A test on passing through bending critical speed of Flexible Rotor supported by AFB

AFB으로 지지된 탄성회전체의 위험속도 통과시험

  • 이영섭 (삼성테크윈 파워시스템 연구소) ;
  • 염병용 (삼성테크윈 파워시스템 연구) ;
  • 김진형 (삼성테크윈 파워시스템 연구) ;
  • 김명섭 (삼성테크윈 파워시스템 연구소)
  • Published : 2001.11.01

Abstract

A flexible rotor was smoothly passed through its bending critical speed, which is supported by AFB. Then, maximum magnitude of the rotor vibration at the middle point was 25${\mu}$m. The test rig was largely consisted of air turbine, multi-leaf type air foil bearing and flexible rotor and its bending critical speed was 32,600 rpm. And the balancing system and method for field balancing of the flexible rotor were developd successfully.

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