• Proceedings of the Korean Society of Tribologists and Lubrication Engineers Conference
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• 1989.06a
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• pp.22-28
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• 1989

유압베인펌프는 토출유량이 많고 소형으로 동력밀도는 높으나 토출압력면에스는 피스톤식 펌프에 뒤지기 때문에 발생압력의 고압화에 대한 연구가 계속되어 왔다. 유압장치의 경제적인 압력으로서 $300kgf/cm^2$가 제시되어 있는 가운데, 유압베인펌프의 고압화의 연구가 진행중에 있는 점, 또한 최근들어 에너지 절약의 일환으로 펌프의 수명연장 문제가 거론되어 지고 있는 점, 물에 타기 어려운 난연성유압 작동유를 사용할 경우 마찰증대 및 마모성능이 저하하는 점 등의 이유에서 유압베인 펌프의 마찰, 윤활문제가 중요시 되어지고 있다. 특히 펌프의 체적효율을 높이는 것과 마찰, 마모를 저하시키는 것과는 서로 상반된 관계에 놓여있기 때문에 문제의 해결에 어려움을 갖고 있다. 이와같은 모순을 해결하기 위해서는 베인과 캠링사이의 슬라이딩부분의 윤활상태를 파악하지 않으면 안된다. 그러나 베인의 선단부에는 10-20ms의 짧은 시간동안에 수백기압의 압력이 변화하기 때문에 지금까지 확실한 작용력의 파악이 어려워 이 분야의 윤활상태 파악에 관한 연구는 거의 이루어지지 않고 있다. 베인과 캠링간의 윤활상태를 윤활공학적 관점에서 보면 변동하중 상태에서의 슬라이딩 탄성유체윤활상태 또는 혼합윤활상태에 있는 것으로 판단되어지는데, 이와같은 여러가지 어려운 조건 때문에 윤활상태를 파악하는데, 어려운점이 뒤따르게 된다. 위와 같은 배경에 착안하여 본 연구에서는 유압베인펌프를 모델화하여 변동하중상태에서 실험이 가능한 장치를 제작, 사용하여 베인 선단 슬라이딩부분의 윤활상태를 파악하였다.

• Proceedings of the Korea Society for Energy Engineering kosee Conference
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• 1995.05a
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• pp.94-99
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• 1995

본 연구는 태양열 열펌프시스템에 의한 약 6평 규모의 실내의 난방방법으로서 간접 난방인 온수순환난방과 직접난방인 복사난방의 성능을 분석하였다. 태양열 열펌프의 최대의 열적성능을 나타낼 수 있도록 알루미늄 롤 본드형 태양열 집열기의 면적을 조절하였으며 집열효과를 극대화하기 위하여 온도감응 자동팽창밸브의 용량을 변화시켰다. 본 실험에서 적용된 태양열 열펌프 난방은 서울지방 봄 가을철의 외기온도에서 실내온도가 18~2$0^{\circ}C$로 유지되도록 설계제작되었다. 태양열 열펌프시스템에 적용된 작용유체는 온수순환 난방에는 R-12냉매. 그 대체냉매는 R-134a 및 혼합냉매, 복사난방에는 R-22냉매이었다.

• The KSFM Journal of Fluid Machinery
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• v.6 no.1 s.18
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• pp.14-22
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• 2003

In this paper the leakage prediction md rotordynamic analysis of an annular seal with a smooth rotor and spiral-grooved stator is performed. For the development of a theoretical model, the three-control-volume analysis of the circumferentially-grooved seal is expanded by considering pressure reduction due to the pumping effect of spiral groove and pressurized flow through the spiral groove. Validation on the present analysis is achieved by comparisons with available experimental data. For the leakage prediction the present analysis generally shows a reasonable agreement with experimental results. Rotordynamic coefficients for rotor speed with spiral angles show same trend, but the magnitudes of rotordynamic coefficients yield differences between analysis and experimental results.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2002.11b
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• pp.799-804
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• 2002

In this paper the leakage prediction and rotordynamic analysis of an annular seal with a smooth rotor and spiral-grooved stator are performed. For developing a theoretical model, the three-control-volume analysis of the circumferentially-grooved seal is expanded by considering pressure reduction due to the pumping effect of spiral groove and pressure flow through the spiral groove. Results by the present analysis are compared with available experimental data. For leakage the analysis results generally show a reasonable agreement to the experimental results. For rotordynamic coefficients the analysis results show the same trend as the experimental results for rotor speed with spiral angles, but their magnitudes show somewhat large deviations.

• Proceedings of the Korean Society for Noise and Vibration Engineering Conference
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• 2002.11a
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• pp.379.1-379
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• 2002

In this paper the leakage prediction and rotordynamic analysis of an annular seal with a smooth rotor and spiral-grooved stator are performed. For developing a theoretical model, the three-control-volume analysis of the circumferentially-grooved seal is expanded by considering pressure reduction due to the pumping effect of spiral groove and pressure flow through the spiral groove. Validation to the present analysis is achieved by comparisons with available experimental data. (omitted)

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.37 no.8
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• pp.744-750
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• 2009

In this study, the pumping performance of a piezoelectric valveless micropump is simulated. The micropump, which was developed in the previous work, is composed of a four-layer lightweight piezocomposite actuator, a polydimethylsiloxane (PDMS) pump chamber, and two diffusers. The piezoelectric domain, the fluid domain and the structural domain are coupled in the three-dimensional simulation. We used ANSYS for the piezoelectric and structural domains and ANSYS CFX for the fluid domain. The effects of driven frequency on the flow rate have been investigated by simulating the flow characteristics for 10 Hz and 40 Hz driven frequencies. The flow rates with respect to driven frequencies up to 300 Hz have been calculated.

• Proceedings of the Korean Radioactive Waste Society Conference
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• 2005.06a
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• pp.21-29
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• 2005

The HANARO, a multi-purpose research reactor of 30 MWth open-tank-in-pool type, has been under normal operation since its initial criticality in February, 1995. Recently, ten years after the initial operation of the HANARO, one of the two primary cooling pumps was decontaminated for overhaul maintenance in 2004. Before decontamination exposure doserate and surface contamination level of primary cooling pump measured at 4 points. After final decontamination exposure doserate and surface contamination level of primary cooling pump remeasured by same method done before. It is easy to decontaminate the out side exposed surfaces of the pump, but it is difficult to approach the inside surface due to double volute installed in the casing. Therefore, a new decontamination facility has been developed to solve this problem. A concentrated de-contaminant (DX-300) is rotated in the closed pump casing by the impeller actuated by a temporary motor. Nuclide particles are removed by the emulsification effect of the de-contaminant and the surface contaminants are chemically removed from the pump by the corrosion and dissolution effect. The inside surfaces of the primary cooling pump have been decontaminated by using the facility. As results, the contamination level of the inside surfaces was maintained below the surface contamination limit.

• Proceedings of the Korean Society of Fisheries Technology Conference
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• 2001.05a
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• pp.612-613
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• 2001

산소가 고갈된 환경속에서는 패각의 폐쇄가 일어나게 되며, 종에 따라 생리적 반응은 차이가 있을지라도, 대체로 저산소에 대한 생리적 보상 기작으로서 수류의 펌프작용과 환기 및 혈중내에서의 산소 수송능력이 증가된다. 저산소상태의 환경속에서는 혐기성 대사가 증가되는 대신, 호기성 대사가 억제되므로서 보유하고 있는 에너지의 사용을 최소화하여 제한된 시간동안 저산소 및 무산소 상태에서도 생존할 수 있다. (중략)

• Aerospace Engineering and Technology
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• v.3 no.2
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• pp.72-80
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• 2004

LOX pump is one of the sub-assemblies constructing turbopump unit. In the current study, static structural analysis on such rotating parts as impeller and inducer has been carried out. Three major factors which can affect the structural stability of the rotating parts of LOX pump, are temperature, pressure, and centrifugal force. The effect of each factor was preliminarily investigated, then the analysis under the consideration of the combined loading conditions has been carried out. The major factor that affects the structural stability was proved to be temperature. The analyses of the combined cases showed that the designed impeller and inducer had reasonable safety margins, which means that the impeller and the inducer will be stable in static structural strength. Although there was no problem in the structural strength of the impeller and the inducer, a model analysis should be followed in order to verify the interference between the rotating part and the inner surface of casing.

• Journal of the Korean Society for Aeronautical & Space Sciences
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• v.34 no.4
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• pp.70-75
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• 2006

The performance of a turbopump system composed of an inducer, an impeller, a volute and seals has been computationally analyzed. To save the computational time, only one flow passage of the inducer and impeller is considered for the computations. A steady mixing-plane method is used on the impeller/volute interface for simulating the unsteady interaction phenomena. The axial thrust is predicted from the turbopump calculation in its entirety, which is necessary for such estimation. Moreover, the effects of each component on the pump performance are investigated at a design condition through the analysis of flow structures. The predicted performance is in good agreement with experimental data in terms of head rise, efficiency and volute wall pressure distributions despite of highly complex flow structures being present. The computational results also show that the axial and radial thrusts are within the design limit although corresponding experimental measurements were not taken.