• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2006.05a
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• pp.331-336
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• 2006

This paper studies the effects of the nozzle-rotor axial clearance of a supersonic turbine on turbine performance. The nozzle-rotor axial clearance of the supersonic turbine developed to drive a turbopump for 30 ton class liquid rocket engines was varied and a numerical analysis of the turbines having the different nozzle-rotor axial clearances was conducted. It has been found that turbine performance degrades with an increasing axial clearance due to the increased stagnation pressure loss in the axial clearance region.

• Proceedings of the KIEE Conference
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• 2006.07d
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• pp.1824-1825
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• 2006

항공기, 차량, 유도탄 등과 같은 동적인 플랫폼에서 표적을 추적하기 위해서는 시선을 안정화하는 외부의 추적루프와 내부의 속도 루프를 포함하는 서보 구조가 필요하다. 본 논문에서는 내부의 속도 루프인 안정화 루프에 큰 입력 전압이 인가되었을 때 구동기(Actuator) 포화 현상에 의해서 공간 안정화 루프 성능이 나빠지지 않게 와인드업 방지(Anti-windup) 기능을 가진 디지털 비례적분(Proportional Integral, PI) 제어기를 설계한다. 디지털 와인드업 방지 비례적분 제어기는 일반적으로 SISO 시스템 설계를 위한 방법으로 와인드업 방지 기능을 가진 R, S, T 다항식으로 표현되는 입출력 형태의 제어기를 이용하여 설계하였다. 설계된 제어기는 모델링에 의한 시뮬레이션 결과와 실험결과를 통해 성능을 분석하였다.

• Bulletin of the Korean Space Science Society
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• 2009.10a
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• pp.28.2-28.2
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• 2009

이 논문에서는 미소진동이 인공위성 영상품질에 끼치는 영향에 대해 살펴본다. 지구관측위성은 임무수행 시 영상의 지상전달 등을 위해 다양한 구동장치를 가동하며, 이로 인해 미소진동에 노출된다. 이러한 미소진동은 광학탑재체를 가진하여 초점면(Focal Plane)상의 영상운동을 야기하며, 이로 인해 영상품질이 저하된다. 특히, 고해상도 관측위성일수록 미소진동에 의한 영상품질의 저하가 커지므로, 위성개발 시에 영상품질에 대한 영향평가는 필수적이다. 이를 해석하기 위해서 키슬러플랫폼 위에서 진동원의 가진력을 측정 및 그 동특성을 분석한다. 이 가진원은 임무수행형상의 유한요소모델에 적용하여 광학탑재체 초점면의 영상운동을 계산하며, 최종적으로 영상품질에 미치는 영향을 평가한다.

• Proceedings of the KIEE Conference
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• 2003.07d
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• pp.2729-2731
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• 2003

본 연구는 경쟁력 있는 국내외 제품들의 성능을 분석 비교하여 보다 저렴하고 고성능의 WIM 시스템을 국산화하였다. 기구부 및 구동부에는 ANSYS 등을 이용한 수치 해석적 방법을 적용해 설계 제작하였고, 측정 인디게이터부는 32 Bit 고속 DSP 전용 컨트롤러를 개발하여 계량물의 고속 이동시에도 완벽하게 처리할 수 있도록 하였다. 개발된 WIM checker의 성능은 다음과 같다 ; 선별속도 : 300개/분, 선별정도 : 최대 0.1%, 분해능력 : 16 bit, 변환속도 : 100 Hz.

• Proceedings of the Korean Institute of Surface Engineering Conference
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• 2008.11a
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• pp.73-73
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• 2008

LCD, OLED 등의 평판디스플레이와 RFID tag, smart card 등의 구동 소자 등 넓은 산업 분야에 적용하기 위하여 PVP 유기물과 병합된 ZnO 산화물을 이용하여 차세대 박막트랜지스터의 제작 공정과 전기적 특성을 조사하였다. 또한 제작된 박막트랜지스터의 전기적 특성을 향상시키기 위하여 유, 무기 박막의 특성을 분석하고, $O_2$ plasma 처리를 통하여 유-무기 박막간 계면 접합력 및 계면 효과의 변화특성이 OITFT 특성에 미치는 영향을 조사하였다.

• Restorative Dentistry and Endodontics
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• v.35 no.2
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• pp.88-95
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• 2010

The purpose of this study was to compare the root canal shaping ability of 4 rotary NiTi instruments in simulated root canals. For the preparation of thirty two curved root canals, Mtwo instruments using "single length"technique, and Profile, ProTaper Universal, and K3 using crown-down technique (N = 8) were used. All canal samples were prepared by reaching an apical canal size of #30. Pre- and post-instrumentation digital images were recorded and an assessment of canal shape was determined using a computer image analysis program SigmaScan Pro (Systat Software Inc., San Jose, CA, USA). The changes of the dimension of inner walls of canals, (2) the changes of the dimension of outer walls of canals, and (3) the centering ratio were measured at 7 measuring points, and then data were statistically analyzed using one-way ANOVA and Duncan's test. The results were as below; 1. The root canal shaping ability of Profile was significantly faster than that of other rotary NiTi instruments (p < 0.05). 2. The deformation and fracture of all instruments used for this study were not experienced. 3. In the degree of changes of the dimension of inner walls of canals, Profile demonstrated the lowest changes of the dimension of inner walls of canals except at the measuring points of the 1 and 2 mm (p < 0.05). However, the ProTaper Universal showed the highest changes of the dimension of inner walls of canals at all measuring points (p < 0.05). 4. In the degree of changes of the dimension of outer walls of canals, Mtwo demonstrated the lowest changse of the dimension of outer walls of canals except at the measuring point of the 1 mm (p < 0.05). However, Profile exhibited the highest changes of the dimension of outer walls of canals at the measuring points of 3 and 4 mm and ProTaper Universal and K3 showed the largest changes of the dimension of outer walls of canals at the measuring points of 1, 2, 6, and 7 mm (p < 0.05). 5. In degree of centering ratio, Profile demonstrated the least centering ratio comparing with the centering ratio shown by other NiTi instruments at the measuring points of 1, 4, 5, and 6 mm. Results suggest that in the coronal part of canal preparation, active cutting files such as ProTaper Universal may efficiently flare the canal orifice and form a better taper, and in the apical part of the canal, files which have a better centering ability such as Profile may maintain the original canal curvature and reduce the shaping time.

• Journal of Korean Tunnelling and Underground Space Association
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• v.17 no.4
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• pp.457-471
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• 2015

A domestic cutterhead with the diameter of 3.6 m was designed and manufactured in this study. Then, it was attached to an existing earth-pressure balanced shield TBM to excavate a cable tunnel with the length of 1,275 m. Especially, the procedures for TBM cutterhead design and its corresponding performance prediction were also summarized. From field data analyses of the refurbished shield TBM, its maximum advance rate was recorded as 14.4 m/day. Penetration depths of disc cutters were found to be approximately 4 mm/rev, which is equal to the maximum penetration depth designed for the strongest rock strength condition in the target tunnel. Every TBM operating thrust and cutter normal force during TBM driving was much smaller than their corresponding maximum capacities. When cutter acting forces recorded in the field were analyzed, their prediction errors by the CSM model were very high for weak rock conditions. In addition, rock strength showed very close relationships with cutter normal force and penetration depth.

• The Transactions of the Korean Institute of Power Electronics
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• v.11 no.2
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• pp.135-141
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• 2006

In this paper, LC output filters are designed to reduce output harmonics and harmonic analysis are peformed. Generally, multilevel inverters are used in high power application and operates with low switching frequency, which, in turn, generates large output harmonics. Output filters we used to reduce output harmonics. The design approach to reduce output harmonics of the 31eve1 multilevel inverter is discussed and DSP(TMS320C31) is used for the digital control of the system. The design example is given. The designed system is verified by simulation and experiment.

• Journal of the Computational Structural Engineering Institute of Korea
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• v.17 no.2
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• pp.161-169
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• 2004

This paper deals with system identification of a three-story building model with active mass damper (MID) for the controller design. Observer Kalman filter identification (OKID) technique is applied to find the relationship between the experimental results of the input and output. The inputs to the building model with MID are ground accelerations and motor command signal, which are, respectively, simulated earthquake and equivalent control force. The outputs are each floor acceleration and MID acceleration. The MID controller is designed based on the experimentally identified building system. Finally it is shown that experimental results agree accurately with simulated results.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.45 no.1
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• pp.63-70
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• 2017

In this paper, we design and fabricate a de-orbiter using drag-sail and evaluate deployment characteristics. Without employing an actuator to deploy, the de-orbiter is activated by the SMA wire based the release mechanism and driven by the restoring force of the tape-spring. For efficient storage and deployment of drag-sail, an origami method of original ISO flasher is chosen and low priced mylar film is used as the material of the drag-sail. In addition, through the fault tree analysis method which is one of the one-shot device reliability evaluation methods, we confirm the reliability of the de-orbiter(0.997572) and the Roller failure has the highest criticality. Finally, we find feasibility of the proposed de-orbiter through the deployment demonstration of drag-sail.