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인듀서 익단간극이 터보펌프용 펌프의 흡입성능에 미치는 영향

Effects of Inducer Tip Clearance on the Suction Performance of a Pump for Turbopumps

  • 최창호 (한국항공우주연구원 터보펌프팀) ;
  • 김대진 (한국항공우주연구원 터보펌프팀) ;
  • 김진한 (한국항공우주연구원 터보펌프팀)
  • 투고 : 2011.06.21
  • 심사 : 2012.01.11
  • 발행 : 2012.02.01

초록

The effects of inducer tip clearance on the suction performance of a pump for turbopumps are investigated. Experiments for the pump with inducer tip clearances of 1.8% and 1.4% of blade height were performed. The experimental results showed that the suction performance of the pump increased as the tip clearance decreased. It seems that the suction performance of the pump becomes better with smaller tip clearances because the strength of the inducer backflow becomes weak with the decreased tip clearance.

키워드

참고문헌

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피인용 문헌

  1. Effects of inducer tip clearance on the performance and flow characteristics of a pump in a turbopump vol.231, pp.5, 2017, https://doi.org/10.1177/0957650917707656