• KSCE Journal of Civil and Environmental Engineering Research
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• v.33 no.1
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• pp.181-194
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• 2013

Landslides are known as gravitational mass movements that can carry the flow materials ranging in size from clay to boulders. The various types of landslides are differentiated by rate and depositional features. Indeed, flow characteristics are observed from very slow-moving landslides (e.g., mud slide and mud flow) to very fast-moving landslides (e.g., debris avalanches and debris flows). From a geomechanical point of view, shear-rate-dependent shear strength should be examined in landslides. This paper presents the design of advanced ring-shear apparatus to measure the undrained shear strength of debris flow materials in Korea. As updated from conventional ring-shear apparatus, this apparatus can evaluate the shear strength under different conditions of saturation, drainage and consolidation. We also briefly discussed on the ring shear apparatus for enforcing sealing and rotation control. For the materials with sands and gravels, an undrained ring-shear test was carried out simulating the undrained loading process that takes place in the pre-existing slip surface. We have observed typical evolution of shear strength that found in the literature. This paper presents the research background and expected results from the ring-shear apparatus. At high shear speed, a temporary liquefaction and grain-crushing occurred in the sliding zone may take an important role in the long-runout landslide motion. Strength in rheology can be also determined in post-failure dynamics using ring-shear apparatus and be utilized in debris flow mobility.

• Journal of the Earthquake Engineering Society of Korea
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• v.13 no.4
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• pp.25-35
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• 2009

This paper introduces the performance of a newly developed base isolation system made from the combination of a polyurethane disk - attached pot bearing and C-shape steel dampers. Ultimate compressive load tests, ultimate rotation tests, dynamic tests, and dynamic load repeat tests have been completed to determine dynamic characteristics and to verify performance characteristics. The experimental results are compared with the analytic results. It is determined that all requirements for bridge bearing in the specifications are satisfied, and that adequate energy dissipation has occurred. The EDC and effective stiffness estimated by tests are similar to the theoretical values.

• Proceedings of the KIEE Conference
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• 2006.07b
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• pp.1213-1214
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• 2006

본 논문에서는 5 kWh급 초전도 플라이휠 에너지 저장장치(Superconductor Flywheel Energy Storage System : SFES)를 제작하고 시험운전을 통하여 회전 테스트를 수행하였다. 본 연구에서 사용된 초전도 베어링은 저널형 베어링으로써 액체 질소를 순환시켜 초전도체를 냉각시키고 휠을 부양시켜서 전동발전기를 통하여 회전시키게 된다. 액체 질소를 순환하였을 경우 초전도 베어링의 냉각특성을 고찰하였고, 전동 발전기를 이용하여 2000[rpm]까지의 회전 테스트가 수행 되었으며, 전동발전기의 동작 특성 및 회전시 휠의 궤적과 축진동 특성을 테스트 하였다.

• Proceedings of the KIEE Conference
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• 1999.07a
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• pp.433-435
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• 1999

전동차의 구동시스템 및 보조 전원장치 등의 제어가 고성능화되고 복잡해지면서 각 기기의 개별 시험이 아닌 조합시험을 통한 신뢰성의 확보가 점점 중요해지고 있다. 특히 구동시스템의 시험을 위해서는 실제 차량부하와 유사한 부하 특성을 조합시험장치가 제공하는 것이 중요하다. 전동차의 부하특성에서 가장 지배적인 역할을 하는 특성은 관성이다. 국내에 운용중인 조합시험장치들은 전동차의 직선 운동에 해당하는 등가 회전관성을 가지는 플라이휠(flywheel)을 이용하여 관성부하를 구현하고 있다. 본 논문에서는 이러한 관성부하를 기계적 질량이 아닌 서보시스템을 이용하여 구현할 경우의 장단점과 특성에 대해 알아보고, 그 적절한 구현방법을 제안하고자 한다. 또한 실험 및 실험 결과를 통해 그 타당성을 검증하고자 한다.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2003.10a
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• pp.173-178
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• 2003

The study was performed to understand combustion characteristics of the slinger combustor. Liquid fuel is discharged radially outwards through injection holes drilled in the high speed rotating shaft. We observed atomizing characteristics with variation of fuel nozzle rotating speed by using PDPA system. The mean drop diameter highly depends on fuel nozzle rotating speed. In KARI combustion test facility, Ignition and combustion tests were performed by using real scale combustor. In the test results, ignition and combustion efficiency were increased according to increasing fuel nozzle rotating speed. The measured radial temperature distribution at the combustor exit shows stable and fairly good distribution.

• Journal of Advanced Navigation Technology
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• v.22 no.5
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• pp.351-358
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• 2018

In this study, we propose a method of suppressing the leakage noise signal of motor assembly through the test. The motor assembly is mounted on outside of the aircraft to rotate an antenna and must satisfy RE102 requirement on MIL-STD-461F in terms of electromagnetic interference. It is confirmed by RE102 test result hat the leakage noise signal of the equipment occurs due to external influx through the power and control cable and rotation of the motor. And it is ascertained that the part where internal/external physical shielding is difficult to rotate is the leakage path. To reduce the leakage noise signal, the electrical ground reinforcement and the electric shielding structure considering the operation of the equipment is applied and it is verified that the requirement is satisfied. Finally, we verified that required specification are met by applying circular corrugated choke with interlocking shapes and conductive grease to the noise leakage path.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 1998.10a
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• pp.39-39
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• 1998

본 연구는 500KW급 수평축 풍력발전기용으로 개발된 회전날개의 시제품 제작에 앞서 축소모델에 대한, 이론적으로 예측된 공력성능과 신축에 의한 공력성능을 비교 검토함으로서, 설계결과를 검증하고, 필요한 경우 설계를 보완하여 개발위험도를 최소화하기 위해 수행되었다. 시험모델의 크기는 실제의 5%로서 직경이 2.1m이며 날개의 시위길이는 0.2r/R에서 0.101m, 날개끝에서 0.043m 이고, 날개단면형 상온 FX-S-03-182이다. 블레이드의 재질은 Glass/Epoxy 복합재료로 제작되었으며, 실제 풍황을 모사하기 위해 자연풍 상태에서 실험하였다. 실험장치의 구성은 15m 높이의 타워에 회전날개와 전자브레이크 및 각종 센서를 장착하였고, 날개가 회전하기 시작하면 제동장치에 의해 부하를 주면서 토크, 회전수, 풍속 등을 각각의 센서로부터 자료획득장치를 통해 자료처리를 할 수 있도록 하였다. 실험하는 동안 풍속은 4m/s-13m/s 정도로서 시동 풍속인 4m/s와 정격풍속인 12m/s를 포함하여 회전날개의 전체적인 특성을 파악하기 용이하였고, 이론적인 예측성능과 측정된 성능을 비교 검토한 결과 비슷한 결과를 얻어 공력설계 및 해석 방법을 검증하였다.

• Journal of the Korean Society of Propulsion Engineers
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• v.14 no.5
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• pp.51-56
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• 2010

An experimental study was performed to understand spray characteristics of the V type rotating fuel nozzle with orifice diameters by using high speed rotational system. The experimental apparatus consist of a high speed rotational system, fuel injection system and acrylic case. The droplet size and velocity were measured by PDPA(Phase Doppler Particle Analyzer) and spray was visualized by using Nd-Yag laser-based flash photography. From the test results, droplet size is reduced with increasing orifice diameter up to the critical value. When increasing orifice diameter over than this critical value, droplet size is not decreased with increasing the orifice diameter. This is due to the irregular distribution of the liquid sheet around the inner surface of injection orifice.

• Proceedings of the Korean Society of Propulsion Engineers Conference
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• 2010.05a
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• pp.258-263
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• 2010

An experimental study was performed to understand spray characteristics of the V type rotating fuel nozzle with orifice diameters by using high speed rotational system. The experimental apparatus consist of a high speed rotational system, fuel injection system and acrylic case. The droplet size and velocity were measured by PDPA(Phase Doppler Particle Analyzer) and spray was visualized by using Nd-Yag laser-based flash photography. From the test results, droplet diameters are reduced with increasing orifice diameter and the optimum injection orifice diameter is 2.6 mm. When increasing orifice diameter over than 2.6 mm, droplet diameter is not decreased with increasing orifice diameter. This is due to the irregular distribution of the liquid sheet around the inner surface of injection orifice.

• Proceedings of the Korean Vacuum Society Conference
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• 2011.08a
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• pp.91-91
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• 2011

본 개발에서는 초고속 복합 분자펌프 구동을 위한 디지털 구동장치를 설계 하였다. 초고속 모터구동을 위한 핵심제어 보드 설계 및 모듈을 설계하여 기본성능을 평가하였다. 또한 초고속 전동기 운전시 급가속 성능을 향상 하기 위해 홀센서에 의한 위치측정 오차를 최소화하는 관측기를 설계하여 모터제어기를 설계하여 고속회전 시험을 하였다. AMB 구동을 위한 전류제어기를 제작하여 성능시험을 하였다. AMB 구동을 위한 와전류식 변위센서 구동부를 설계 제작하였다.