Labyrinth seal with angled fins

An aircraft engine having a shaft, an engine casing, at least one bearing located between the shaft and the engine casing, the engine casing defining a bearing cavity containing the at least one bearing, an air distribution system configured to inject compressed air to the bearing cavity to in use p...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Legare, Pierre-Yves, Smith, Alexander
Format: Patent
Sprache:eng
Schlagworte:
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