AIRCRAFT TURBOSHAFT ENGINE COMPRESSOR COMPRISING A DEVICE FOR IMMOBILISING A RETAINING RING

Disclosed is a compressor of a dual-flow aircraft turboshaft engine extending longitudinally along an axis X, the compressor comprising a low-pressure compressor, a high-pressure compressor and an intermediate casing axially connecting the low-pressure compressor and the high-pressure compressor, th...

Ausführliche Beschreibung

Bibliographische Detailangaben

Hauptverfasser:	DELAHAYE, Thomas, Nolwenn, Emmanuel, DUMAS, Lilian, Yann, BERGON, Blaise, JABLONSKI, Laurent, SEVI, Guillaume, ROBIN, Noël, Joseph, Camille, VAN DE KERCKHOVE, Thomas, Etienne, Camille, Marie
Format:	Patent
Sprache:	eng ; fre ; ger
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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