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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.
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 language | English |
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Title of host publication | Heat Transfer - General Interest/Additive Manufacturing Impacts on Heat Transfer; Internal Air Systems; Internal Cooling |
Subtitle of host publication | Internal Air Systems |
Volume | 7B |
ISBN (Electronic) | 9780791887011 |
DOIs | |
Publication status | Published - 28 Sept 2023 |
Event | ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition - Boston, Massachusetts, USA Duration: 26 Jun 2023 → 30 Jun 2023 |
Publication series
Name | Proceedings of the ASME Turbo Expo |
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Volume | 7-B |
Conference
Conference | ASME Turbo Expo 2023: Turbomachinery Technical Conference and Exposition |
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Period | 26/06/23 → 30/06/23 |
Funding
Engineering and Physical Sciences Research Council (Grant No. EP/P008232/1; Funder ID: 10.13039/501100000266).
Funders | Funder number |
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Engineering and Physical Sciences Research Council | EP/P008232/1 |
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Dive into the research topics of 'Fluid Dynamic Behaviour of Conventional and Pressure Relieving Brush Seals'. Together they form a unique fingerprint.Projects
- 1 Finished
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A Fundamental Investigation into Brush Seal Fluid Dynamics
Scobie, J. (PI)
Engineering and Physical Sciences Research Council
3/01/17 → 1/07/19
Project: Research council