• 핵의학기술
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• 제14권2호
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• pp.197-202
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• 2010

목적: 각 검사실에서는 임상의 신속한 검사 결과 보고 요청에 부응하고 검사 결과의 신뢰도 및 효율성을 증가시키기 위해 자동화 장비를 많이 사용한다. 국산 자동화 장비는 기존 자동화 장비의 단점을 개선, 보완하여 폭넓은 수행능을 가진 국산 자동화 장비이다. 본 연구에서 국산 자동화 장비와 기존 자동화 장비와의 상관성 및 분석능력을 평가하여 검사실에서의 결과보고시간 단축에 대한 유용성과 신뢰성을 알아보고자 하였다. 대상 및 방법: 2009년 9월 삼성서울병원에서 갑상선 호르몬 검사(TT3, TSH, FT4)가 의뢰된 환자를 대상으로 저농도에서 고농도 검체 100개씩 국산 자동화 장비와 RIA-mat 280을 사용하여 상관성을 알아보았다. 국산 자동화 장비의 부분별 평가로 첫째, Tip부분은 정확도, 회수율, 검체 간 상호 오염도를 측정하였다. 둘째, Incubator부분은 회전수(RPM)와 회전축 원경(mm)에 따른 최적의 검사반응 조건을 알아보았다. 검체처리 속도를 분석하기 위해 특정기간의 검사결과 보고시간을 조사하였다. 결과: 국산 자동화 장비와 RIA-mat 280의 상관계수($R^2$)는 TT3 0.98, TSH 0.99, FT4 0.92로 좋은 상관관계를 보였다. Tip의 평가로 정밀도 CV 0.38 %(1번 Tip), CV 0.39 %(2번 Tip), 정확도 98.3 %(1번 Tip), 98.6 %(2번 Tip). 검체 간 상호 오염도는 0.01 %(1번 Tip), 0 %(2번 Tip)로 검체 간 상호 오염도가 거의 없었다. Incubator 조건에서 회전수(RPM)와 회전수 원경(mm) 500 RPM의 1.0 mm, 1.5 mm와 600 RPM의 1.0 mm, 1.5 mm 중 600 RPM의 1.0 mm가 최상의 조건임을 알 수 있었다. 기존의 자동화 장비에서 6회/일 시행되던 검사가 최대20회/일로 늘어남으로써 검체 접수에서 결과보고까지 소요시간이 평균 4.20시간에서 평균 2.19시간으로 약 2시간 단축되었다. 결론: 국산 자동화 장비(Gamma Pro) 사용으로 결과보고 시간이 평균 2.19시간으로, 약 2시간 단축되는 결과를 얻었다. 본 기기는 일정시간당 대량 검체 처리능력이 뛰어나고 실용성을 갖춘 효율적인 장비라고 여겨진다. 검사결과 보고 시간 단축으로 인해 응급환자의 신속한 진단과 외래환자의 진료대기시간 단축에 유용할 것이다.

• 제어로봇시스템학회:학술대회논문집
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• 제어로봇시스템학회 1993년도 한국자동제어학술회의논문집(국제학술편); Seoul National University, Seoul; 20-22 Oct. 1993
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• pp.197-201
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• 1993

A method for the closedloop control of the torsional tip motion of a piezo-polymer actuator is presented. The application of Lyapunov's direct, method to the problem is explored. A feedback control of the torsional tip motion of tile piezopolymer actuator is derived by considering tile time rate of change of the total energy of the system. If the angular velocity of the tip of the actuator is known, all the modes of tile actuator can be controlled simultaneously. This approach has tile advantage over the conventional methods in the respect that it allows one to directly with tile system's partial differential equations without resorting to approximations.

• 한국전산유체공학회지
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• 제13권4호
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• pp.45-49
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• 2008

The present paper describes the results of performance analysis for UH-60A rotor blade in hover. For the numerical simulations, commercial CFD software, FLUENT was used with Spalart-Allmaras turbulence model. The flow solver was based on node based scheme and second order spatial accuracy options was used for simulations. For the enhancement of wake capturing capability, high resolution grid was used around tip vortex region. Granting that somewhat over-prediction of thrust was observed near blade tip region, performance was well correlated with experimental data within 3% accuracy in the operating region. Finally it was shown that the present flow solver can be used as a preliminary performance analysis tool for hovering helicopter rotor blades.

• 한국전산유체공학회:학술대회논문집
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• 한국전산유체공학회 2007년도 추계 학술대회논문집
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• pp.73-76
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• 2007

The present paper describes the results of performance analysis for UH-60A rotor blade in hover. For the numerical simulations, commercial CFD software, FLUENT was used with Spalart-Allmaras turbulence model. The flow solver was based on node based scheme and second order spatial accuracy options was used for simulations. For the enhancement of wake capturing capability, high resolution grid was used around tip vortex region. Granting that somewhat over prediction of thrust was observed near blade tip region, performance was well correlated with experimental data within 3% accuracy in the operating region. Finally it was shown that the present flow solver can be used for preliminary performance analysis tool for hovering helicopter rotor blades.

• 대한기계학회논문집B
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• 제28권3호
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• pp.330-337
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• 2004

Analysis of flow phenomena in a centrifugal compressor impeller has been carried out with numerical simulation to understand the physics of flow near stall. Near stall point, tip leakage flow spills ahead of the leading edge of adjacent blade and other leakage flow passes over the clearance of the adjacent blade instead of rolling up into vortex within the passage. The tip leakage flow at the mid chord of impeller blade impinges against the pressure surface of the adjacent blade and then rolls up into vortex within the passage, which blocks the flow passage and generates viscous loss. The spillage of leakage flow ahead of the adjacent blade generates the recirculation of flow entering the impeller, which causes the power transferred into the flow by the impeller to decrease and blocks the flow passage. Near diffuser hub wall, flow recirculation occurs. As operating point goes to stall point, the core of recirculation approaches the impeller exit The length rises to peak point and then drops with mass flow reduction, while the height steadily rises.

• 대한전기학회논문지:전기물성ㆍ응용부문C
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• 제54권12호
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• pp.527-531
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• 2005

Because of increasing demand for safety of the power transformer, the seismic qualification process in accordance with the standard of IEEE Std 693-1997 is essentially required by customer. Dynamic analysis method and static analysis method were used to qualify the seismic withstanding of the power transformer at high seismic level. Maximum stress was detected at the connection between the main structure and appendages, and maximum displacement was detected at the point of appendage's end tip. Load path and substructure system can be considered as important elements to prevent over stress and over displacement.

• Ocean Systems Engineering
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• 제5권2호
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• pp.125-138
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• 2015

In this study, hydrodynamic performance of a 400 mm diameter horizontal axis marine current turbine model was tested in a cavitation tunnel with 1.21 m x 0.8 m cross-section for over a range of tip speed ratios. Torque and thrust data, as well as cavitation visualizations, for certain operating conditions were acquired. Experimental results indicated that the turbine can be exposed to significant amount of sheet and cloud cavitation over the blades along with vortex cavitation at the blade tips. Inception and distribution of cavitation along the blades of the model turbine were then modelled numerically for design operating conditions using a vortex lattice method. The method was also applied to a turbine tested previously and obtained results were compared with the data available. The comparison between simulation results and experimental data showed a slight difference in terms of span-wise extent of the cavitation region. The cloud and tip vortex cavity observed in experiments cannot be modelled due to the fact that the VLM lacks the ability to predict such types of cavitation. Notwithstanding, the use of such prediction methods can provide a reasonably accurate approach to estimate, therefore take the hydrodynamic effects of cavitation into account in design and analysis of marine current turbines.

• 유체기계공업학회:학술대회논문집
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• 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
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• pp.243-249
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• 2001

Steady state flow calculations are executed for turbo-pump inducers of modem design to validate the performance of Tascflow code. Hydrodynamic performance is evaluated and structure of the passage flow and leading edge recirculation are also investigated. Calculated results show good coincidence with experimental data of static pressure performance and velocity profiles over the leading edge. Upstream recirculation, tip leakage and vortex flow at the blade tip and near leading edge are main source of pressure loss. Amount of pressure loss from the upstream to the leading edge corresponds to that of pressure loss through the whole blade. The total viscous loss is considerably large due to the strong secondary flow.

• 전기의세계
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• 제25권1호
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• pp.87-94
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• 1976

The characteristic of flashover electric discharge has been brought to light in this paper for the situation in which the space and creeping gaps are laid out in series. The result of this study has disclosed the facts that the over all flashover characteristics have three kind of features such as unilateral increase after increase, and increase after decrease in compliance with varied layout method and relative magnitude of gap length, and accordingly there exist a ratio among the magnitudes of gap length and a proper layort method through which the over all flashover voltage reaches the highest. Also involved with this study is the theoretic analysis of flashover characteristics even in the case of creeping electric discharge from hand tip of the gauge, where the over all value of flashover voltage can be estimated from the peculiar value of flashover voltage and flicker voltage for the space and creeping gap within the extent of 5% error.

• Wind and Structures
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• 제32권3호
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• pp.267-281
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• 2021

Bending-twisting coupling induced in big composite wind turbine blades is one of the passive control mechanisms which is exploited to mitigate loads incurred due to deformation of the blades. In the present study, flutter characteristics of bend-twist coupled blades, designed for load alleviation in wind turbine systems, are investigated by time-domain analysis. For this purpose, a baseline full GFRP blade, a bend-twist coupled full GFRP blade, and a hybrid GFRP and CFRP bend-twist coupled blade is designed for load reduction purpose for a 5 MW wind turbine model that is set up in the wind turbine multi-body dynamic code PHATAS. For the study of flutter characteristics of the blades, an over-speed analysis of the wind turbine system is performed without using any blade control and applying slowly increasing wind velocity. A detailed procedure of obtaining the flutter wind and rotational speeds from the time responses of the rotational speed of the rotor, flapwise and torsional deformation of the blade tip, and angle of attack and lift coefficient of the tip section of the blade is explained. Results show that flutter wind and rotational speeds of bend-twist coupled blades are lower than the flutter wind and rotational speeds of the baseline blade mainly due to the kinematic coupling between the bending and torsional deformation in bend-twist coupled blades.