SLEEVE MOUNTED ONTO A LOW-PRESSURE SHAFT IN A TURBOMACHINE

The present invention relates to a rotating assembly of a turbomachine, comprising:-a shaft configured to drive a propeller of the turbo machine around an axis and comprising a first flange radially extending from the shaft, the first flange being monolithic with the shaft;-a sleeve fitted onto the...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	ROSSET, Patrice Jean-Marc, TAILLANT, Jean-Claude Christian, SIMON, Vianney, SULTANA, Patrick Jean Laurent
Format:	Patent
Sprache:	eng
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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