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Numerical prediction of impact of clearance on rotordynamic coefficients for labyrinth brush seal

Publication ,  Journal Article
Wei, Y; Dowell, EH; Chen, Z
Published in: International Journal of Turbo and Jet Engines
March 1, 2019

The clearance has an obvious influence on the rotordynamic characteristics of brush seals. In order to better know the influence of brush seal on the stability of the rotor bearing system, the rotordynamic coefficients of labyrinth brush seal under different clearance cases and operating conditions are numerically analyzed using CFD RANS solutions coupling with a non-Darcian porous medium model. The results show that at the same geometry parameter the radial force and tangential force will increase when the pressure ratio rises. And when the clearance increases, the direct stiffness decreases sharply at first and then rises slightly. The variation of cross-coupled stiffness is complex. Moreover, at the same operating condition the value of direct damping coefficients increases when clearance increases, which add a stable factor to the rotor.

Duke Scholars

Published In

International Journal of Turbo and Jet Engines

DOI

EISSN

2191-0332

ISSN

0334-0082

Publication Date

March 1, 2019

Volume

36

Issue

1

Start / End Page

31 / 43

Related Subject Headings

  • Aerospace & Aeronautics
 

Citation

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MLA
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Wei, Y., Dowell, E. H., & Chen, Z. (2019). Numerical prediction of impact of clearance on rotordynamic coefficients for labyrinth brush seal. International Journal of Turbo and Jet Engines, 36(1), 31–43. https://doi.org/10.1515/tjj-2016-0065
Wei, Y., E. H. Dowell, and Z. Chen. “Numerical prediction of impact of clearance on rotordynamic coefficients for labyrinth brush seal.” International Journal of Turbo and Jet Engines 36, no. 1 (March 1, 2019): 31–43. https://doi.org/10.1515/tjj-2016-0065.
Wei Y, Dowell EH, Chen Z. Numerical prediction of impact of clearance on rotordynamic coefficients for labyrinth brush seal. International Journal of Turbo and Jet Engines. 2019 Mar 1;36(1):31–43.
Wei, Y., et al. “Numerical prediction of impact of clearance on rotordynamic coefficients for labyrinth brush seal.” International Journal of Turbo and Jet Engines, vol. 36, no. 1, Mar. 2019, pp. 31–43. Scopus, doi:10.1515/tjj-2016-0065.
Wei Y, Dowell EH, Chen Z. Numerical prediction of impact of clearance on rotordynamic coefficients for labyrinth brush seal. International Journal of Turbo and Jet Engines. 2019 Mar 1;36(1):31–43.
Journal cover image

Published In

International Journal of Turbo and Jet Engines

DOI

EISSN

2191-0332

ISSN

0334-0082

Publication Date

March 1, 2019

Volume

36

Issue

1

Start / End Page

31 / 43

Related Subject Headings

  • Aerospace & Aeronautics