• 제목/요약/키워드: Asymmetric pre-swirl stator

검색결과 4건 처리시간 0.016초

제원 및 날개 끝 형상 변화에 따른 비대칭 전류고정날개 성능연구 (Study on Performance of Asymmetric Pre-Swirl Stator according to Variations in Dimensions and Blade Tip Shape)

  • 신용진;김문찬;강진구;이준형
    • 한국해양공학회지
    • /
    • 제30권6호
    • /
    • pp.431-439
    • /
    • 2016
  • This paper reports a numerical method for determining the resistance and self-propulsion performance of an asymmetric pre-swirl stator used as an energy saving device by cancelling a propeller's rotational energy. The present asymmetric pre-swirl stator propulsion system consists of three blades at the port and one blade at the starboard, which can effectively recover the biased rotating flow. This paper provides the design concept for the present asymmetric stator, which produces more efficient results than a conventional propeller.

편재된 비대칭형 전류고정날개 추진시스템에 관한 연구 (A Study on the Design of a Biased Asymmetric Pre-swirl Stator Propulsion System)

  • 김문찬;강용덕;전호환
    • 대한조선학회논문집
    • /
    • 제41권3호
    • /
    • pp.13-21
    • /
    • 2004
  • This paper deals with a theoretical and experimental method for the design of a biased asymmetric pre-swirl stator propulsion system which is an energy saving device by recovering a propeller rotational energy. In the case of slow-speed ships, the upward flow is generated along the afterbody hull form at the propeller plane. The generated upward flow cancels the rotating flow of the propeller at the starboard part while it increases at port part. The present biased asymmetric pre-swirl stator propulsion system consists of three blades at the port and one blade at the starboard which can recover the biased rotating flow effectively. This paper provides the design concept which gives more simple and a high degree of efficiency and the experimental results for the compound propulsion system.

선미의 불균일 유동장에서 받음각을 고려한 비대칭 전류고정날개 설계 (Design of Asymmetric Pre-swirl Stator for KVLCC2 Considering Angle of Attack in Non-uniform Flow Fields of the Stern)

  • 이기승;김문찬;신용진;강진구
    • 대한조선학회논문집
    • /
    • 제56권4호
    • /
    • pp.352-360
    • /
    • 2019
  • International Maritime Organization (IMO) regulates an emission of greenhouse gases by creating an Energy Efficiency Design Index (EEDI) to reduce environmental pollution. In propulsion system field, studies are under way on Energy Saving Device (ESD), which can improve propulsion efficiency with the propeller, to reduce the EEDI. Among the studies, the study of Pre-Swirl Stator (PSS) has been actively conducted from long time ago. Recently the variable pith angle type pre-swirl stator has been studied to improve the propulsion efficiency in non-uniform flow fields of the Stern. However, for traditional design methods, no specific design method has been established on the blade or location of radius. In this study, proper design method is proposed for each blade or location for radius according to hydrodynamic pitch angle.

날개의 형상 변화에 따른 LNG선용 비대칭 전류고정날개 설계 (Design of Asymmetric Pre-swirl Stator for LNG Carrier according to Variation of Stator Shapes)

  • 이철민;신용진;김문찬;최정은;전호환
    • 대한조선학회논문집
    • /
    • 제53권1호
    • /
    • pp.37-44
    • /
    • 2016
  • Recently researchers are conducting a lot of research related to EEDI in order to satisfy IMO resolution MEPC. Especially they are interested in design of energy saving device. This paper is to design the asymmetric pre-swirl stator for 160K LNG carrier in order to reduce energy. Two types of the asymmetric pre-swirl stator are taken into account; constant and variable pitch angle stators. “constant” and “variable” mean state that the pitch of stators change by radius. The dimensions of the stators are initially determined using potential-flow code. The propulsion performances of the stators are predicted using viscous-flow code. The model test is carried out in towing tank in PNU. Prediction of ship performance generally follow ITTC recommended. Ship wake prediction was done by two method, ITTC 1978 and ITTC 1999. Therefore propulsion performances were compared ITTC 1978 with ITTC 1999 methods. Comparison components are delivered power and thrust deduction coefficient of the model. Final pre-swirl stator is selected by comparing experiment and CFD.