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Numerical investigation of temperature field in brush seals

  • Li Ke Li*
  • , Zhi Li Wang
  • , Fei Song
  • , Wei Wang
  • , Cong Hui Chen
  • *Corresponding author for this work
  • Beihang University
  • China Aviation Industry Corporation

Research output: Contribution to journalArticlepeer-review

Abstract

The mechanism of frictional heat generation and heat transfer in brush seals was analyzed and a computational fluid dynamics (CFD) model was developed. In the model, the brush was treated as an anisotropic porous region with nonlinear resistance coefficients and the frictional heat as a heat source. The pressure distribution, velocity field and temperature field were obtained and the maximum temperature under various interference and pressure difference conditions were studied. The investigation shows a steep temperature rise in bristle-rotor interface, which diminishes further away in the radial direction; fluid convection and leakage flow affect temperature distribution deeply. The results can be used to guide brush seal geometry design, contact-pair material selection and interference fit.

Original languageEnglish
Pages (from-to)1018-1024
Number of pages7
JournalHangkong Dongli Xuebao/Journal of Aerospace Power
Volume25
Issue number5
StatePublished - May 2010

Keywords

  • Brush seals
  • Computational fluid dynamics
  • Heat transfer
  • Porous media
  • Temperature field

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