• Title/Summary/Keyword: Open water test dynamometer

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Experimental Study of the POW Characteristics using High-capacity Inclined-shaft Dynamometer (고용량 경사류용 동력계를 이용한 프로펠러 단독시험 특성의 실험적 연구)

  • Ahn, Jong-Woo;Kim, Ki-Sup;Park, Young-Ha
    • Journal of the Society of Naval Architects of Korea
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    • v.56 no.2
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    • pp.168-174
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    • 2019
  • In order to investigate Propeller Open Water (POW) characteristics for the high-speed propeller in Large Cavitation Tunnel (LCT), the high-capacity inclined-shaft dynamometer was designed and manufactured. Its measuring capacities of thrust and torque are ${\pm}2200N$ and ${\pm}120N-m$, respectively. The driving motor is directly connected to the propeller shaft. Inclined angle of the propeller shaft can be adjusted up to ${\pm}10^{\circ}$. As the pressure inside LCT can be adjusted in the range of 0.1~3.0bar, we can carry out the POW test at high Reynolds number (above $1.0{\times}10^6$) without propeller cavitation and the cavitation test in uniform flow. After the new dynamometer setup in LCT, the Reynolds number variation test and propeller open-water test were conducted at the inclined angle of $0^{\circ}$ and $6^{\circ}$. The present POW results of the new dynamometer are compared with those of the existing high-capacity dynamometer in LCT and of the dynamometer in the towing-tank. Through systematic model tests and comparison with their results, the performance of the new inclined-shaft dynamometer was verified. It is thought the POW test for the high-speed propeller should be better conducted at high Reynolds number.

Study of the Open-Water Test and Analysis for a Pumpjet Propulsor in LCT (대형 캐비테이션터널에서 펌프젯 추진기 단독성능 시험 및 해석 기법 연구)

  • Ahn, Jong-Woo;Seol, Han-Shin;Jung, Hong-Seok;Park, Young-Ha
    • Journal of the Society of Naval Architects of Korea
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    • v.59 no.3
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    • pp.149-156
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    • 2022
  • In order to study the open-water test and analysis techniques for pumpjet propulsors in the Large Cavitation Tunnel (LCT), at the Korea Research Institute of Ships and Ocean Engineering, a set of test equipment was designed and manufactured. The pumpjet propulsor is composed of rotor, stator and duct resulting in the strong interaction between the components. A ring-shaped sensor was developed to measure the thrust and torque for duct and stator. The test equipment including the pumpjet is installed on an existing POW dynamometer in the reverse direction. The results from the reverse POW test setup were validated against those from the conventional POW test setup in the Towing Tank (TT) as well as in the LCT. The pumpjet open-water test was conducted at the Reynolds number of around 1.0×106, at which the obtained experimental data became stable in the Reynolds number effect test. The open-water test for the rotor (rotor-only) was conducted to study whether the duct and stator should be considered as a part of the hull or the propulsor. On the basis of the test results, it was shown that the duct and stator could be included in the propulsor. The total thrust, combined thrust of rotor, duct, and stator was used for the pumpjet open-water test analysis. As the whole pumpjet is defined as a propulsor, it is thought that the self-propulsion test and analysis could be conducted in the same way as that of the conventional propeller.

Development and Application of an Open Water Test System for Azimuth Thrusters (아지무스 추진기 단독시험 시스템 개발 및 적용)

  • Lee, Young-Jin;Rhyu, Seong-Sun;Seo, Jong-Soo;Lew, Jae-Moon
    • Journal of the Society of Naval Architects of Korea
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    • v.50 no.4
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    • pp.199-205
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    • 2013
  • To research and develop an azimuth thruster, the new type of open water test dynamometers to measure thrust, torque, total thrust and duct force are designed and manufactured by Samsung Ship Model Basin(SSMB). A compact servomotor to be accurately controlled is connected to precise spiral bevel gear through shafting system combined by couplings and main shafts. The dynamometers have shown excellent linearity and repeatability for all components of forces and a torque. Also, the open water tests have been successfully performed to show the performance of the system. In near future, it is expected that the device can be used for the study of scale effects and development of azimuth thrusters.

Performance Test of 5.5MW Azimuth Thruster Model in LCT(Large Cavitation Tunnel) (5.5MW급 아지무스 추진기(azimuth thruster)에 대한 대형 캐비테이션 터널 모형시험)

  • Paik, Bu-Geun;Park, Young-Ha;Kim, Ki-Sup;Kim, Ju-In;Na, Yun-Cheol
    • Journal of the Society of Naval Architects of Korea
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    • v.52 no.1
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    • pp.34-42
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    • 2015
  • The development of an azimuth thruster which has the function of dynamic positioning and propulsion has been greatly required as the demand of vehicles with it increases. To develop or design a reliable azimuth thruster, it is appropriate that the performance and cavitation observation tests should be conducted in the regime of high Reynolds number. In the present study, to satisfy high Reynolds number condition new dynamometer for a large azimuth thruster is manufactured and arranged in the test section of the Large Cavitation Tunnel (LCT). The test method composed of the open water and the cavitation observation tests is established successfully in LCT, considering the thruster design.