선량체적표를 비교할 경우, 콜리메이터를 보정하여 posterior edge의 일치를 이룬 경우가 더 적은 용적의 폐가 조사되는 것을 확인할 수 있었다. 결론: 유방암 환자의 방사선 치료에서 삼문으로 치료할 경우에 갠트리와 테이블을 동시에 회전하여 쇄골위 영역의 아래 면과 접면 빔의 윗면을 일치시킬 때 각각의 접면 빔의 posterior edge가 어긋남을 인지해야 하며, 약간의 콜리메이터를 회전시킴으로써 이 어긋남은 보정가능하고, 폐에 조사되는 방사선 양도 줄일 수 있었다.

• Transactions on Electrical and Electronic Materials
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• 제15권5호
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• pp.235-240
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• 2014

Nanocomposites made of linear low density polyethylene (LLDPE) and organo-modified montmorillonite (O-MMT) were processed by melt compounding from a commercially available premixed LLDPE/nanoclay masterbatch, at different nanoclay loadings, by co-rotating twin-screw extruder. The morphological and dielectric properties of LLDPE/O-MMT nanocomposites were investigated to understand the structure-dielectric properties relationship in the nanocomposites. The microstructures of the materials were characterized by wide angle X-ray diffraction (WAXD), scanning electron microscopy (SEM), transmission electron microscopy (TEM) and atomic force microscopy (AFM). Initial findings by FTIR spectroscopy characterization indicated the absence of any chemical interaction between LLDPE and nanoclay during the extrusion process, while DSC showed that a 1% wt loading of nanoclay particles increased the degree of crystallinity of the nanocomposites samples. On the other hand, XRD, SEM, TEM and AFM indicated that nanoclay layers were intercalated or exfoliated in the LLDPE matrix. A correlation between the structure and dielectric properties of LLDPE/O-MMT nanocomposites was found and discussed.

• 대한기계학회논문집A
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• 제21권1호
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• pp.53-61
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• 1997

The performance characteristics of magnetic fluid seals are studied numerically as a function of working gap, pole width, angle of pole sharpening, and shaft speed. The temperature distribution of a magnetic fluid seal with multiple tooth is investigated as a function of the contact fraction of magnetic fluids at the periphery of pole tooth using a finite element method. The most significant design parameter of a magnetic fluid seal is the working gap between the pole pieces and the rotating shaft. The result shows that with increasing the working gap, the friction torque decreases radically. The practical working gap for the pole pieces with triangular tooth zone profile is 0.2-0.4mm. The FEM results indicate that the optimal filling of a magnetic fluid between the pole pieces and the shaft is very important due to the accumulations of nonuniform friction heating within the pole pieces, which may interfere the magnetic circuit flow.

• 한국지능시스템학회논문지
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• 제12권6호
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• pp.524-530
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• 2002

본 연구에서는 Sugeno-type 퍼지시스템을 이용하여 계단형 퍼지 이동 슬라이딩 평면을 구성하고 이를 이용한 슬라이딩 모드제어방식을 제안한다 이 퍼지시스템은 위상평면 상에서 상태오차벡터가 이루는 각도와 원점과의 거리를 입력으로 가지며 출력으로 1차 선형방정식을 갖는다. 이 퍼지 슬라이딩 평면을 이용하여 초기 상태를 이 평면상에 위치시키고 이 슬라이딩 평면을 회전시키거나 이동시킴으로써 도달시간을 줄이고 추적시간을 줄인다. 제안된 이동 슬라이딩 평면은 개념적으로 계단형의 이산적인 형태를 가지지만 이 평면이 퍼지시스템으로 구성되기 때문에 연속으로 이동하는 특징을 나타낸다. 제안된 퍼지 슬라이딩 평면에 대한 슬라이딩 모드의 동특성이 안정함을 증명하며 이를 2차 예제시스템을 이용하여 그 타당성을 보인다.

• 한국유체기계학회 논문집
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• 제19권6호
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• pp.5-13
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• 2016

Three-dimensional unsteady numerical analysis has been performed to observe aerodynamic characteristics of a H-rotor. Generally, the structure of the H-rotor is simple but the aerodynamic characteristics are exceptionably complicated since the angle of attacks and incident velocities to a blade are considerably varied according to the azimuth angles and solidities. The blade in the upwind revolution between 0 to 180 degree obtains aerodynamic energy from the free stream but the blade in the downwind revolution between 180 to 360 degree does not. When the rotating speed increases, the blade in the downwind revolution accelerates the air around the blade like a fan and it consumes the energy and shows negative torque in the area. On the other hand, the direction of the free stream is bent because of the interaction between blade the free stream. Therefore, the operation point (highest power coefficient) appears at a lower tip-speed-ratio what it is expected.

• 한국소음진동공학회논문집
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• 제25권12호
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• pp.881-887
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• 2015

The stiffness and natural frequencies for blades, flexbeam, and torque tube of bearingless rotor system are measured to determine the material input properties such as mass distributions and stiffness distribution for the rotor dynamics and load analysis. The flap stiffness, lag stiffness, and torsional stiffness are calculated by measuring section strain or twist angle, gages position, and applied loads through bending and twist tests. The modal tests are undertaken to find out the natural frequencies for flap, lag, torsion modes in non-rotating conditions. The stiffness values and mass properties are tuned and updated to match prediction frequencies to the measured frequencies. The rotorcraft comprehensive code(CAMRAD II) is used to analyze the natural frequencies of the specimens. The analysis results with the updated material properties agree well with the measured frequencies. The updated properties will be used to analyze the rotor stability, dynamic characteristics and loads for the rotor rotation test in a whirl tower.

• 한국소음진동공학회:학술대회논문집
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• 한국소음진동공학회 2006년도 추계학술대회논문집
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• pp.531-536
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• 2006

In four cylinder engine, the second order inertia force occurs due to the reciprocating parts of the cylinder. Because the magnitude of the inertia force is proportional to a square of the angular velocity of crank shaft, engine gets suffered from vibration excited by unbalanced inertia force in high speed. This vibration excited by the unbalanced inertia force can be canceled by applying a balance shaft. Balance shaft has one or more unbalance mass and rotates twice quickly than the crank shaft. In this paper, an unbalanced force caused by the rotating of unbalance mass of balance shafts was calculated. The directional equivalent stiffness and damping coefficients of the journal bearing of balance shafts was calculated. Equations of rotational vibration modes were derived using directional stiffness and damping coefficients. The dynamic stability of balance shafts was analyzed and evaluated for two type models using the equivalent stiffness and damping coefficients. An efficient procedure to he able to evaluate dynamic stability and design optimal balance shaft was proposed.

• 한국통신학회논문지
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• 제23권5호
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• pp.1319-1324
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• 1998

빔을 방위각 방향으로 조종하는데 주파수 주사를, 고도각방향으로 조종하는데 위상변위기를 쓰는 회전 레이다시스템의 위상과 주파수 명령을 지상좌표계의 각으로 얻는다. 안테나로는 X대역 같은 높은 주파수 대역에서 쓸수 있고 만들기 쉬운 홈 도파관 안테나를 생각한다. 비선형 특성을 나타내는 주파수를 고도각의 함수로 나타내며, 유도한 주파수 식을 계산시간을 줄일 수 있도록 근사화하여 실시간 다기능 레이다 시스템에 쓸 수 있도록 한다. 방위각 주사 범위가 ${\pm}10^{\circ}$를 넘지 않으면 근사 주파수 명령을 실제값과 잘 일치한다는 것을 보인다.

• 한국군사과학기술학회지
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• 제18권2호
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• pp.181-188
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• 2015

This paper present, the result of the guidance and control law for a course correction munitions(CCM) with 2sets of canards positioned in the rotating nose section. The nonlinear simulation model of the CCM was developed based on 7DOF equation of motion. The ability of correcting position was verified by open-loop control input with nonlinear model. The guidance and control command was constructed by reference trajectory which can be obtained with no control. Finally, the performance of the guidance and control law was evaluated through Monte-carlo simulation. The CEP(Circular Error Probability) was obtained by considering the errors in muzzle velocity, aerodynamic coefficient, wind, elevation and azimuth angle and density.

• 한국정밀공학회지
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• 제25권9호
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• pp.86-94
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• 2008

A total stroke of an opening or closing motion of a hinge mechanism in a folder-type mobile phone is composed of two portions. In the first portion, human fingers act a force to open or close the folder. In this portion, the rotating folder compresses the coil spring installed in the mechanism. In the last portion, this compressed coil spring generates a torque to rotate the folder. The main merit of this study is that we have designed a hinge mechanism to be operated by a uniform torque in the first portion of the total stroke. The uniform torque means that it is constant along the folder's swing angle. This mechanism will give softer feeling to human fingers. A pair of contours in the mechanism plays an important role. It transforms rotation into translation in the first portion; on the other hand, it transforms translation into rotation in the last portion. In this study, we have developed an algorithm to obtain the pair of contour curves. We divided the total contour curves into finite sub-intervals. Assuming that the curves in every sub-interval are parabolas, we have obtained the coefficients of them by solving systems of nonlinear equations recursively.