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Vibration Response Analysis of a Small Gas Turbine Rotor

소형 가스터빈 회전체의 진동응답 해석

  • Received : 2009.09.03
  • Accepted : 2010.04.27
  • Published : 2010.06.01

Abstract

This paper predicts the unbalance and transient (start-up) response of a 5MW industrial gas turbine by using commercial rotordynamic tool, DYNAMICS 4.3. The gas turbine is operated at 12,975rpm on squeeze film dampers or tilting pad bearings. The stiffness and damping coefficients of the squeeze film dampers and tilting pad bearings are estimated. It is seen that the vibration amplitude of the gas turbine rotor is sufficiently small around the critical speeds and at the rated speed.

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References

  1. 김영철, 하진웅, 명지호, 2009, “소형 가스터빈 회전체의 위험속도 해석”, 유체기계저널, 12권 3호, pp. 26-30. https://doi.org/10.5293/KFMA.2009.12.3.026
  2. 김영철, 이동환, 심재호, 2006, “가스터빈엔진(GTE)의 동적설계기술현황”, 유체기계저널, 9권 5호, pp. 60-63. https://doi.org/10.5293/KFMA.2006.9.5.060