• Title/Summary/Keyword: 펌프 토오크효율

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An Experimental Study on the Efficiency of the Water Hydraulic Piston Pump System driven by an Electric Inverter (전기 인버터 구동 수압 피스톤 펌프 시스템의 효율 성능에 관한 실험적 연구)

  • Ham, Y.B.;Park, J.H.;Kim, S.D.
    • Transactions of The Korea Fluid Power Systems Society
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    • v.3 no.4
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    • pp.1-7
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    • 2006
  • A water hydraulic pump is likely to have serious problems of high leakage, friction and low energy efficiency. A water hydraulic pump has commonly a fixed displacement type and its outlet flow is adjusted by controlling rotation speed of the pump, which can be implemented by using an electric inverter. This study aims to investigate energy efficiency of the water hydraulic pump system which is driven by an electric inverter. The study is based on the experimental results. The pump which is used in the study shows relatively good efficiency and low leakage, low friction as well. The reasons for the good performance of pump is also investigated.

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Performance Test and Model-Ship Correlation for a Waterjet Propulsion System (실선 물분사 추진장치 성능시험 및 모형선-실선 상관관계)

  • Jong-Woo Ahn;Chang-Yong Lee;Young-Ha Park;Jong-Ahn Chung;Byung-Hyun Kim
    • Journal of the Society of Naval Architects of Korea
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    • v.35 no.4
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    • pp.11-18
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    • 1998
  • This study describes sea trial tests for a waterjet propulsion system attached in the hybrid super high speed cargo ship named "Narae". A measuring technique of jet velocity, gross thrust and impeller torque for the waterjet system is explained. From the measured data in sea trial test, performance of the waterjet propulsion system is analyzed and compared with model test results of a similar waterjet system which was carried out in 1996. The erective horse power estimated from sea trial tests shows a good agreement with resistance test results of the model ship. The optimum rising height is estimated as 0.75 m, and the overall efficiency of the waterjet system is predicted as 0.315 at 15 knots. Useful data such as the pump performance, the jet efficiency, the losses of inlet duct and nozzle were obtained. Test results show a similar behavior to the model test results.

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