VENTILATION RING FOR THE REAR BEARING SUPPORT MEMBER OF AN AIRCRAFT TURBINE ENGINE

A ventilation ring for a bearing support member of an aircraft turbine engine includes two or more tubular walls and one or more spacer walls. The two or more tubular walls extend opposite each other, and one or more of the tubular walls includes a main portion and a base, the base having a thicknes...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GARNIER, Fabien Stéphane, VOIRON, Mickaël, OVAERE, Nicolas
Format:	Patent
Sprache:	eng
Schlagworte:	BLASTING ENGINE PLANTS IN GENERAL HEATING LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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