터보펌프 축추력 조절용 캐버티 베인에 대한 수치해석적 연구

Numerical Study on the Effect of Cavity Vanes to Control the Axial Thrust of a Turbopump

  • 노준구 (한국항공우주연구원 터보펌프그룹) ;
  • 최창호 (한국항공우주연구원 터보펌프그룹) ;
  • 김진한 (한국항공우주연구원 터보펌프그룹)
  • 발행 : 2005.12.01

초록

The magnitude of the axial force acting on turbopump bearings has a great influence on the operational reliability and service life of a turbopump. In the turbopump under current investigation the cavity vanes are introduced to the pump shroud casing to control the axial thrust of the turbopump. To investigate the effect of the cavity vanes, 3D computational flow analyses for a propellant pump stage including an inducer, impeller, volute and secondary flow passages are performed with and without the vanes. The results show that the cavity vanes are very effective in reducing the magnitude of axial thrust without notable changes on the overall performance of the turbopump.

키워드