• 제목/요약/키워드: slipstream rotational velocity

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편재된 비대칭형 전류고정날개 추진시스템 설계에 관한 연구 (A Study on the Design of a Biased Asymmetric Preswirl Stator Propulsion System)

  • 강용덕;김문찬;전호환
    • 한국해양공학회:학술대회논문집
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    • 한국해양공학회 2003년도 춘계학술대회 논문집
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    • pp.32-36
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    • 2003
  • This paper deals with a theoretical method for the design of a biased asymmetric preswirl stator propulsion system which has been used to increase efficiency by the recovery of a propeller slipstream rotational energy by the counter rotating flow of a stator. In the case of full slow-speed ship, the upward flow is generated at the propeller plane by the after body hull form. The generated upward flow cancells the rotating flow of the propeller at the starboard part while it increases at port part. A biased asymmetric preswirl 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. The model tests for the designed compound propulsion system will be carried out later.

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

  • 김문찬;강용덕;전호환
    • 대한조선학회논문집
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    • 제41권3호
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    • pp.13-21
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    • 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.