• 한국소음진동공학회논문집
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• 제25권2호
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• pp.75-82
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• 2015

Noises from the large scale marine propeller are calculated numerically on non-cavitation condition. The hydrodynamic analysis is carried out by potential based panel method with time marching free wake approach. The distribution of hydrodynamic loads on the propeller surface and noise signals are obtained using the unsteady Bernoulli's equation and the Farasssat's formula respectively. It turns out that the noise signal at the narrow band shows strong peak at the blade passage frequency, and the peak value at the 1/3 octave band also shows the same trend. Noise signals and directivity patterns for both the thickness and the loading noise are compared with each other. The directivity pattern for the loading noise shows minor lobe at the backward side of the rotating disc plane.

• 대한조선학회지
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• 제21권2호
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• pp.9-17
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• 1984

Laminar and turbulent boundary layers on a rotating sector and a helical blade are calculated by differential method. The estimation of three dimensional viscous flows provide quite useful informations for the design of propellers and turbo-machinery. A general method of calculation is presented in this paper. Calculated laminar boundary layer on a sector shows smooth development of flows from Blasius' solution at the leading edge to von Karman's solution of a rotating disk at the down-stream. Eddy viscosity model is adopted for the calculation of turbulent flows. Turbulent flows on a rotating blade show similar characters as laminar flows. But cross-flow angle of turbulent flows are reduced in comparison with laminar boundary layers. Effects of rotation make flow structures significantly different from two-dimensional flows. In the range of Reynolds number of model scale propellers, large portion of the blade are still in the transition region from laminar to turbulent flows. Therefore viscous flow pattern might be quite different on the blade of model propeller. The present method of calculation is to be useful for the research of scale effects, cavitation, and roughness effects of propeller blades.

• 한국가시화정보학회지
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• 제5권1호
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• pp.22-29
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• 2007

In the present study, naturally generated bubbles were investigated to be sure if they could be adopted as the tracer for PIV techniques. The bubble can be grown from the nuclei melted in the water of tunnel and the size of bubbles is changed through the variation of tunnel pressure. Since the trace ability and appropriate size of tracer are so important for PIV techniques, the characteristics of bubbles as tracer are revealed in terms of trace ability and bubble size with the variation of flow speed and tunnel pressure in this study. In addition, PIV measurements of (low behind a rotating propeller are conducted to confirm the trace ability of bubbles even in a highly vortical flow.

• 대한기계학회논문집B
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• 제32권4호
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• pp.266-274
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• 2008

The need for more fuel-efficient and lower-emission vehicles has driven the technical development of alternative fuels such as Liquefied Petroleum Gas(LPG) which is able to meet the limits of better emission levels without many modifications to current engine design. LPG has a high vapor pressure and lower viscosity and surface tension than diesel and gasoline fuels. These different fuel characteristics make it difficult to apply it for the conventional gasoline or diesel fuel pump directly. In this study, experiments are performed to get performance and efficiency of the fuel pump at different condition as temperature, rotating speeds, composition of fuel. The characteristics of fuel pump is affected by cavitation due to the variation of temperature and composition.

• KSTLE International Journal
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• 제2권2호
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• pp.146-149
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• 2001

Recently, laser printers have been developed to have high-speed laser scanner with hydrodynamic bearings. Among the bearings, herringbone grooved bearing (HGB) produces hydrodynamic pressure by high-speed rotating and so make the surfaces between the shaft and sleeve separated. Accordingly, the bearings with non-contact rotation are suitable to high-speed rotating and have long bearing life and reliability. HGB is a kind of journal bearing and uses oil for a lubricant. HGB has excellent stiffness and load carrying capacity. Also, HGB is leakage-free due to groove pumping action. Consequently, HGB is valuable to be applied to high-performance devices such as hard disk drive, copier, and so on.

• 한국음향학회지
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• 제28권3호
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• pp.198-207
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• 2009

캐비테이션 기포 (cavitation bubble)가 존재하는 유체 내에서 다중 주파수 (multi-frequency)를 송수신할 때 음파의 감쇠(attenuation)와 음속 (sound speed) 변화가 발생되었고, 이 특징을 이용하여 기포의 크기와 분포량을 추정하였다. 음향실험은 $20{\sim}300\;kHz$ 대역의 다중 주파수를 이용하여 실시하였고, 기포가 존재하는 경우와 존재하지 않는 경우의 주파수별 음속 비와 음파의 감쇠 값을 측정하였다. 캐비테이션 기포는 모터 끝에 장착된 둥근 막대형 블레이드 (blade)를 물 속에서 고속회전시켜 발생되었다. 캐비테이션 기포의 크기 및 분포량은 모터의 회전 속도, 블레이드 끝단 (tip)의 겉넓이를 변화시키며 관측하였고, 기포 생성 후 시간별 기포량 감소율을 측정하였다. 실험 결과 발생된 기포의 크기는 반경 $10{\sim}60{\mu}m$였고, $10{\sim}20{\mu}m$와 $20{\sim}30{\mu}m$ 반경의 기포가 전체의 약 45%와 25%를 차지하였다. 세부실험 결과로 모터의 회전 속도가 증가할수록 더 많은 양의 기포가 발생되지만 블레이드 끝단 면적의 증가와 기포 발생량의 변화는 상관성이 없음을 확인하였다. 또한 기포량의 감소율은 지속시간별로 일정하였고, 2분 이내에 전체량의 80%가 소멸됨을 관측하였다. 음향실험의 결과를 검증하기 위해 동일한 조건에서 광학카메라로 촬영한 기포 분포량과 비교하였다.

• 융복합기술연구소 논문집
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• 제4권2호
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• pp.61-65
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• 2014

Pressure distribution around rotating impeller blades in centrifugal pump has been main issue for design of efficient and high performance automotive water pump. In addition, pressure losses of inlet water pipes should be considered to reduce additional pressure drop and design high performance engine cooling system. In this paper, pressure distribution inside water pump and pressure drop between inlet and outlet of water pump are investigated numerically to design plastic water pump for clean diesel engine application. And the inlet geometry of water pump was considered to analysis the effect of inlet water pipe geometry on pressure distribution around impeller blades and outlet pressure. The prediction results are compared with experimental data to validate and determine optimal operation condition without water pump cavitation. Major design parameters such as blade angle, volute geometry, system pressure, and coolant flow rate are considered to confirm applying possibility of plastic blades to the clean diesel engine.

• 한국가스학회지
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• 제11권4호
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• pp.29-34
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• 2007

근래들어 강화되는 배출가스 규제에 대응하기 위한 대책으로 LPG 차량에 적용되고 있는 제3세대 LPG 연료공급방식인 LPLi(Liquid Phase LPG Injection)는 LPG 연료를 펌프를 이용해서 고압의 액상연료를 공급하는 것이 가장 핵심적인 기술이다. 그러나 LPG 연료의 경우 저점도, 저비등점의 물리적 특성을 갖는 가스연료로서 기존의 가솔린 또는 디젤용 펌프를 사용할 경우 성능 및 효율이 달라질 수 있다. 본 연구에서는 가솔린 연료 펌프의 임펠라 방식을 응용 변형시켜서 LPG연료용으로 개발된 펌프를 이용하여 다양한 온도와 운전 조건에서 성능 및 효율을 파악하고, 펌프의 성능에 영향을 줄 수 있는 캐비테이션에 대하여 살펴보고자 한다.

• 해양환경안전학회지
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• 제23권4호
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• pp.400-406
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• 2017

선박용 입형 편흡입 원심 해수펌프의 회전체와 파이프 시스템 내부에 발생한 과도한 손상의 원인을 분석하고자 실제 모델을 역설계 하였다. 이를 위해 전산유체역학(CFD)을 이용하여 해수냉각펌프의 내부유동 분석을 실시하였다. 결과적으로 역설계를 통한 대상펌프의 형상 및 경계조건을 설정하여 설계 운전점인 $125m^3/h$에서의 펌프 효율은 85.3 %, 양정 32.0미터로 계산되었다. 대상 펌프의 최고 효율점은 $150m^3/h$에서 약 86.2 %로 예측되었으나 실제 운전점과는 차이가 있었다. 최저 유량점인 $112.5m^3/h$에서는 저 유량점 특성상 유동이 불안정하여 해석의 수렴이 좋지 않았다. 선박에서 운전 중인 해수펌프 및 파이프 시스템 전반에 걸쳐 진행 중인 공동현상의 원인 규명을 통해 개선방안을 도출하고자 하였으나, 입 출구 전체 파이프 시스템의 계산, 각 지관들에 대한 유량 및 유속 측정 등을 통해 보다 명확한 원인분석을 위한 후속연구가 필요하다.

• International Journal of Naval Architecture and Ocean Engineering
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• 제5권3호
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• pp.414-430
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• 2013

This paper shows the study of preswirl duct as an effective energy saving devices that have been devised and reviewed to support the propeller performance, especially for the ship of VLCC with large block coefficients. From the bare hull wake measurements, typical upper/lower asymmetry of hull wake at the propeller disk was found. The 2 kinds of pre-swirl duct, Unconventional half circular duct and Conventional circular pre-swirl duct have been designed and reviewed to recover the loss of propeller running in that condition. The general function of the pre-swirl duct was set to work against this asymmetry of wake and generate pre-swirled flow into the propeller against the propeller rotating direction. The optimum self propulsion tests with various angle configurations were carried out and the best configuration was decided. Accordingly, cavitation test was carried out with best configuration of unconventional half circular duct. The blade surface and tip vortex cavitation behaved smoother when the duct was mounted. The hull pressure amplitudes reflected this difference, so the hull pressure amplitude with duct was smaller than that of without duct.