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A Study of Fault Mechanisms in a Rotor-Seal System

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Periodical:

Key Engineering Materials (Volumes 245-246)

Pages:

399-406

DOI:

https://doi.org/10.4028/www.scientific.net/KEM.245-246.399

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Online since:

July 2003

Authors:

Li Dong He, Jin Ji Gao

Keywords:

Fault Mechanism, Fluid Solid Coupling, Rotor, Seal

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© 2003 Trans Tech Publications Ltd. All Rights Reserved

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References

[1] R. Nordanm, P. Werner: Rotordynamic coefficients for Labyrinth seal calculated by means of finite difference technique. (1988), NASA CP3026.

Google Scholar

[2] J. A. Moore: CFD comparison to 3D laser anemometer and rotordynamic force measurements for grooved liquid annular seals. Journal of Tribology, Vol. 121 (1999), p.306.

DOI: 10.1115/1.2833937

Google Scholar

[3] R. Beatty, M. Hine: Improved rotor response of the uprated high pressure oxygen turbopump for the space shuttle main engine. Journal of Vibration, Acoustic, Stress, and Reliability in Design, Vol. 111 (1989), p.163.

DOI: 10.1115/1.3269837

Google Scholar

[4] E. Memmott: Stability analysis and testing of a train of centrifugal compressors for high pressure gas injection. Journal of Engineering for Gas Turbines and Power, Vol. 121 (1999), p.509.

DOI: 10.1115/1.2818502

Google Scholar

[5] D. Childs: A comparison of experimental rotordynamic coefficients and leakage characteristics between hole-pattern gas damper seals and a honeycomb seal. Journal of Engineering for Gas Turbines and Power, Vol. 120 (1998), p.778.

DOI: 10.1115/1.2818467

Google Scholar

[6] E. Soto, D. Childs: Experimental rotordynamic coefficient results for (a) a labyrinth seal with and without shunt injection and (b) a honeycomb seal. Journal of Engineering for Gas Turbines and Power, Vol. 121 (1999), p.153.

DOI: 10.1115/1.2816303

Google Scholar

[7] K. Chien: Predictions of channel and boundary layer flows with low-Reynolds-number turbulence model. AIAA Journal, Vol. 20 (1982), p.33.

DOI: 10.2514/3.51043

Google Scholar

[8] A. Muszynska: Improvements of lightly loaded rotor/bearing and rotor/seal models. Journal of vibration, Acoustics, Stress and Reliability in Design, Vol. 110 (1988), p.129.

DOI: 10.1115/1.3269489

Google Scholar

[9] N. Zirkelback: Qualitative characterization of anti-swirl gas dampers. Journal of Engineering for Gas Turbines and Power, Vol. 121 (1999), p.342.

DOI: 10.1115/1.2817126

Google Scholar

[10] H. Kanki, Y. Keneko: Prevention of low-frequency vibration of high-capacity steam turbine units by squeeze-film damper. Journal of Engineering for Gas Turbines and Power, Vol. 120 (1998), p.391.

DOI: 10.1115/1.2818135

Google Scholar

[11] Xin Yuan: Stabilization of high-order high resolution schemes for the compressible NavierStokes equation. Int. J Numerical methods for Heat and Fluid Flow, Vol. 7 (1997).

Google Scholar