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Development of Inter-propellant Seal for High Thrust Turbopump

고추력 터보펌프용 추진제 혼합 방지 실 개발

  • Kwak, Hyun-D. (Turbopump Department, Korea Aerospace Research Institute) ;
  • Jeon, Seong-Min (Turbopump Department, Korea Aerospace Research Institute) ;
  • Kim, Jin-Han (Turbopump Department, Korea Aerospace Research Institute)
  • 곽현덕 (한국항공우주연구원 터보펌프팀) ;
  • 전성민 (한국항공우주연구원 터보펌프팀) ;
  • 김진한 (한국항공우주연구원 터보펌프팀)
  • Published : 2008.12.31

Abstract

An inter-propellant seal (IPS) for high thrust turbopump is designed. With given operating conditions and requirements, the inter-propellant seal is designed to satisfy the leakage characteristics which is less than 0.1% of normal flow rate of pumps. A numerical analysis is developed to predict the leakage flow rate. The results show that the maximum leakage of LOX and kerosene are less than 0.1% of normal flow rate of pumps, respectively. Based on the numerical analysis results, the detail of IPS is performed. Finally a prototype of IPS is manufactured to perform sets of performance tests in the near future.

Keywords

References

  1. 곽현덕, 전성민, 김진한, '터보펌프용 Inter-Propellant Seal의 개발 현황', 한국윤활학회 2004년도 추계학술대회, pp. 195-200, 2004
  2. Hyun D. Kwak, Seong Min Jeon, and Jinhan Kim, 'Development of Inter-propellant Seal for the Turbopump', ASIATRIB 2006 International Conferrence, Kanazawa, Japan, pp. 677-678, 2006
  3. 곽현덕, 전성민, 김진한, '터보펌프용 미케니컬 페이스 실의 수락시험', 유체기계저널, 제10권, 제1호, pp. 20-25, 2007 https://doi.org/10.5293/KFMA.2007.10.1.020
  4. 전성민, 곽현덕, 윤석환, 김진한, '고추력 액체 로켓 엔진용 터보펌프의 회전체 동역학 해석', 한국항공우주학회지, 제36권, 제7호, pp. 688-694, 2008 https://doi.org/10.5139/JKSAS.2008.36.7.688
  5. 하태웅, '편심된 펌프 실의 누설 및 회전체동역학적 해석', 유체기계저널, 제4권, 제2호, pp. 15-21, 2001

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  2. 추진제 혼합 방지 실의 성능시험 vol.26, pp.6, 2008, https://doi.org/10.9725/kstle.2010.26.6.322
  3. 터보펌프 볼 베어링의 마찰 토크 평가 vol.27, pp.1, 2008, https://doi.org/10.9725/kstle.2011.27.1.025