• 한국진공학회지
• /
• 제13권2호
• /
• pp.47-53
• /
• 2004

국내 진공기술 기반을 구축하는 국가사업의 일환으로 게터펌프 성능평가장치를 개발하고 있다. 본격적으로 장치를 구성하기 전에 평가절차의 개발, 장치 설계요건 및 사양을 확정하기 위해 예비실험장치를 만들었다. 이 장치를 이용하여 밀봉형 기기에 들어가는 비교적 활성화 온도가 낮은 게터 소자들의 특성평가 절차를 만들고 이를 적용하여 수소, 일산화탄소, 질소 등에 대해 배기속도와 배기용량을 측정해 보았다. 주로 고순도 기체 공급장치용으로 국내에서 개발된 게터 소자와 램프용으로 널리 쓰이는 외국제품의 배기성능을 비교해 보았다.

• 유체기계공업학회:학술대회논문집
• /
• 유체기계공업학회 2001년도 유체기계 연구개발 발표회 논문집
• /
• pp.264-270
• /
• 2001

The hydraulic performance analysis of an entire pump system composed of an inducer, impeller, volute and seal for the application on turbopumps is performed using three-dimensional Wavier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this wort the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results due to the limitation of the applying the quasi-steady method. Since the volute was found to be over-designed according to the pressure distribution of the volute wall, redesign of the volute has been performed resulting in an improved performance characteristic.

• 한국유체기계학회 논문집
• /
• 제5권2호
• /
• pp.15-21
• /
• 2002

The hydraulic performance analysis of an entire pump system composed of inducer, impeller, volute and seal for the application of turbopumps is numerically performed using three-dimensional Navier-Stokes equations. A quasi-steady mixing-plane method is used on the impeller/volute interface to simulate the unsteady interaction phenomena. From this work, the effects of each component on the pump performance are investigated at design and off-design conditions through the analysis of flow structures and loss mechanisms. The computational results are in a good agreement with experimental ones in terms of the headrise and efficiency even though very complex flow structures are present. It is found that the asymmetric pressure distribution along the volute wall constitutes the main reason of the difference between experimental and computational results, due to the limitation of the quasi-steady method. Since the volute was found to be over-designed by the pressure distribution of the volute wall, re-design of the volute has been performed, resulting in an improved performance characteristic.

• Nuclear Engineering and Technology
• /
• 제52권10호
• /
• pp.2183-2195
• /
• 2020

A mathematical model for the flowrate and rotation speed of RCP during idling was established. The numerical calculation method and dimensionless method were used to analyze the flow, head, torque and pressure and speed changes under idle conditions. Regularity, using the Q criterion vortex identification judgment method combined with surface flow spectrum morphology analysis to diagnose the vortex dynamic characteristics on RCP blade. On impeller blade, there is two oscillations in the pressure ratio on pressure surface in blade outlet region. The velocity on the suction surface is two times more oscillating than the inlet of blade, and there is an intersection with the velocity ratio curve on pressure surface. On blade of guide vane, the pressure ratio increases along the inlet to outlet direction, and the speed ratio decreases with the increase of idle time. There is a vortex that rotates counterclockwise on the suction surface, and the streamline on the suction surface of blade is subjected to the entrainment and blocking action of the vortex creates a large reverse flow in the main flow region. There are two vortices at the outlet of guide vane suction side and the vortices are in opposite directions.

• 설비공학논문집
• /
• 제24권6호
• /
• pp.487-496
• /
• 2012

Recently, utilization of building foundations as ground-coupled heat exchangers has attracted much attention because they reduce the cost and enhance the heat transfer. The objective of this study is to evaluate the performance of energy-slab ground-coupled heat exchanger installed in a commercial building. In order to demonstrate the energy transfer characteristics of the energy-slab, experiments were conducted from October 2010 to September 2011. The 1-year measurement results showed that the mean EWTs of brine returning from the energy-slab were $9.6^{\circ}C$ in heating season and $24.9^{\circ}C$ in cooling season, which were in a range of design target temperatures. In addition, the geothermal heat pump system with the energy-slab showed on-off operation according to the setting temperatures of secondary fluid in water storage tank. The results also showed that the energy-slab extracted heat of 198.6 kW from the ground and injected heat of 318.9 kW to the ground, respectively.

• 한국물환경학회지
• /
• 제23권4호
• /
• pp.543-550
• /
• 2007

In this study, combined sewer overflows (CSOs) from five independent rainfall events in rural city area were collected and investigated. First flush effect in sewage pumping station located near the WWTP was retarded 30 to 60 minutes from booster pumping station. The ratios between SS, COD and TP concentrations prior to rainfall and peak concentrations during the period of rainfall were highly increased but nitrogen was relatively constant, which indicates that it is not associated with particles washed off from the surface of watershed. Mass balance results show that 30% of CSO was generated from booster pump station and 66.5% of CSO was from the whole runoff area. In the area of newly constructed sewer system, CSO problem was related with pump and sewer capacities, but in other old sewer system equipped area, it was due to the collection efficiency. Finally, Log-Log pollutant rating equations were suggested.

• 항공우주시스템공학회지
• /
• 제14권5호
• /
• pp.91-99
• /
• 2020

액체로켓엔진은 발사 전까지 성능의 입증을 위해 많은 시험을 거친다. 점화 및 시동 조건 설정을 위한 시험이나 정격 조건에서의 성능시험을 통해 설계 성능을 검증한다. 하지만 개발과정에서 여러 작동조건의 시험을 통해 탈설계 조건에서의 성능확인이 필요하며 이는 엔진 개발기간에 영향을 준다. 엔진 내의 제어 밸브의 개도를 변화시키는 엔진 성능 시험과 함께 엔진으로 공급되는 추진제의 조건을 변경시켜 탈설계 성능 시험을 수행한다. 본 논문에서는 나로우주센터에 설치되어 있는 한국형발사체 액체로켓 엔진 시험설비에서 수행된 엔진 시험 운용 결과를 기초로 하고 있으며, 시험 대상체에 공급되는 추진제의 압력과 온도의 변화로 터보펌프의 입구 조건을 변경시키는 탈설계 조건 성능시험을 위한 시험설비 운용에 관한 내용을 기술하였다.

• 항공우주시스템공학회지
• /
• 제11권3호
• /
• pp.8-15
• /
• 2017

본 논문에서는 압전유압펌프가 적용된 브레이크 등가 유압회로를 구성하고, 유압회로의 가감압 특성 실험 및 부하압 제어에 대한 연구를 수행하였다. 유압회로의 가감압 특성을 파악하기 위해 펌프 입력 전압에 따른 부하압 형성 실험을 수행하였고, 솔레노이드 밸브 특성이 감압에 미치는 효과를 파악하는 실험을 수행하였다. 가압 특성 실험을 통해 유압회로의 부하압 상승에 필요한 과도응답시간은 압력상승 구배를 조절하는 전압제어를 적용하여 개선할 수 있음을 확인하였고, 감압시는 솔레노이드 밸브 특성을 활용한 밸브 개폐시간 제어와 전압제어를 통해 과도응답시간 개선이 가능함을 확인하였다. 본 연구에서 개발된 제어기법을 적용하여 부하압 제어실험을 수행한 결과, 가압의 경우 10ms 이내로, 감압의 경우 30ms 이내로 과도응답시간을 개선할 수 있었다. 본 연구에서 제안된 부하압 제어기법은 압전유압펌프가 적용된 유압 브레이크 회로의 부하압을 제어하는데 매우 유용할 것으로 판단된다.

• 한국진공학회:학술대회논문집
• /
• 한국진공학회 2016년도 제50회 동계 정기학술대회 초록집
• /
• pp.391-391
• /
• 2016

The carrier transport is a key factor that determines the device performances of semiconductor devices such as solar cells and transistors [1]. Particularly, devices composed of in amorphous semiconductors, the transport is often restricted by carrier trapping, associated with various defects. So far, the trapping has been studied for as-grown films at room temperature; however it has not been studied during growth under plasma processing. Here, we demonstrate the detection of trapped carriers in hydrogenated amorphous silicon (a-Si:H) films during plasma processing, and discuss the carrier trapping and defect kinetics. Using an optically pump-probe technique, we detected the trapped carriers (electrons) in an a-Si:H films during growth by a hydrogen diluted silane discharge [2]. A device-grade intrinsic a-Si:H film growing on a glass substrate was illuminated with pump and probe light. The pump induced the photocurrent, whereas the pulsed probe induced an increment in the photocurrent. The photocurrent and its increment were separately measured using a lock-in technique. Because the increment in the photocurrent originates from emission of trapped carriers, and therefore the trapped carrier density was determined from this increment under the assumption of carrier generation and recombination dynamics [2]. We found that the trapped carrier density in device grade intrinsic a-Si:H was the order of 1e17 to 1e18 cm-3. It was highly dependent on the growth conditions, particularly on the growth temperature. At 473K, the trapped carrier density was minimized. Interestingly, the detected trapped carriers were homogeneously distributed in the direction of film growth, and they were decreased once the film growth was terminated by turning off the discharge.

• 한국추진공학회:학술대회논문집
• /
• 한국추진공학회 2009년도 춘계학술대회 논문집
• /
• pp.11-17
• /
• 2009

가스발생기 사이클의 추력 30톤급 액체로켓엔진용 터보펌프에 대하여 실매질 고온 시험이 이루어졌다. 산화제펌프와 연료펌프에는 각각 액체산소, 케로신이 공급되고 터빈에는 고온의 가스가 공급되며이 가스는 펌프로부터 배출되는 추진제의 일부를 가스발생기에서 연소시켜 생성된다. 터보펌프는 시험중에 설계점과 탈설계점의 전 영역에서 안정적으로 작동하였고 성능 요구 조건을 만족시켰다. 본 논문에서는 여러 차례의 시험 중에서 단일 운전으로 세 운용점에서 총 120초간 작동된 경우에 대하여 터보펌프에 관심을 두고 시험결과를 소개한다. 펌프와 터빈의 성능 특성 관점에서 터보펌프 조립체의 실매질 고온 시험 성능시험 결과와 터보펌프 구성품의 상사 성능 시험 결과가 양호하게 일치하였다.