Flow Conditioning to Control the Effects of Inlet Swirl on Brush Seal Performance in Gas Turbine Engines
When subject to highly swirling inlet flow, the bristles on the upstream face of a brush seal in gas turbine engines tend to slip circumferentially, which may lead to aeromechanical instability and seal failure. In this article, a new design of the front plate of brush seal, which mitigates this eff...
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| Hauptverfasser: | , , , , , |
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| Format: | Artigo |
| Sprache: | Inglês |
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Frontiers Media S.A.
2022-02-01
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| Schriftenreihe: | Frontiers in Energy Research |
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| Online-Zugang: | https://www.frontiersin.org/articles/10.3389/fenrg.2021.815152/full |
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