Fluid Dynamic Behaviour of Conventional and Pressure Relieving Brush Seals

Joshua p. Bowen, Joshua j. Bird, Harry Cross, Matthew r. Jenkins, Aaron a. Bowsher, Peter f. Crudgington, Carl M. Sangan, James A. Scobie

Research output: Chapter or section in a book/report/conference proceedingChapter in a published conference proceeding

1 Citation (SciVal)

Abstract

Brush seals consist of a static ring of densely packed, flexible, fine wire bristles that provide resistance to the flow. Pressure relieving brush seals can be employed to overcome issues such as hysteresis that affect seal durability by reducing friction between the bristle pack and back plate surface. The impact of such designs on the fluid dynamic behaviour of brush seals was studied following a concomitant methodology that exploited the benefits of both engine representative and large-scale testing facilities. Leakage data were fitted using a porous medium model found in the literature to quantify viscous and inertial resistance coefficients.

Shaft rotation was shown to cause a reduction in seal leakage and an increase in static pressure on the back plate surface. The pressure relieving back plates also resulted in increased static pressures at this location, causing a reduction in flow resistance that increased leakage through the porous bristle pack. Interrogation of the large-scale inter-bristle pressure field for the two back plate designs revealed the distributions of axial pressure diverged towards the rear of the bristle pack. The detail gathered using the large-scale study has been shown to be representative, hence the insight is generically applicable to brush seals.
Original languageEnglish
Title of host publicationHeat Transfer - General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling
Subtitle of host publicationInternal Air Systems
Volume7B
ISBN (Electronic)9780791887011
DOIs
Publication statusPublished - 28 Sept 2023
EventASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition - Boston, Massachusetts, USA
Duration: 26 Jun 202330 Jun 2023

Publication series

NameProceedings of the ASME Turbo Expo
Volume7-B

Conference

ConferenceASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition
Period26/06/2330/06/23

Funding

Engineering and Physical Sciences Research Council (Grant No. EP/P008232/1; Funder ID: 10.13039/501100000266).

FundersFunder number
Engineering and Physical Sciences Research CouncilEP/P008232/1

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