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터보차져용 터빈의 스핀 테스트를 위한 로터다이나믹 특성분석

Rotordynamic Characteristics Analysis of Turbocharger Turbine for Spin Test

  • 김병옥 (한국기계연구원 시스템다이나믹스연구실) ;
  • 양성진 (STX 종합기술원) ;
  • 이명호 (STX Metal 주식회사)
  • 투고 : 2011.09.14
  • 심사 : 2011.09.27
  • 발행 : 2011.12.01

초록

This paper deals with the detail rotordynamic analysis for the assembly rotor composed of turbine wheel, turbine shaft, connecting arbor, and flange & spindle in order to perform the spin test of turbocharger turbine. Prior to rotordynamic analysis, the 1st spin test was performed but the test was failed by excess vibration in the neighborhood rated speed. It is the reason for this fail that the separation margin between the rated speed and critical speed is not enough, confirmed by rotordynamic analysis results. Since then, the dimension of turbine shaft was modified and the critical speeds were again reviewed for modified assmebly rotor. In results, the separation margin between the rated speed and critical speed is over 20% and then the 2nd spin test was performed successfully. In preparing spin test for turbine, compressor wheels and etc., the geometry design of connecting arbor and dimension of rough machining should be reviewed by considering rotordynamic results, and the separation margin should be enough for successful spin test.

키워드

참고문헌

  1. 김기두 외, 2004, "중형 디젤엔진의 터보챠저 과급 시스템 최적화에 관한 연구," 한국박용기관학회지, Vol. 28, No. 7, pp. 1138-1144.
  2. 양보석, 김용한, 석호일, 유광택, 2003, "과급기 축계의 진동해석," 한국박용기관학회지, Vol. 27, No. 2, pp. 190-197.
  3. 김병옥, 이안성, 2010, "터보차져의 로터다이나믹 해석모델 개발 및 진동응답 해석," 유체기계공업학회, Vol. 13, No. 5, pp. 35-42. https://doi.org/10.5293/KFMA.2010.13.5.035
  4. Schenck, 2002, Balancing and diagonostic systems, Catalog 2002.
  5. ISO 1940-1, 2003, Mechanical vibration-Balance quality requirement for rotors in a constant(rigid) state.
  6. Lund, J. W., 1974, "Stability and Damped Critical speeds of a Flexible Rotor in Fluid Film Bearings," ASME Journal of Engineering for Industry, Vol. 96, No. 2, pp. 509-517. https://doi.org/10.1115/1.3438358

피인용 문헌

  1. FEM 시뮬레이션을 이용한 임펠러의 구조 안전성 평가 vol.43, pp.4, 2020, https://doi.org/10.11627/jkise.2020.43.4.041