위험속도를 통과하는 회전체시스템 개발

Development of Flexible Rotor Systems For Gas Turbine Engine

  • 이정훈 (삼성테크윈 엔진연구소) ;
  • 이영섭 (삼성테크윈 엔진연구소) ;
  • 김경수 (삼성테크윈 엔진연구소) ;
  • 김창근 (삼성테크윈 엔진연구소) ;
  • 김명섭 (삼성테크윈 엔진연구소)
  • 발행 : 2000.06.22

초록

High speed rotor test rig was developed for flexible rotor systems which have its bending critical speed at 14000 rpm. In designing the flexible rotor systems, operating speed have to be escaped from the critical speed, due to large vibration. In this paper, dynamic characteristics of the rotor systems were analyzed and compared with test results. And the effect of allison ring damper and rotor balancing were examined both theoretically and experimentally. Finally, the magnitude of vibration was largely reduced at the critical speed.

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