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소형 가스터빈 회전체의 위험속도 해석

Critical Speed Analysis of a Small Gas Turbine Rotor

  • 투고 : 2009.01.13
  • 심사 : 2009.04.07
  • 발행 : 2009.06.01

초록

This paper predicts the critical speeds of a 5MW industrial gas turbine by using commercial rotordynamic tool, DYNAMICS 4.3. The gas turbine is operated at 12,975 rpm on squeeze film dampers. The stiffness of the squeeze film dampers are estimated. The critical speeds of the gas turbine rotor are calculated to have a sufficient separation margin (2%) from the 1st bending mode and pass over 2 rigid body modes below 4,000 cpm. This paper discussed the coupling effects on the dynamic response of the gas turbine.

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참고문헌

  1. 김영철, 이동환, 심재호, 2006, '가스터빈엔진(GTE)의 동적설계기술현황,' 유체기계저널, 9권 5호, pp. 60~63 https://doi.org/10.5293/KFMA.2006.9.5.060

피인용 문헌

  1. vol.13, pp.1, 2010, https://doi.org/10.5293/KFMA.2010.13.1.069