대형 캐비테이션터널에서 펌프젯 추진기 자항성능 시험 및 해석 기법 연구
Study of the Self-Propulsion Test and Analysis for a Pumpjet Propulsor in LCT
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초록
In order to study the self-propulsion test and analysis techniques for the submerged body with 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 which results in the strong interaction between the components. To measure the thrust and torque for duct and stator, a ring-shaped sensor was applied. The test equipment including pumpjet is installed on the stern of the submerged body. As the whole pumpjet including duct and stator was considered as the propulsor from pumpjet open-water test, the self-propulsion test was conducted in the same way. The total thrust, combined thrust of rotor, duct and stator was used for the pumpjet self-propulsion test analysis. Accordingly, the self-propulsion test and analysis were conducted in the same way as those of the conventional propeller. The full-scale performances of the pumpjet propulsor were compared with those of the reference propeller. On the basis of the present study, it is thought that the pumpjet propulsor would be designed optimally.
Abstract
In order to study the self-propulsion test and analysis techniques for the submerged body with 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 which results in the strong interaction between the components. To measure the thrust and torque for duct and stator, a ring-shaped sensor was applied. The test equipment including pumpjet is installed on the stern of the submerged body. As the whole pumpjet including duct and stator was considered as the propulsor from pumpjet open-water test, the self-propulsion test was conducted in the same way. The total thrust, combined thrust of rotor, duct and stator was used for the pumpjet self-propulsion test analysis. Accordingly, the self-propulsion test and analysis were conducted in the same way as those of the conventional propeller. The full-scale performances of the pumpjet propulsor were compared with those of the reference propeller. On the basis of the present study, it is thought that the pumpjet propulsor would be designed optimally.
참고문헌 (8)
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- 안종우, "대형 캐비테이션터널에서 몰수체 자항시험 및 해석 기법 연구", 대한조선학회 논문집, 58(2), pp.58~65 (2021), 대한조선학회[DOI]
- 안종우, "대형 캐비테이션터널에서 몰수체 저항시험 및 위벽효과 수정 기법 연구", 대한조선학회 논문집, 57(3), pp.133~139 (2020), 대한조선학회[DOI]
- Aidan, M., "A Comparison of pumpjets and propellers for non-nuclear submarine propulsion", Trendlock Consulting, ~ (2018)
- Resistance for DARPA suboffas represented by model 5470, "Crook, B.", David Talor Research Center Report, ~, pp.Report No DTRC (1990), SHD-1298-07
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- Renilson, R., "Submarine Hydrodynamics" (2015), Springer Briefs in Applied Sciences and Technology
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