This article presents a brief review of the experimental and theoretical state of the art regarding the leakage flow prediction of brush seals. The authors model a computational fluid dynamics (CFD)-based approach for the leakage flow of brush seals. The brush seal is treated by modeling its real geometrical structure, namely numerous bristles in an array in transverse flow. The fluid domain is segregated into discrete volumes surrounding each bristle. Two different discretization schemes are chosen to study their influence on the leakage behavior. Furthermore, for each scheme multiple inter-bristle distances, pressure ratios and turbulence models are evaluated. In addition, the influence of irregular arrangement configurations, which forms a quasi-chaotic inner structure, is studied. The results gained are compared to other authors' experimental and numerical data.
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February 2019
Research-Article
Effects of Uncertainty and Quasi-Chaotic Geometry on the Leakage of Brush Seals
Alexander Fuchs,
Alexander Fuchs
Division Space Propulsion,
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: alexander.fuchs@ltf.mw.tum.de
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: alexander.fuchs@ltf.mw.tum.de
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Oskar J. Haidn
Oskar J. Haidn
Professor
Division Space Propulsion,
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: oskar.haidn@ltf.mw.tum.de
Division Space Propulsion,
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: oskar.haidn@ltf.mw.tum.de
Search for other works by this author on:
Alexander Fuchs
Division Space Propulsion,
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: alexander.fuchs@ltf.mw.tum.de
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: alexander.fuchs@ltf.mw.tum.de
Oskar J. Haidn
Professor
Division Space Propulsion,
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: oskar.haidn@ltf.mw.tum.de
Division Space Propulsion,
Chair of Turbomachinery and Flight Propulsion,
Department of Mechanical Engineering,
Technical University of Munich,
Boltzmannstraße 15,
Garching bei München 85748, Germany
e-mail: oskar.haidn@ltf.mw.tum.de
1Corresponding author.
Manuscript received February 14, 2018; final manuscript received July 19, 2018; published online January 16, 2019. Assoc. Editor: Coutier-Delgosha Olivier.
J. Turbomach. Feb 2019, 141(2): 021003 (9 pages)
Published Online: January 16, 2019
Article history
Received:
February 14, 2018
Revised:
July 19, 2018
Citation
Fuchs, A., and Haidn, O. J. (January 16, 2019). "Effects of Uncertainty and Quasi-Chaotic Geometry on the Leakage of Brush Seals." ASME. J. Turbomach. February 2019; 141(2): 021003. https://doi.org/10.1115/1.4041081
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