Feasibility Study on Design of Thrust Bearing for Micro Gas Turbine/Generator

초소형 가스 터빈/제너레이터용 스러스트 베어링의 설계 및 타당성에 관한 연구

  • 곽현덕 (한국과학기술연구원 트라이볼로지 연구센터) ;
  • 이용복 (한국과학기술연구원 트라이볼로지 연구센터) ;
  • 김창호 (한국과학기술연구원 트라이볼로지 연구센터) ;
  • 장건희 (한양대학교 정밀기계공학과)
  • Published : 2001.11.01

Abstract

Feasibility study of gas-lubricated bearing in micro gas turbine was performed. Based on Reynolds equation, finite difference method with coupled boundary was developed to analyze bearing characteristics, such as load-carrying capacity, mass flow rates and stiffness. By the bearing force and mass flow rates analysis with the variation of supply pressure, bearing clearance and capillary radius, acceptable range of design parameters were suggested in terms of load capacity and stiffness of bearings. Additionally, coupled boundary effect on pressure distribution was investigated and it is stated that coupling could reduce all excitation force due to narrow pressure distribution.

Keywords