Trunnion for high-pressure turbine, and turbojet engine including such a trunnion

The invention relates to a trunnion (23) for a high-pressure turbine (11), to be arranged between a shaft of a low-pressure turbine (9) and an inner surface (34) of a seal mounting (26) of the low-pressure turbine (8), the trunnion (23) being characterized in that it includes a drop-launching extens...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser: Garin, Fabrice, Coulombeau, Laurent Jacques Michel, Judet, Maurice Guy
Format: Patent
Sprache:eng
Schlagworte:
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