ANNULAR COMPONENT FOR SUPPORTING A BEARING OF A TURBINE ENGINE

A component (1, 2) for supporting at least one bearing (3) for a turbine engine (10) comprising: - two coaxial walls, internal (4) and external (5) walls respectively, defining a gas flow vein (6) between them and interconnected by a row of arms (7); - an external ferrule (50) comprising an internal...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	VIVE, LOIS PIERRE DENIS, JOSSE, ALBERT, LAMEIGNERE, YVAN LUDOVIC, CASAUX-BIC, JEAN-MAURICE
Format:	Patent
Sprache:	eng ; fre
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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