Effect of a booster inducer on the suction performance of turbopumps

보조 인듀서가 터보펌프의 흡입성능에 미치는 영향

  • 최창호 (한국항공우주연구원 터보펌프개발그룹) ;
  • 홍순삼 (한국항공우주연구원 터보펌프개발그룹) ;
  • 김진한 (한국항공우주연구원 터보펌프개발그룹)
  • Published : 2004.12.01

Abstract

Effects of a booster inducer on the suction performance of turbopumps are investigated in this paper. To see the effect of the booster inducer, suction performance tests are conducted with and without the booster inducer for three turbopumps. It is shown that the booster inducer can enhance the suction performance of turbopumps when the tip clearance of the main inducers are relatively large. Numerical analysis are also carried out to see the effects of the booster inducer on the performance of the main inducer. The booster inducer is shown to increase the static pressure at the inlet of the main inducer and prevent growing of inlet back flows which are believed to have deleterious effects on the suction performance of the inducer.

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