Abstract
Sealing in gas turbines is paramount to overall performance and efficiency. Brush seals offer superior performance compared to other sealing solutions commonplace in modern turbomachinery. When subjected to a pressure load, a ring of flexible fine wire bristles — fitted at a lay angle to the radial plane — compact to resist the oncoming flow and deflect towards the rotor in a process known as blow-down. This study employs Digital Image Correlation to track individual bristle tips in three spatial axes throughout a large-scale brush seal test facility. This is the first-time direct measurements of blow-down throughout the bristle pack have been presented, providing a unique insight into the mechanical behaviour of brush seals.
Increased magnitudes of blow-down and axial bristle deflection were demonstrated in upstream bristle rows and at larger clearances. Analysis of these results in conjunction with the interrogation of the inter-bristle pressure field proved that blow-down is more prevalent for pressure relieving brush seals in comparison to conventional configurations. The reduction in the through-flow clearance area resulted in a significant enhancement in sealing performance for a clearance seal, highlighting a key advantage of the pressure relieving back plate design.
Increased magnitudes of blow-down and axial bristle deflection were demonstrated in upstream bristle rows and at larger clearances. Analysis of these results in conjunction with the interrogation of the inter-bristle pressure field proved that blow-down is more prevalent for pressure relieving brush seals in comparison to conventional configurations. The reduction in the through-flow clearance area resulted in a significant enhancement in sealing performance for a clearance seal, highlighting a key advantage of the pressure relieving back plate design.
| Original language | English |
|---|---|
| Title of host publication | Heat Transfer |
| Subtitle of host publication | Internal Air Systems; Heat Transfer: Internal Cooling; Industrial and Cogeneration |
| Publisher | American Society of Mechanical Engineers (ASME) |
| Volume | 8 |
| ISBN (Electronic) | 9780791888001 |
| ISBN (Print) | 9780791888001 |
| DOIs | |
| Publication status | Published - 28 Aug 2024 |
| Event | ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition - London, United Kingdom Duration: 24 Jun 2024 → 28 Jun 2024 |
Publication series
| Name | Proceedings of the ASME Turbo Expo |
|---|---|
| Volume | 8 |
Conference
| Conference | ASME Turbo Expo 2024: Turbomachinery Technical Conference and Exposition |
|---|---|
| Period | 24/06/24 → 28/06/24 |
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