A Development of Turbine Simulator and Foundation Excitation Test

모사터빈 시험기 개발 및 기초가진 시험

  • 김영철 (한국기계연구원 구조연구부 회전체그룹) ;
  • 이안성 (한국기계연구원 구조연구부 회전체그룹) ;
  • 김병옥 (한국기계연구원 구조연구부 회전체그룹) ;
  • 김영춘 (두산중공업(주) 기술연구원) ;
  • 우성현 (한국항공우주연구원 우주시험그룹)
  • Published : 2004.05.01

Abstract

In this study, a turbine simuiator is designed and manufactured to investigate the transient response of an actual turbine. The rotor mass and bearing stiffness is reduced to 1/140 of its actual turbine. The dynamic characteristics of turbine simulator are similar to those of the actual turbine. The turbine simulator is excited by an electro-magnetic type exciter in the form of half sine wave. Duration time is con☞oiled by Sms, 10ms, and Isms, and maximum acceleration is applied by 3g. Foundation excitation test is performed in stationary condition and rotating condition(6000rpm). The test results can be used to verify the validif of the theoretical afproach for transient analysis of actual turbine.

Keywords