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Acceptance Test of a Mechanical Face Seal for Turbopumps

터보펌프용 미케니컬 페이스 실의 수락시험

  • 곽현덕 (한국항공우주연구원 터보펌프팀) ;
  • 전성민 (한국항공우주연구원 터보펌프팀) ;
  • 김진한 (한국항공우주연구원 터보펌프팀)
  • Published : 2007.02.01

Abstract

A mechanical face seal has been tested in Korea Aerospace Research Institute for turbopump applications. In this paper the acceptance test results of the mechanical face seal are described. By means of simulating a practical operating environment, the performance against leakage of mechanical face seal is monitored. In addition the carbon wear is measured to estimate the life of a mechanical face seal. The test results show the acceptable leakage performance and resonable wear tendency as well. Lastly the repeated test had been carried out to guarantee the endurance performance of mechanical face seal based on the turbopump life.

Keywords

References

  1. Kim, J., Lee, E. S., Choi, C. H. and Jeon, S. M., 2004, 'Current Status of Turbopump Development in Korea Aerospace Research Institute,' IAC-04-S.P.17, International Astronautical Congress, Vancouver, Canada
  2. 곽현덕, 전성민, 김진한, 2004, '터보펌프용 Inter-propellant seal의 개발현황,' 한국윤활학회 추계학술대회, pp. 195-200
  3. Kwak, H. D., Jeon, S. M. and Kim, J., 2006, 'Development of Inter-propellant Seal for the Turbopump,' 3rd Asia International Conference on Tribology, ASIATRIB 2006, Kanazawa, Japan
  4. 곽현덕, 전성민, 김진한, 2005, '터보펌프용 극저온 베어링/실 성능시험설비,' 2005년도 유체기계연구개발 발표회, pp. 341-347