공동 스퀴즈 필름 댐퍼에 지지된 회전체의 정상상태 응답 해석

Steady State Respknse of a Rotor Supported on Cavitated Squeeze Film Dampers

  • 정시영 (인하공업전문대학 항공기계과) ;
  • 정재천 (인하대학교공과대학기계공학과) ;
  • 심상규 (인하대학교공과대학기계공학과)
  • 발행 : 1992.09.01

초록

The effect of cavitation on the synchronous steady state response of a single rotor supported on cavitated squeeze film dampers executing a circular orbit is investigated theoretically. The Swift-Stieber boundary conditions and a long bearing approximation are utillized to evaluate the direct and the cross coupled damping coefficients of a cavitated squeeze film damper. For typical design parameters, frequency response curves are presented here to exhibit the effect of cavitation on the imbalance response and transmissibilities for both a flexible rotor and a rigid rotor. Investigations show that cavitation occured in a squeeze film damper produces bistable jump phenomena and deteriorates the performance of a squeeze film damper. This arises from that the large cavity causes substantial increment of the cross coupled damping which has radial stiffening effect. Furthermore, the large cavity causes the decrement of the direct damping which has pure damping effect. It is also observed that in the absence of cavitation, both rotor excursion amplitude and imbalance transmissibilities are very well damped.

키워드

참고문헌

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