TURBOMACHINE ELEMENT COMPRISING AN AUXILIARY SEALING MEANS, AND METHOD FOR TESTING THIS ELEMENT

The invention relates to a turbomachine element comprising a stator (2), a rotor (1), and a first sealing means (9) for sealing between the rotor (1) and the stator (2) arranged to be active when the rotor is in the operating position of same around the axis of rotation (LL) thereof, the element bei...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	RENON, OLIVIER, LEUTARD, FLORENCE IRENE NOELLE, JAMON, THIBAULT
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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