Ventilation of a high-pressure turbine in a turbomachine

Turbomachine high-pressure turbine comprising a rotor disc (24) with upstream (30, 32) and downstream (40, 42) annular flanges separating a radially internal annular cavity (72) in which the hub (64) of the disc (24) extends from two radially external annular cavities of which one (50) is upstream o...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	GARIN FABRICE, ROUSSIN-LEROUX DELPHINE, SCHWEBLEN WILFRIED, DAKOWSKI MATHIEU
Format:	Patent
Sprache:	chi ; 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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